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1988 INDEX


1988-001: THE ESA POLICY AND PROGRAMME FOR THE DEVELOPMENT OF ELECTRIC PROPULSION; W. Berry, C. Bartoli, A. Trippi, ESA/ESTEC Technical Directorate, Noordwijk, The Netherlands

1988-002: THE NASA ELECTRIC PROPULSION; James R. Stone, Office of Aeronautics and Space Techology, David C. Byers, National Aeronautics and Space Administration, and David  Q. King, Jet Propulsion Laboratory

1988-003: ELECTRIC PROPULSION PROJECTS AND RESEARCHES IN JAPAN; Kyoichi Kuriki, Institute of Space and Astronautical Science, Yoshinodai, Sagamihara-shi 229, Japan; Yoshihiro Nakamura, National Aerospace Laboratory, Jindaiji-higashi-cho, Chofu, Toyko 182, Japan

1988-004: RECENT PROGRESS IN THE USSR ELECTRIC PROPULSION; V.V. Zhurin, A.S. Koroteev, A.A. Porotnikov, B.B. Rodrevich, Academy of Sciences, Moscow, USSR

1988-005: INTERESTS IN ELECTRIC PROPULSION; Captin Wayne M. Schmidt, USAF, and John C. Andrews, U.S. Air Force Astronautics Laboratory, Edwards Air Force Base, CA

1988-006: ELECTRIC PROPULSION: IMPLEMENTATION ISSUES; Rolland Schreib, International Telecommunication Satellite Organization (INTELSAT), Washington, D.C. 20008, USA

1988-007: THE ROLE OF ELECTRIC PROPULSION IN EXTENDING THE ECONOMIC LIFE-CYCLE OF COMMERCIAL  EUROPEAN TELECOMMUNICATION SATELLITES; H. G. Lechte and L. C. van Holtz, ESA/ESTEC Communications Department, Noordwijk, The Netherlands

1988-008: ELECTRIC PROPULSION FOR LOW EARTH ORBIT APPLICATIONS; M. Andrenucci, Dipartimento di Ingegneria Aerospaziale, Università di Pisa, Pisa, Italy; and A. Trippi, ESA/ESTEC Technical Directorate, Noordwijk, The Netherlands

1988-009: THE ROSETTA/CNSR MISSION: A POSSIBLE APPLICATION OF ELECTRIC PROPULSION TO INTERPLANETARY MISSIONS; A. Atzei, D/SCI, ESA/ESTEC, Noordwijk, The Netherlands

1988-011: PLASMA PROPULSION ACTIVITIES AT SNIA BPD; G. Baiocchi, G. Cruciani, E. Tosti, SNIA BPD, Colleferro, Italy

1988-013: SPACECRAFT AND MISSION DESIGN FOR THE SP-+100 FLIGHT EXPERIMENT, William D. Deininger, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California, USA; and Robert J. Vondra, W. J. Schafer, Associates, Arlington, Virginia, USA

1988-015: DEVELOPMENT OF AN MPD PROPULSION SYSTEM, Y. Shimizu, K. Toki, and K. Kuriki, Institute of Space and Astronautical Science, Sagamihara-shi, Kanagawa 229, Japan

1988-016: INTERACTION OF HIGH VOLTAGE SOLAR ARRAY WITH IONOSPHERIC PLASMA; H. Kurninaka, S. Satori, Y. Nozaki, and K. Kuriki; Institute of Space and Astronautical Science, Yoshinodai, Sagamihara, Kanagawa, Japan

1988-018: THE INTERACTION BETWEEN A POSITIVELY BIASED CONDUCTOR ON A HIGH VOLTAGE SOLAR ARRAY AND A PLASMA; Daniel E. Hastings, MIT, Cambridge, MA 02139, USA

1988-019: DEPLOYABLE AEROSPACE PHOTOVOLTAIC ARRAY BASED ON AMORPHOUSE SILICON ALLOYS; J. J. Hanak, Lee Walter, David Dobias and Harvey Flaisher, Sovonics Solar Systems, 100 West Maple Road, Troy, Michigan 48084, USA

1988-020: FEEP POWER CONDITIONING UNIT: DESIGN AND DEVELOPMENT STATUS; A. Bonati and C. Bocchiola, F.I.A.R., Milan, Italy and D. Valentian, S.E.P. Vernon, France

1988-021: FIELD EMISSION ELECTRIC PROPULSION: EMISSION PERFORMANCE OF SLIT-TYPE LIQUID METAL ION SOURCES; J. Mitterauer, Technishce Universität Wien, Vienna, Austria

1988-022: FIELD EMISSION ELECTRIC PROPULSION (FEEP) ATTITUDE CONTROL CAPABILILTIES; D. Valentian and J. P. Bugeat; SEP; AND C. Bartoli and H. Von Rohden; ESA/ESTEC

1988-025: CYLINDRICAL STEADY-STATE MPD THRUSTER; H. L. Kurtz, M. Auweter-Kurtz, B. Glocker, H. Habiger, W. Merke, and H. O. Schrade, Institut für Raumfahrtsysteme, Universität Stuttgart

1988-026: IMPROVED THRUST GENERATION MECHANISM FOR ELECTROTHERMAL/ELECTROMAGNETIC ARCJET; Eiji Nishida, Mitsubishi Electric Corporation and Yukio Shimizu and Kyoichi Kuriki, Institute of Space and Astronautical Science

1988-028: NOZZLE TYPE AND THRUSTER EXPERIMENTAL INVESTIGATION; W. D. Merke, H. Auweter-Kurtz, H. Habiger, H. Kurtz and H. O. Schrade, Institut für Raumfahrtsysteme, Universität Stuttgart

1988-029: STATUS OF THE RITA – EXPERIMENT ON EURECA; H. Bassner, H-P. Berg, MBB Ottobrunn, FRG; C. Bartoli, and A. Trippi, ESA/ESTEC, Noordwijk, The Netherlands

1988-031: THE PROPOSED DEMONSTRATION OF THE UK-10 ION PROPULSION SYSTEM ON ESA’S SAT-2 SPACECRAFT; D. G. Fearn, Space Department, Royal Aerospace Establishment, Farnborough, Hants., UK

1988-033: DESIGN AND DEVELOPMENT OF THE UK-10 ION PROPULSION SUBSYSTEM; P. Smith, Principal Propulsion Engineer, Marconi Space Systems Ltd., Portsmouth, U.K.

1988-034: AUXILIARY PROPULSION RF-ENGINE RIT 15 – PROTOTYPE DESIGN AND PERFORMANCE, K. H. Groh, A. Dillmann, H. W. Loeb, F. Weber, 1st Institute of Physics, Giessen University, Heinrich-Buff-Ring 16, D-6300 Giessen, FRG

1988-035: SUCCESSFUL COMPLETION OF A CYCLIC GROUND TEST OF A MERCURY ION AUXILIARY PROPULSION SYSTEM; David R. Francisco, Charles A. Low, Jr., and John L. Power; National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135

1988-036: DESIGN AND INTEGRATION OF AN ELECTRIC PROPULSION SYSTEM ON THE EUROSTAR SPACECRAFT; T. Duhamel, P. H. Ricaud, and P. Greff, MATRA Espace, Toulouse, France

1988-038: NUMERICAL CODES FOR CYLINDRICAL MPD THRUSTERS; P. C. Sleziona, M. Auweter-Kurtz, and H. O. Schrade, Institut für Raumfahrtsysteme, Universität Stuttgart

1988-039: FLUID MECHANICS IN A MAGNETOPLASMADYNAMIC THRUSTER; D. J. Heimerdinger, and M. Martinez-Sanchez, Massachusetts Institute of Technology, Space Systems Laboratory, Cambridge, Massachusetts 02139

1988-040: AN IMPROVED CODE FOR NOZZLE TYPE STEADY STATE MPD THRUSTERS; M. Auweter-Kurtz, S. F. Glaser, H. L. Kurtz, H. O. Schrade, and P. C. Sleziona; Institut für Raumfahrtsysteme, Universität Stuttgart

1988-042: CURRENT DRIVEN INSTABILITIES OF AN ELECTROMAGNETICALLY ACCELERATED PLASMA; E. Y. Choueiri, A. J. Kelly, and R. G. Jahn; Electric Propulsion Laboratory, Princeton University, Princeton, NJ 08544

1988-043: INVESTIGATION OF INSTABILITIES IN MPD THRUSTER FLOWS USING A LINEAR DISPERSION RELATION; D. Rempfer and M. Auweter-Kurtz, Institut für Raumfahrtsysteme, Universität Stuttgart; H. J. Kaeppeler, Institut für Plasmaforschung, Universität Stuttgart; and M. Maurer, MAN Technologie GmbH, München, Federal Republic of Germany

1988-045: DC POWER CONTROL FOR A LIQUID-FED RESISTOJET; Robert P. Gruber, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135

1988-047: DEVELOPMENT OF A FLIGHT STANDARD POWER CONDITIONING AND CONTROL SYSTEM FOR THE T5 ION THRUSTER; Manoj Mohan, Royal Aerospace Establishment, Farnborough, UK; David Diani, Royal Aerospace Establishment, Farnborough, UK and Polytechnic of Wales, Pontypridd, UK; and David Rees, Polytechnic of Wales, Pontypridd, UK

1988-048: VERIFICATION OF PERFORMANCE AND ENDURANCE OF CAPACITOR BANK FOR THE ELECTRIC PROPULSION EXPERIMENT (EPEX); Y. Kunii, M. Sumida, T. Moriai, H. Sasaki, T. Okamura, H. Harada, and K. Ijichi; Mitsubishi Electric Corporation, Kamakura Works, Kamimachiya, Kamakura, Kanagawa 247, Japan and Y. Shimizu and K. Toki, Institute of Space and Astronautical Science, yoshinodai, Sagamihara, Kanagawa 229, Japan

1988-049: VERIFICATION OF CONTROL SEQUENCE AND ARGORITHM FOR THE ELECTRIC PROPULSION EXPERIMENT (EPEX); M. Sumida, Y. Kunii, T. Moriai, T. Okamura, T. Yoshida, and K. Ijichi; Mitsubishi Electric Corporation, Kamakura Works, Kamimachiya, Kamakura, Kanagawa 247, Japan; and Y. Shimizu and K. Toki; Institute of Space and Astronautical Science, Yoshinodai, Sagamihara, Kanagawa 229, Japan

1988-051: CONTROLLING A STATIONARY ORBIT USING ELECTRIC PROPULSION; Bernard M. Anzel, Laboratory Scientist, Hughes Aircraft Company, Space and Communications Group, Systems Laboratories, El Segundo, California, U.S.A.

1988-056: CONTINUOUS OPERATION OF A QUASI-STEADY MPD PROPULSION SYSTEM WITH AN EXTERNAL MAGNETIC FIELDS; T. Yoshikawa, Y. Kagaya, H. Tahara, and T. Wasa, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka 560, Japan

1988-057: OPTIMIZAATION OF CURRENT DISTRIBUTION IN AN APPLIED-FIELD MPD THRUSTER; A. Sasoh, A. E. Solem, and Y. Arakawa, University of Tokyo, Tokyo, Japan

1988-058: HYBRID MPD THRUSTER WITH AXIAL AND CUSP MAGNETIC FIELDS; H. Tahara, Y. Kagaya, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka 560, Japan

1988-060: XENON ION THRUSTER TEST FACILITY – DESIGN AND OPERATION; S. Kitamura, K. Miyazaki, Y. Hayakawa, and Y. Nakamura, National Aerospace Laboratory, Tokyo, Japan

1988-061: DISCHARGE PERFORMANCE OF A 12 CM CUSP XENON ION THRUSTER; Yoshihiro Nakamura, Manabu Matsumoto, Shoji Kitamura, and Katsuhiro Miyazaki, National Aerospace Laboratory, Jindaiji-higashi, Chofu, Tokyo 182, Japan, Tokai University

1988-062: HIGH THRUST OPERATION OF THE UK-10 RARE GAS ION THRUSTER (T4A); A. R. Martin and P. M. Latham, Culham Laboratory, Abingdon, Oxon OX14 3DB, England

1988-064: RING CUSP/HOLLOW CATHODE DISCHARGE CHAMBER PERFORMANCE STUDIES; J. A. Vaughn and P. J. Wilbur, Colorado State University, Fort Collins, Colorado U.S.A.

1988-065: SURVEY OF ELECTRIC PROPULSION THRUSTER APPLICABILITY TO NEAR EARTH SPACE MISSIONS; Mitat Birkan, Air Force Office of Scientific Research, Bolling AFB, DC; Michael M. Micci, Department of Aerospace Engineering, The Pennsylvania State University, University Park, PA

1988-067: ELECTRICAL TRANSFER VEHICLE ANALYSIS FOR FUTURE SPACE OPERATIONS (MESCATS); W. Kleinau, D. E. Koelle and W. Müller, MBB Space Communications and Propulsion Systems Division, Munich/ Fed. Rep. of Germany

1988-068: A CASE STUDY OF A MISSION TO THE KORDYLEWSKI CLOUDS USING ION PROPULSION; K. A. Ryden, Pinehurt Cottages; P. G. Herrington, Wayman Rd.; and N. C. Wallace, Farnborough Rd., Farnborough, Hants, UK.

1988-069: A SMALL ION-PROPELLED SPACECRAFT FOR NEAR EARTH EXPERIMENTS; K. A. Ryden and N. C. Wallace, Space Department, Royal Aerospace Establishment, Farnborough, Hants, UK

1988-072: CATHODE PROCESSES IN A MPD ARCJET; K. D. Goodfellow and S. N. B. Murthy; School of Mechanical Engineering, Purdue University, West Lafayette, IN 47907

1988:073: THERMAL DESIGN IMPROVEMENTS FROM 30kWe ARCJET ENGINES; W. D. Deininger, A. Chopra, D. Q. King, and T. J. Pivirotto, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

1988-074: ELECTRODE EROSION IN STEADY-STATE ELECTRIC PROPULSION ENGINES; Thomas J. Pivirotto and W. D. Deininger, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1988-075: CHARACTERIZATION OF COLD CATHODE EROSION PROCESSES; J. E. Polk, A. J. Kelly, and R. G. Jahn, Electric Propulsion Laboratory, Princeton University, Princeton, NJ 08544

1988-076: ANODE-NOZZLE EXPERIMENTAL ANALYSIS IN A COAXIAL NON-STEADY SOLID PROPELLANT MPD THRUSTER; Giorgio Paccani, University of Roma “La Sapienza,” Roma, Italy

1988-077: THE PROPELLANT SUPPLY AND MONITORING EQUIPMENT (PSME) FOR THE UK-10 ION PROPULSION SUBSYSTEM; S. D. Watson, Senior Propulsion Engineer, Marconi Space Systems Ltd, Portsmouth, England

1988-078: A REVIEW OF THE CATHODE CONSTRUCTION FOR THE RAE 10/25mN THRUSTER; S. A. Gair, Central Materials Laboratory, Philips Components, Mitcham, England; and P. T. Harris, Central Materials Laboratory, Philips Components, Mitcham, England

1988-079: DISCHARGE PLASMA CALCULATIONS IN CUSPED ION THRUSTERS USING THE FINITE ELEMENT METHOD; Yoshihiro Arakawa, University of Tokyo, Tokyo, Japan; and Paul J. Wilbur, Colorado State University, Fort Collins, Colorado, USA.

1988-080: AN APPROACH TO THE PARAMETRIC DESIGN OF ION THRUSTERS; Paul J. Wilbur, Colorado State University, Fort Collins, Colorado 80523, U.S.A.; and John R. Beattie and Jay Hyman, Jr., Hughes Research Laboratories, Malibu, California 90265, U.S.A.

1988-082: MAGNETIC INDUCTION THRUSTER WITH LITHIUM PROPELLANT, Stewart A. Burton and Michael M. Micci, Department of Aerospace Engineering, The Pennsylvania State University, University Park, PA

1988-083: EXPERIMENTAL STUDY OF DOUBLE STAGE DISCHARGE HALL ION THRUSTER; Y. Yamagiwa and K. Kuriki, Toshiba Komukai Works, 1 Komukaitoshiba-cho, The Institute of Space and Astronautical Science 3-1-1 Yoshinodai, Sagamihara-shi, Japan

1988-084: ULTIMATE PERFORMANCE LIMITS AND MISSION CAPABILITIES OF ADVANCED ION THRUSTERS; A. R. Martin, A. Bond, and R. A. Bond, Culham Laboratory, Abindon, Oxon, OX14 3DB, England

1988-085: INTERSTELLAR FLIGHT: ASPECTS OF BEAMED ELECTRIC PROPULSION; G. L. Matloff, Baruch College of CUNY, Dept. of Natural Sciences, New York, NY, USA and St. Hilda’s and St. Hugh’s School, Dept. of Mathematics, New York, NY and E. F. Mallove, MIT News Office, Cambridge, MA, USA

1988-086: INTEGRATED FUSION PROPULSION PLANTS FOR AEROSPACE PLANES AND SPACE VEHICLES; Alex Farkas, Mechanical Engineer, Westinghouse Electric Corporation, Sunnyvale, California, U.S.A.

1988-088: QUANTITATIVE IMAGING OF MPD FLOWFIELDS; T. Nakayama, K. Toki, and K. Kuriki, Sagamihara-shi, Kanagawa 229, Japan

1988-091: EXPERIMENTAL EVALUATION OF RESISTOJET THRUSTER PLUME SHIELDS; Lynnette M. Carney, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH 44135; and Allan B. Bailey, Calspan Corporation, Arnold Engineering Development C enter, Arnold Air Force Base, TN 37389

1988-092: ANALYTICAL AND NUMERICAL SOLUTIONS FOR CYLINDRICAL BLAST WAVES IN A PLASMA OF VARYING DENSITY; Bishun D. Pandey, The Ohio State University, Marion, Ohio 43302, U.S.A.

1988-095: A 30-CM DIAMETER XENON ION THRUSTER: DESIGN AND INITIAL TEST RESULTS; Y. Yamagiwa, Y. Takeshita, and H. Kawauchi, Toshiba Komukai Works, 1 Komukaitoshiba-cho, Saiwai-ku, Kawasaki, Japan;  H. Yoshida, Toshiba R & D Center, 4-1 Ukishima-cho, Kawasaki-ku, Kawasaki, Japan; D. Miyazaki and T. Higuchi, Toshiba Horikawa-cho Works, 72 Horikawa-cho, Saiwai-ku, Kawasaki, Japan; K. Miyazaki, S. Kitamura, Y. Hayakawa, and Y. Nakamura, National Aerospace Laboratory, 7-44-1 Jindaiji-higashimachi, Chofu, Tokyo, Japan

1988-096: PROPELLANT SELECTION CRITERIA FOR DEEP SPACE ELECTRICALLY PROPELLED MISSIONS; A. R. Martin and P. M. Latham, Culham Laboratory, Abingdon, Oxon OX14 3DB, England

1988-098: INERT GAS PERFORMANCE OF THE RIT 35 MAIN PROPULSION UNIT; K. H. Groh, H. W. Loeb, W. Schmidt, B. Schuetz, and F. Zarnitz, 1st Institute of Physics, Giessen University, Heinrich-Buff-Ring 16, D-6300 Giessen, FRG

1988-099: CHARACTERISTICS OF FREE-FLOATING NITROGEN AND HELIUM PLASMAS GENERATED IN A MICROWAVE RESONANT CAVITY; Phillip Balaam, William Maul, and Michael M. Micci, Department of Aerospace Engineering, The Pennsylvania State University, University Park, PA 16802

1988-100: NUMERICAL AND EXPERIMENTAL INVESTIGATIONS OF A PROPATING MICROWAVE – HEATED PLASMA; Juergen Mueller and Michael M. Micci, Department of Aerospace Engineering, The Pennsylvania State University, University Park, PA

1988-101: EXPERIMENTS AND ANALYSIS OF A COMPACT ELECTROTHERMAL THRUSTER; Jes Asmussen, Professor, Department of Electrical Engineering, Michigan State University, East Lansing, MI, USA 48824-1226; and Stan Whitehair, Research Engineer, IBM, T.S. Watson Research Center, Yorktown Hts., NY, USA 10598

1988-103: ELECTROTHERMAL THRUSTERS UTILIZING ELECTRODELESS DISCHARGES; H. Tahara, Y. Tanaka, K. Onoe, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka 560, Japan

1988-104: PERFORMANCE CALCULATION OF AN H2 ARCJET BY MEANS OF A DUAL CHANNEL MODEL; H. O. Schrade and P. C. Sleziona, Universität Stuttgart, Institut für Raumfahrtsysteme

1988-105: NUMERICAL STUDIES OF THE FLOW FIELD IN A DC ARCJET THRUSTER; Michio NISHIDA, Department of Aeronautical Engineering, Kyoto University, Kyoto 606, Japan; Keiji KAITA, Kashima Steel Works, Sumitomo Metals Corporation, Kashima-cho, Ibaraki 314, Japan; and Ken-ichi TANAKA, Central Research Laboratory, Mitsubishi Electric Corporation, Amagasaki, Hyogo 661, Japan

1988-106: COMPUTATIONAL INVESTIGATION ON THE CHARACTERISTICS OF A LOW POWER DC ARCJET THRUSTER; Ken-ichi TANAKA and Kazuo TSUCHIYA, Central Research Laboratory, Mitsubishi Electric Corporations, Amagasaki, Hyogo 661, Japan; Keiji KAITA and Michio NISHIDA, Department of Aeronautical Engineering, Kyoto Univerity, Kyoto, 606 Japan

1988-107: A 15 KW EXPERIMENTAL ARCJET; H. L. Kurtz, M. Auweter-Kurtz, B. Glocker, W. Merke, and H. O. Schrade, Institut  für Raumfahrtsysteme, Universität Stuttgart, Stuttgart, West Germany

1988-108: OPERATING CHARACTERISTICS OF 1 kW HYDRAZINE ARCJET THRUSTER; T. Yoshikawa, K. Onoe, H. Yoshida, and S. Kotani, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka 560, Japan; and H. Suzuki and K. Uematsu, Ishikawajima-Harima Heavy Industries Co. Ltd.

1988-109: EXPERIMENTAL INVESTIGATION ON THE CHARACTERISTICS OF A LOW POWER DC ARCJET THRUSTER; Ken-ichi TANAKA and Kazuo TSUCHIYA, Central Research Laboratory, Mitsubishi Electric Corporation, Amagasaki, Hyogo 661, Japan; and Keiji KAITA and Michio NISHIDA, Department of Aeronautical Engineering, Kyoto University, Kyoto 606, Japan

1988-112: OPTICAL EMISSION SPECTRUM OF THE UK-10 ION THRUSTER OPERATING ON XENON; P. M. Lathem, A. R. Martin and M. T. Cresdee, Culham Laboratory, Abingdon, Oxon OX14 3DB, England

1988-113: DIAGNOSTIC TOOLS FOR AN ION THRUSTER IN SPACE; G. L. Wrenn, K. A. Ryden and D. G. Fearn, Space Department, Royal Aerospace Establishment, Farnborough, Hants, GU14 6TD, U.K.; A. R. Martin and P. M. Latham, UKAEA Culham Laboratory, Abingdon, Oxon, OX14 3DB, U.K.; and D. R. Rodgers, D. M. Walton, and A. D. Johnstone, UCL Mullard Space Science Laboratory, Holmbury St. Mary, Dorking, Surrey RH5 6NT, U.K.

1988-114: STEADY STATE MPD DEVICES FOR REENTRY SIMULATION; M. Auweter-Kurtz, J. Epple, H. Habiger, H. Kurtz, O. Loesener, E. Messerschmid, and D. Mulzer, Institut  für Raumfahrtsysteme Universität Stuttgart

1988-116: A 6 CM DIAMETER ION SOURCE FOR ASSISTANT DEPOSITION; Kuang Yuan-Zhu, and Feng Yu-Cai, Space Science and Technology Center, Academia Sinica, P.O. Box 2703, Beijing, China

1988-117: DEVELOPMENT OF HIGH-CURRENT RF-PLASMA SOURCES FOR NEUTRAL PARTICLE INJECTORS; J. Freisinger, H. Hellmann, M. Kaufmann, H. W. Loeb, and A. Scharmann, 1st Institute of Physics, Giessen University, Heinrich-Buff-Ring 16, D-6300 Giessen, FRG; and W. Kraus, Max-Planck-Institute of Plasma Physics, Boltzmannstrasse 2, D-8046 Garching, FRG

1988-118: NON-PROPULSIVE APPLICATION OF THE RF-ION THRUSTER FOR MATERIAL PROCESSING WITH REACTIVE GASES; J. Freisinger, K. Groh, J. Krempel-Hesse, J. M. Krumeich, H. W. Loeb, A. Scharmann, and H. W. Velten; 1st Institute of Physics, Giessen University, Heinrich-Buff-Ring 16, D-6300 Giessen, FRG

1988-119: THE USE OF ELECTRIC PROPULSION TECHNIQUES FOR LEO ATOMIC OXYGEN SIMULATION; M. A. Kinnersley and J. P. W. Stark, University of Southampton, England

1988-120: PERFORMANCE RESEARCH OF XENON ION ROCKET ENGINE; N. H. Wang, G. F. Wu, Z. Y. Guo, J. Z. Han, J. M. Qin, N. Wang, W. G. Wang, and Y. D. Chen, Chinese Academy of Space Technology, Lanzhou Institute of Physics, P. O. Box 94, Lanzhou, China

1988-124: KREM: A MODEL FOR EVALUATING ORBITAL TRANSFER VEHICLES UTILIZING NUCLEAR ELECTRIC PROPULSION SYSTEMS; W. F. Lyon, Research Associate, Advanced Nuclear Fuels Laboratory, Department of Nuclear Engineering, Texas A&M University, College Station, Texas, United States of America

1988-125: CAPACITORS FOR PULSED ELECTRIC PROPULSION, Rolf Dethlefsen and Joel Ennis, Maxwell Laboratories, Inc., 8888 Balboa Avenue, San Diego, California 92123, USA

1988-126: A TANDEM MIRROR HYBRID PLUME PLASMA PROPULSION FACILTIY; F. R. Chang-Diaz, T. F. Yang, W. A. Krueger, S. Peng, J. Urbahn, X. Yao, and D. Griffin, M.I.T. Plasma Fusion Center, Cambridge, Massachuesetts, 02139, Astronaut Office, NASA, Lyndon B. Johnson Space Center, Houston, Texas 77058, United States of America

1988-127: FIELD EMISSION ELECTRIC PROPULSION (FEEP): EXPERIMENTAL INVESTIGATIONS ON CONTINUOUS AND PULSED MODES OF OPERATION; C. Petagna, H. von Rohden, and C. Bartoli, ESA/ESTEC Technical Directorate, Noordwijk, The Netherlands; and D. Valentian, SEP, Vernon, France

1988 FILE DIRECTORY

IEPC1988-001.pdf  14:19  5.9M

IEPC-1988-002.pdf  14:20  4.5M

IEPC1988-003.pdf  14:20  6.0M

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1991 INDEX

1991-001: REVIEW OF EUROPEAN ACTIVITIES ON ELECTRIC PROPULSION; C. Bartoli, ESA Technical Directorate, ESTEC, Noordwijk, The Netherlands

1991-002: AN OVERVIEW OF THE NASA ELECTRIC PROPULSION PROGRAM; Francis M. Curran, Gary L. Bennett, and Marcus A. Watkins, NASA Headquarters, Office of Aeronautics, Exploration, and Technology, Washington, D.C. 20546; David C. Byers, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135; and John R. Brophy and Joel C. Sercel, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109

1991-003: STATE OF WORKS ON ELECTRICAL THRUSTERS IN THE USSR; A. S. Bober, Enterprise “Fakel”; V. P. Kim and G. A. Popov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute; A. S. Koroteev, Research Institute of Thermal Processes; L. A. Latyshev, Moscow Aviation Institute; A. I. Morozov, Institute of Atomic Energy named after I. V. Kurchatove; Yu P. Rylov, All-Union Research Institute of Electromechanics; and V. V. Zhurin, Institute of Earth Magnetism and Wave Propagation, of USSR AcSci

1991-004: ELECTRIC PROPULSION RESEARCH AND DEVELOPMENT IN JAPAN; T. Yoshikawa, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka, Japan

1991-005: REVIEW OF PLASMA PROPULSION ACTIVITIES IN ITALY; W. D. Deininger, BPD Difesa E Spazio, Colleferro (Roma) Itally; M. Andrenucci, Centrospazio, Pisa, Italy, G. Paccani, University of Rome, Rome, Italy, A. Trippi, ESA/ESTEC, Noordwijk, The Netherlands; and F. Rossi, ASSI, Rome, Italy

1991-006: THE STATUS AND FUTURE PLANS FOR ELECTRIC PROPULSION DEVELOPMENT BY THE UNITED STATES AIR FORCE; Capt. Terry M. Sanks, USAF, OLAC Phillips Laboratory, Edwards Air Force Base, CA 93525-5000; Lt. Barry Raygor, USAF, Space Systems Division AFSC, Los Angeles Air Force Base, CA 90009-2960; and Dr. Mitat A. Birkan, Air Force Office of Scientific Research, Bolling Air Force Base, Washington D.C. 00000-0000

1991-007: THE ADVANCED SPACE PROPULSION PROGRAMMES AT AEA TECHNOLOGY, CULHAM LABORATORY; R. A. Bond, A. R. Martin, and S. D. Watson, Space Applications Department, AEA Technology, Culham Laboratory, Abingdon, Oxon OX14 3DB, United Kingdom

1991-009: THE UK-10 ION PROPULSION SYSTEM – A TECHNOLOGY FOR IMPROVING THE COST-EFFECTIVENESS OF COMMUNICATION SPACECRAFT; D. G. Fearn, Space Department, Royal Aerospace Establishment, Farnborough, Hampshire, UK

1991-010: 18-mN XENON ION PROPULSION SUBSYSTEM; J. R. Beattie, R. R. Robson, and J. D. Williams, Hughes Research Laboratories, Malibu, California 90265, USA

1991-013: HYDRAZINE ARCJET PROPULSION SYSTEM INTEGRATION TESTING; Sidney Zafran, Space & Technology Group, TRW Inc., Redondo Beach, CA 90278

1991-014: FINAL RESULTS OF 15 kWe WATER-COOLED ARCJET TESTING; E. Tosti, BPD Difesa e Spazio, Colleferro, Italy; B. Glocker, Institut  für Raumfahrtsysteme Universität Stuttgart, Germany; and A. Trippi, ESA/ESTEC, Noordwijk, The Netherlands

1991-015: EXPERIMENTAL AND NUMERICAL STUDIES OF A 10-kW WATER-COOLED ARCJET THRUSTER; H. Tahara, T. Sakakibara, K. Onoe, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka, Japan

1991-016:  MEDIUM POWER ARCJET ANALYSIS AND EXPERIMENTS; B. Glocker, Th. Rösgen, Institut  für Raumfahrtsysteme Universität Stuttgart; and A. Laxander, Institut  für Computeranwendungen, Universität Stuttgart

1991-018: HYDROGEN ARCJET TECHNOLOGY; John M. Sankovic, John A. Hamley, Thomas W. Haag, Charles J. Sarmiento, and Francis M. Curran, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135

1991-019: A REVIEW OF THE THEORY OF SELF-FIELD MPD THRUSTERS; J. L. Lawless, Space Power Inc., San Jose, CA 94134; and V. V. Subramaniam, Department of Mechanical Engineering, The Ohio State University, Columbus, Ohio 43210-1107

1991-020: LOCAL ANALYSES IN MPD THRUSTER: MAGNETODYNAMIC REGIMES; J. Marc, G. Chanty, and M. Martinez-Sanchez, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139, U.S.A.

1991-021: ONSET AND EROSION IN SELF-FIELD MPD THRUSTERS; V. V. Subramaniam, Department of Mechanical Engineering, The Ohio State University, Columubs, Ohio 43210, U.S.A.

1991-022: THE ONSET PHENOMENA EXPLAINED BY RUN-AWAY JOULE HEATING; Herbert O. Schrade, Thomas Wegmann, and Thomas Rosgen, Institut für Raumfahrtsysteme Universität Stuttgart, Germany

1991-023: THE DEVELOPMENT OF THE CATHODES-COMPENSATORS FOR STATIONARY PLASMA THRUSTERS (SIT) IN USSR; B. A. Arkhipov and K. N. Kozubsky, Enterprise “Fakel, Kaliningrad (obl), USSR

1991-024: DESIGN CONSOLIDATION AND SPACE (PRE)QUALIFICATION OF A PLASMA BRIDGE NEUTRALIZER FOR THE RITA 10 ION THRUSTER; M. Bianconi, G. F. Cirri, G. Matticari, and A. Severi, Proel Tecnologi – Firenze, Italy

1991-025: EVALUATION OF ION THRUSTER BEAM NEUTRALIZATION; S. Shimada, Y. Gotoh, E. Nishida, and H. Takegahara, Space Systems Department, Kamakura Works, Mitsubishi Electric Corporation, Kamakura, Japan; and K. Nakamaru, H. Nagano, and K. Terada, National Space Development Agency of Japan, Minato-ku, Tokyo, Japan

1991-026: ENDURANCE TEST OF PROEL NEUTRALIZER FOR THE RIT 10: REVIEW OF THE ACTIVITIES AT ESTEC LABORATORIES; H. V. Rohden, ESA/ESTEC – Electric Propulsion Unit, Noordwijk, The Netherland; and G. F. Cirri and G. Matticari, Proel Tecnologie, Firenze, Italy

1991-027: POWER SUPPLY AND CONTROL UNIT FOR RADIOFREQUENCY ION THURSTER RIT; P. Cesa, FIAR SpA Space Division, Corso Milano, 94 Padova, Italy; and S. Gandini, P. Leoni, and G. Passoni, FIAR SpA Space Division, Via Montefeltro, 8 Milano, Italy

1991-028: OPERATING LIMITS OF POWER CONVERTERS FOR HIGH POWER ION ENGINE CONTROL; A. J. Forsyth, P. D. Evans, K. W. E. Cheng, and M. R. D. Al-Mothafar, University of Birmingham, U.K., B15 2TT

1991-029: DEVELOPMENT OF A POWER CONDITIONER UNIT OF A 1-kW ARCJET; M. Andrenucci, University of Pisa, Pisa, Italy; and M. Sandrucci, CENTROSPAZIO, Pisa, Italy

1991-030: TESTING OF THE 30 kW ARCJET PCU STARTER USING THE SHORTING SWITCH APPROACH; See-pok Wong, Manager, Electrical Systems, Space Power, Inc., 621 River Oaks Parkway, San Jose, CA 95134

1991-031: PERFORMANCE MEASUREMENTS OF A RESONANT CAVITY ELECTROTHERMAL THRUSTER; Philip Balaam and Michael M. Micci, Department of Aerospace Engineering, The Pennsylvania State University, University Park, PA 16802

1991-032: THEORETICAL MODELING OF DIAGNOSTIC EVALUATIONS OF MICROWAVE GENERATED PLASMA SYSTEMS; Scott S. Haraburda, Department of Chemistry, United States Military Academy, West Point, New York, 10996; Martin C. Hawley and Duane W. Dinkel, Department of Chemical Engineering, Michigan State University, East Lansing, Michigan, 48824

1991-033: DESIGN AND PERFORMANCE CHARACTERISTICS OF A NEW MICROWAVE ELECTROTHERMAL THRUSTER; Juergen Mueller and Michael M. Micci, Department of Aeropsace Engineering, The Pennsylvania State University, University Park, PA, USA

1991-034: THE EFFECT OF MOLECULAR PROPELLANTS ON THE PERFORMANCE OF A RESONANT CAVITY ELECTROTHERMAL THRUSTER; D. J. Sullivan and M. M. Micci, Department of Aerospace Engineering, The Pennsylvania State University, University Park, PA, USA

1991-035: NUCLEAR ELECTRIC PROPULSION FOR FUTURE NASA SPACE SCIENCE MISSIONS; Chen-wan L. Yen and Carl G. Sauer, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1991-036: THE ULYSSES MISSION: THE ION PROPULSION ALTERNATIVE; D. G. Fearn, Space Department, Royal Aerospace Establishment, Farnborough, Hampshire, UK

1991-037: MISSION STUDY OF MARS/VENUS PROBES DRIVEN BY ELECTRIC PROPULSION; Hitoshi Kuninaka, Institute of Space and Astronautical Science, Yoshinodai, Sagamihara, Kanagawa 229, Japan

1991-038: MISSION AND SYSTEM OPTIMIZATION OF NUCLEAR ELECTRIC PROPULSION VEHICLES FOR LUNAR AND MARS MISSIONS; James H. Gilland, Sverdrup Technology, Inc. NASA Lewis Research Center, Brookpark, Ohio

1991-039: SYSTEMS ENGINEERING OF A NEP ROCKET TO THE MOON AND MARS; Dr. John A. Dearien, Idaho National Engineering Laboratory, Idaho Falls, Idaho; M. P. Doherty, J. A. George, and J. S. Sovey, NASA – Lewis Research Center, Cleveland, Ohio

1991-040: TO PLANETS USING NUCLEAR-ELECTRIC THRUST TO L1, THEN CHEMICAL TO OBTAIN LUNAR FUEL, SHIELDING, SUPPLIES, AND EARTH GRAVITY ASSIST; Thomas M. Morse, Consultant, Mooresville, N.C. 28115, USA

1991-041: IGNITION STABILTY OF A LOW POWER ARCJET; T. Yamada, Y. Iwamoto, Y. Shimizu, K. Toki, and K. Kuriki, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229, Japan

1991-042: DEVELOPMENT OF A LOW POWER RADIATIVELY COOLED THERMAL ARCJET THRUSTER; D. M. Zube, B. Glocker, and H. L. Kurtz, Institut für Raumfahrtsysteme Universität Stuttgart, 7000 Stuttgart 80, F. R. Germany; M. Kinnersley and G. Matthäus, MBB-ERNO Raumfahrttechnik GmBH, 2800 Bremen, F.R. Germany

1991-043: DEVELOPMENT OF A LOW POWER ARCJET THRUSTER: THRUST PERFORMANCE AND LIFE EVALUATION; T. Yoshikawa, K. Onoe, and S. Tsuri, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka 560, Japan; M. Ishil and K. Uematsu, Ishikawajima Harima Heavy Industries Co. Ltd., Isogo, Yokohama, Kanagawa 235, Japan

1991-044: ADVANCED LABORATORY MODEL, 1 kW-CLASS ARCJET ENGINE TESTING; G. Cruciani, M. J.  Glogowski, and W. D. Deininger, BPD Difesa e Spazio, Collefero (Roma), Italy; and A. Trippi, ESA/ESTEC, Noordwijk, The Netherlands

1991-045: PERFORMANCE STUDY OF A LABORATORY MODEL OF LOW POWER ARCJET; M. Andrenucci, University of Pisa, Pisa, Italy; G. Saccoccia, ESTEC, Noordwijk, The Netherlands, F. Scortecci, N. Panattoni, U. Schulz, CENTROSPAZIO, Pisa, Italy; and W. D. Deininger, BPD Difesa e Spazio, Colleferro, Italy

1991-047: PLASMA DIAGNOSTICS IN MPD THRUSTER PLUMES; M. Andrenucci, F. Paganucci, A. Venturini, and A. Turco, CENTROSPAZIO, Pisa, Italy; and G. Paccani, University of Rome, Italy

1991-048: OPTICAL MEASUREMENT OF VELOCITY DISTRIBUTIONS IN MPD ARCJET; T. Nakayama, T. Yoshida, K. Toki, and K. Kuriki, Institute of Space and Astronautical Science, Kanagawa, Japan

1991-049: MPD THRUSTER EXHAUST VELOCITY MEASUREMENT USING INJECTED PLASMA WAVES; K. D. Diamant, D. L. Tilley, E. Y. Choueiri, A. J. Kelly, and R. G. Jahn, Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Princeton, NJ 08544

1991-052: IONIZATION PROCESSES IN THE INTERELECTRODE REGION OF AN MPD THRUSTER; T. M. Randolph, W. F. von Jaskowsky, A. J. Kelly and R. G. Jahn, Electric Propulsion Laboratory, Princeton, University, Princeton, NJ 08544

1991-053: MISSION AND OPERATION ASPECTS OF IN-ORBIT ION PROPULSION MANAGEMENT; L. Mazzini and A. Notarantonio, Alenia Spazio S.p.A. Rome, Italy; and S. Falzini and F. Palutan, Space Engineering, S.r.l., Rome, Italy

1991-054: INTEGRATION OF ION PROPULSION TECHNOLOGY IN A SYNCHRONOUS SATELLITE: THE ARTEMIS CHALLENGE; M. SilvI, Alenia Spazio S.p.A., and H. Kellermeier, M.B.B.

1991-055: ION PROPULSION PACKAGE FOR N/S – STATIONKEEPING OF THE ARTEMIS SATELLITE; H. Bassner, H. P. Berg, K. Fetzer, and G. Müller, Deutsche Aerospace, Messerschmitt Bölkow Blohm, Space Communications and Propulsion Systems Division, Munich, Germany

1991-056: THE UK-10 ION THRUSTER TEST PROGRAMME AT AEA TECHNOLOGY, CULHAM LABORATORY; Staff of the Space Applications Department (Principal Author S. D. Watson), AEA Technology, Culham Laboratory, Abingdon, Oxon OX14 3DB, United Kingdom

1991-057: RITA DEVELOPMENT AND FABRICATION FOR THE ARTEMIS SATELLITE; H. Bassner, H. P. Berg, and R. Kukies, Deutsche Aerospace, Messerschmitt Bölkow Blohm GMBH, Space Communications and Propulsion Systems Division

1991-058: DESIGN OF AN MPD ARCJET FOR OPERATION AT GIGAWATT POWER LEVELS; P. J. Turchi, The Ohio State University, Columbus, Ohio, USA

1991-059: BASIC EQUATIONS AND ELEMENTS OF THE DISPERSION RELATION FOR A FOUR-FLUID FORMALISM OF MAGNETO-PLASMADYNAMICS WITH NON-EQUILIBRIUM IONIZATION; H. J. Kaeppeler, Institut für Plasmaforschung der Universität Stuttgart. F. R. Germany

1991-060: VISCOUS AND DIFFUSIVE EFFECTS IN ELECTROTHERMAL AND MPD ARCJET THRUSTERS; S. Miller and M. Martinez-Sanchez, Space Power and Propulsion Laboratory, Dept. of Aeronautics and Astronautics, MIT, Cambridge, MA 02139

1991-061: QUASI ONE-DIMENSIONAL IONIZING MPD FLOW; G. Lefever-Button and V. V. Subramaniam, Department of Mechanical Engineering, The Ohio State University, Columbus, Ohio 43210, U.S.A.

1991-062: THRUST FORMULA FOR AN APPLIED-FIELD MPD THRUSTER DERIVED FROM ENERGY CONSERVATION EQUATION; Akihiro Sasoh, Institute of Fluid Science, Tohoku University, Sendai, Japan; and Yoshihiro Arakawa, Department of Aeronautics, University of Tokyo, Tokyo, Japan

1991-063: A FLIGHT TEST OF THE ALLEVIATION OF SPACECRAFT CHARGING USING A UK-10 ION THRUSTER CATHODE; N. C. Wallace, Space Department, Defence Research Agency, Aerospace Division, Farnborough, Hampshire, U.K.

1991-064: PLASMA CONTRACTOR FOR THE ISTP/POLAR SPACECRAFT; R. R. Robson and W. S. Williamson, Hughes Research Laboratories, Malibu, California 90265; R. C. Olsen, Naval Postgraduate School, Monterey, California 93943; and T. E. Moore, NASA, Marshall Spaceflight Center, Huntsville, Alabama 35812

1991-065: A METAL-ION IMPLANTER BASED ON ION-THRUSTER TECHNOLOGY; Paul J. Wilbur and Ronghua Wei, Department of Mechanical Engineering, Colorado State University, Fort Collins, Colorado

1991-066: THE RF-ION SOURCES ‘RIM’ AND ‘PRIS’ FOR MATERIAL PROCESSING AND SURFACE MODIFICATION; M. Bisten, J. Freisinger, J. Heland, J. Krempel-Hesse, J. Krumeich, H.Löb, and P. Neumann, 1st Institute of Physics, Giessen University, Heinrich-Buff-Ring 16, D-6300 Giessen, FRG

1991-067: ELECTRIC PROPULSION APPLICATIONS IN PLASMA-DRIVEN ELECTROMAGNETIC RAILGUNS; B. Azzerboni, Istituto di Elettrotecnica ed Elettronica, V. le A. Dorica 6, 95125 Catania; and E. Cardelli, M. Raugi, and A. Tellini, Dipartimento di Sistemi Elettrici ed Automazione, Via Diotisalvi 2, 56100 Pisa

1991-068: ENDURANCE TEST OF AN AMMONIA ARCJET AT 10 kWe; J. E. Polk and K. D. Goodfellow, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1991-070: TESTING OF 30 kW ARCJET PCU WITH ARCJET THRUSTERS; See-pok Wong, Manager, Electrical Systems, Space Power, Inc., 621 River Oaks Parkway, San Jose, CA 95134

1991-071: ACOUSTICAL RESONANT BEHAVIOR AND V-1 CURVES FOR A 30 kWe NITROGEN ARCJET; Montgomery D. Grimes, Southwest Research Institute, San Antonio, TX 78228; and William J. Harris, Edgar A. O’Hair, Lynn L. Hatfield, Magne Kristiansen, and Mary C. Baker; Pulsed Power Laboratory, Texas Tech University, Lubbock, TX 79409

1991-072: HIGH POWER ARCJET THRUSTER EXPERIMENTS; T. M. Gölz, M. Auweter-Kurtz, H. L. Kurtz, and H. O. Schrade; Institut für Raumfahrtsysteme Universität Stuttgart

1991-073: PERFORMANCE CHARACTERISTICS AND DISCHARGE FEATURES OF A QUASI-STEADY APPLIED-FIELD MPD ARCJET; H. Tahara, F. Takiguchi, Y. Kagaya, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka, Japan

1991-074: AN EXPERIMENTAL AND NUMERICAL INVESTIGATION OF AN APPLIED-FIELD MAGNETOPLASMADYNAMIC SPACE PROPULSION ENGINE; Thomas J. Pivirotto and Keith D. Goodfellow, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California, USA

1991-075: CONTINUOUS OPERATIONAL TESTS OF A QUASI-STEADY MPD ARCJET SYSTEM: THERMAL AND PERFORMANCE CHARACTERISTICS; T. Yoshikawa, Y, Kagaya, and K. Onoe, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka 560, Japan

1991-076: PRELIMINARY TEST RESULTS OF A HOLLOW CATHODE MPD THRUSTER; M. A. Mantenieks, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135; and R. M. Myers, Sverdrup Technology, Inc., Lewis Research Center Group, Brook Park, Ohio 44142

1991-078: PLASMA ACCELERATION PROCESS IN A HALL-CURRENT THRUSTER; Kimiya Komurasaki, Miharu Hirakawa, and Yoshihiro Arakawa, Department of Aeronautics, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Toyoko, Japan

1991-079:  PHYSICAL …. AND CHARACTERISTICS OF STATIONARY PLASMA THRUSTERS WITH CLOSED ELECTRONS DRIFT; A. I. Bugrova, Moscow Institute of Radioelectronics and Automatics, Moscow, USSR; V.P. Kim; Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute, Moscow, USSR; N. A. Maslennikov; Enterprise “Fakel”, Kaliningrad, USSR; and A. I. Morozov, Institute of Atomic Energy Named After I. V. Kurchatov, Moscow, USSR.

1991-080: THE STATE OF RESEARCH AND DEVELOPMENT OF END-HALL PLASMA THRUSTERS IN THE USSR; V. V. Zhurin, Front Range Research, Fort Collins, Colorado; A. G. Popov, A. A. Porotnikov, and V. B. Tikhonov, Moscow Aviation Institute, Moscow; and Iu. A. Utkin, Research Institute for Thermal Processes, Moscow

1991-081: RESEARCH OF ION THRUSTERS IN THE USSR; V. N. Korovkin, Scientific Research Assotiation “Verter”, Kalliningrad, USSR; L. A. Latyshev and V. G. Grigoryan, Moscow Aviation Institute, Moscow, USSR; V. A. Obukhov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute Moscow, USSR

1991-082: RECENT PERFORMANCE RESULTS OF THE RIT 15 AUXILIARY PROPULSION ENGINE; K. H. Groh, N. Kreiling, H. W. Loeb, Th. Schmidkunz, and F. Zarnitz; 1st Institute of Physics, Giessen University, D-6300 Giessen, FRG

1991-083: BEAM DIAGNOSTICS FOR THE CHARACTERIZATION OF ION THRUSTER BEAM PARAMETERS; K. H. Groh, N. Kreiling, H. W. Loeb, Th. Schmidkunz; Ist Institute of Physics, Giessen University, D-6300 Giessen, FRG

1991-084: MICROWAVE ION THRUSTER WITH ELECTRON CYCLOTRON RESONANCE DISCHARGE; H. Miyoshi, S. Ichimura, H. Kuninaka, and K. Kuriki; Institute of Space and Astronautical Science, Yoshinodai, Sagamihara, Kanagawa, Japan; and Y. Horiuchi, NEC Corporation, Ikebe-cho, Midori-ku, Yokohama, Kanagawa, Japan

1991-085: PERFORMANCE CHARACTERISTICS OF A MICROWAVE ION THRUSTER USING A RESONANT CAVITY; T. Yasui, H. Tahara, K. Onoe, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka, Japan

1991-087: MPD THRUSTER CALCULATION CONSIDERING HIGH IONIZATION MODES; P. C. Sleziona, M. Auweter-Kurtz, and H. O. Schrade, Institut für Raumfahrtsysteme Universität Stuttgart, FRG

1991-088: IONIZATIONAL IGNITION AT THE INLET OF AN MPD THRUSTER; E. J. Sheppard and M. Martinez-Sanchez, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139, U.S.A.

1991-089: PRE-IONIZATION PROCESSES IN A SELF-FIELD MPD ACCELERATOR; Rodney L. Burton and Nicholas Tiliakos, Department of Aeronautical and Astronautical Engineering, University of Illinois at Urbana-Champaign, Urbana, IL 61801

1991-091: OPTICAL DIAGNOSTICS OF A LOW POWER HYDROGEN ARCJET; M. A. Cappelli, R. K. Hanson, J. G. Liebeskind, and D. H. Manzella, Stanford University, High Temperature Gasdynamics Laboratory, Department of Mechanical Engineering, Stanford, CA 94305, U.S.A.

1991-092: PLUME ANALYSIS OF A 10 kWe/N ARCJET USING EMISSION SPECTROSCOPY; E. Tosti and W. D. Deininger, BPD Difesa e Spazio, Colleferro, Italy

1991-093: LASER FLUORESCENCE VELOCIMETRY OF AN ARCJET EXHAUST PLUME; Wilhelmus M. Ruyten, University of Tennessee-Calspan, Center for Space Transportation and Applied Research, UTSI Research Park, Tullahoma, Tennessee 37388; Dennis Keefer, Center for Laser Applications, University of Tennessee Space Institute, Tullahoma, Tennessee 37388

1991-095: ADVANCED DIAGNOSTICS OF ARCJETS; M. W. Crofton, R. P. Welle, S. W. Janson, and R. B. Cohen, The Aerospace Corporation, Los Angeles, CA 90009

1991-096: EROSION PROCESSES IN THE UK-25 ION THRUSTER; P. M. Latham, A. J. Pearce, and R. A. Bond, Space Applications Department, AEA Technology, Culham Laboratory, Abingdon, OXON OX14 3DB, United Kingdom

1991-097: METAL AND METAL NITRIDE EROSION RATES IN A DIVERGENT FIELD ION ENGINE; Charles E. Garner, John R. Brophy, and L. C. Pless, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

1991-098: EROSION RATE DIAGNOSTICS IN ION THRUSTERS USING LASER-INDUCED FLUORESCENE; C. J. Gaeta, R. S. Turley, J. N. Matossian, J. R. Beattie, W. S. Williamson, and J. D. Williams, Hughes Research Laboratories, Malibu, CA 90265

1991-099: THE HALL EFFECT IN A NUMERICAL MODEL OF MPD THRUSTERS; E. H. Niewood and M. Martinez-Sanchez, Space Power and Propulsion Laboratory, Dept. of Aeronautics and Astronautics, MIT, Cambridge, MA 02139

1991-100: CURRENT-DRIVEN PLASMA ACCELERATION VERSUS CURRENT-DRIVEN ENERGY DISSIPATION PART II: ELECTROMAGNETIC WAVE STABILITY THEORY AND EXPERIMENTS; E. Y. Choueiri, A. J. Kelly, and R. G. Jahn, Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Princeton, NJ 08544, USA

1991-101: GRADIENT INFLUENCED SPACE CHARGE INSTABILITIES IN MPD THRUSTERS; H. P. Wagner, M. Auwetere-Kurtz, E. W. Messerschmid, Institut für Raumfahrtsysteme (IRS); H. J. Kaeppeler, Institut für Plasmaforschung (IPF), Universität Stuttgart, FRG

1991-102: AN MPD CODE WITH ANOMALOUS TRANSPORT; G. Caldo, E. Y. Choueiri, A. J. Kelly, and R. G. Jahn, Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Princeton, New Jersey 08544, USA

1991-103: EXPERIMENTAL STUDY OF FEEP EMITTER STARTING CHARACTERISTICS; M. Andrenucci, University of Pisa, Pisa, Italy; S. Marcuccio, L. Spagli, A. Genovese, and F. Repola, CENTROSPAZIO, Pisa, Italy

1991-104: EXPERIMENTAL INVESTIGATION OF FIELD EMISSION ELECTROSTATIC THRUSTERS; A. Ciucci, Auburn University, Auburn, Al, USA; G. Genuini, CENTROSPAZIO, Pisa, Italy, and M. Andrenucci, University of Pisa, Pisa, Italy

1991-105: PROSPECTS OF LIQUID METAL ION THRUSTERS FOR ELECTRIC PROPULSION; J. Mitterauer, Technische Universität Wien Institut für Allgemeine Elektrotechnick und Elektronik, Gusshausstrasse 27-29, 1040 Wien, Austria

1991-106: THERMIONIC SYSTEMS FOR NUCLEAR ELECTRIC PROPULSION; Thomas H. Van Hagan, General Atomics, P.O. Box 85608, San Diego, California, USA 92186-9784

1991-107: PROPELLANT STORAGE CONSIDERATIONS FOR ELECTRIC PROPULSION; Richard P. Welle, The Aerospace Corporation, Los Angeles, CA 90009

1991-108: A LIGHTWEIGHT LIQUID HYDROGEN STORAGE SYSTEM FOR ELECTRICAL ORBITL TRANSFER VEHICLE APPLICATION; T. M. Miller and E. C. Cady, McDonnell Douglas Space Systems Company, Huntington Beach, California

1991-109: MASS FLOW CONTROLLER OF ION ENGINE SYSTEM; S. Shimada, Y. Gotoh, and H. Takagahara, Space Systems Department, Kamakura Works, Mitsubishi Electric Corporation, Kamakura, Kanagawa, Japan; and H. Nagano, National Space Development Agency of Japan, Minato-ku, Tokyo, Japan

1991-110: MOEDLLING ARCJET THRUSTER PERFORMANCE; R. Spurrett and R. A. Bond, AEA Technology, Culham Laboratory, Abingdon, Oxon OX14 3DB, United Kingdom

1991-111: COMPARISON OF MODEL CALCULATIONS WITH EXPERIMENTAL DATA FROM HYDROGEN ARCJETS; Robert Rhodes and Dennis Keefer, Center for Laser Applications, University of Tennessee Space Institute, Tullahoma, TN 37388

1991-112: NUMERICAL STUDIES OF THE FLOW FIELD IN A LOW POWER DC ARCJET THRUSTER USING NAVIER-STOKES EQUATIONS; Hiroyuki Okamoto and Michio Nishida, Department of Aeronautical Engineering, Kyushu University, Fukouka 812, Japan; and Ken-ichi Tanaka, Central Research Laboratory, Mitsubishi Electric Corporation, Hyougo 661, Japan

1991-113: DEVELOPMENT OF A COMPUTER PROGRAMME OF THE ANALYSIS OF ARCJET NOZZLES; M. Andrenucci, University of Pisa, Pisa, Italy, F. Scortecci, G. Capecchi, and T. Wünsch, CENTROSPAZIO, Pisa, Italy

1991-114: OPERATION OF A PULSED ELECTROTHERMAL DEVICE WITH THE XRAM INDUCTIVE GENERATOR, J. Ashkenazy, R. Cerny, M. Kanter, and Z. Kaplan, Soreq Nuclear Research Center, Yavne 70600, Israel

1991-115: AN OPTIMAL DESIGN PROCEDURE FOR A PULSE FORMING NETWORK; E. Cardelli, N. Esposito, and M. Raugi, Dipartimento di Sistemi Elettrici ed Automazione, Via Diotisalvi 2, 56100 Pisa; and G. Tina, Dipartimento di Elettrotecnica ed Elettronica, Viale A. Doria 6, 95125 Catania

1991-118: A NUMERICAL CODE FOR CUSPED ION THRUSTERS; Yoshihiro Arakawa and Kazutomi Ishihara, Department of Aeronautics, University of Tokyo, Hongo, Tokyo, 113 Japan

1991-119: THREE-DIMENSIONAL PARTICLE SIMULATION OF GRID EROSION IN ION THRUSTERS; Xiaohang Peng, Wilhelmus M. Ruyten, and Dennis Keefer, Center for Space Transportation and Applied Research and University of Tennessee Space Institute, Tullahoma, Tennessee 37388

1991-120: VARIATIONS OF TRIPLE-GRID GEOMETRY AND POTENTIALS TO ALLEVIATE ACCEL GRID EROSION; B. Free, Scionics, inc. Derwood, MD, USA; J. R. Owens, INTELSAT, Washington, D.C. USA, and P. Wilbur, Colorado State University, Fort Collins, CO, USA

1991-121: ORBITAL CONTROL AND MANOEUVERING OF LIGHTSATS/SYNCHRONOUS SATELLITES: ASSESSMENT OF NEW ION PROPULSION TECHNOLOGIES, BASED ON THE ELECTRON CYCLOTRON RESONANCE PHENOMENON, TO IMPROVE THE PERFORMANCES OF THRUSTERS IN THE MILLINEWTON RANGE; G. Perrotta, Alenia Spazio, Via Saccomuro n. 24-00131 Roma (Italy); M. Bianconi, A. Bicci, M. Capacci, G. F. Cirri, and G. Matticari, Proel Technologie, Viale Machiavelli n. 29-50125 Firenze (Italy)

1991-122: AN INVESTIGATION OF MICROINSTABILITIES IN A kW LEVEL SELF-FIELD MPD THRUSTER; D. L. Tilley, E. Y. Choueiri, A. J. Kelly, R. G. Jahn, Electric Propulsion & Plasma Dynamics Lab, Princeton University, Princeton, NJ 08544

1991-123: SCALE EFFECTS ON THE PERFORMANCE OF MPD THRUSTERS; M. Andrenucci, University of Pisa, Pisa, Italy; F. Paganucci, M. Frazzetta, G. LaMotta, and G. Schianchi, CENTROSPAZIO, Pisa, Italy

1991-125: ANODE POWER DEPOSTITIOIN IN MPD THRUSTERS; A. D. Gallimore, A. J. Kelly, and R. G. Jahn, Electric Propulsion Laboratory, Princeton University, Princeton, New Jersey 08544

1991-126: EXPERIMENTAL COMPARISION OF ELECTRIC OF KINETIC ENERGY TRANSFORMATION EFFECTIVENESS IN ELECTRODISCHARGE AND ELECTRODYNAMIC SYSTEMS; F. G. Rutberg, A. I. Kulishevitch, G. M. Cherniavsky, and S. A. Kaliadin, Department of Physics and Technology, USSR Academy of Sciences, Leningrad, USSR

1991-127: FROM ANTI-GRAVITY TO ZERO-POINT ENERGY: A TECHNICAL REVIEW OF ADVANCED PROPULSION CONCEPTS; George D. Hathaway, Hathaway Consulting Services, 39 Kendal Ave., Toronto, Ontario, Canada M5R 1L5

1991-128: DESIGN CHARACTERISTICS OF THE VARIABLE ISP PLASMA ROCKET; F. R. Chang Diaz and T. F. Yang, M.I.T. Plasma Fusion Center, Cambridge, MA USA

1991-129: AN ICRF PLASMA HEATING EXPERIMENT IN THE TANDEM MIRROR PROPULSION DEVICE; T. F. Yang and S. Peng, MIT Plasma Fusion Center, Cambridge, MA 02139, USA; and F. R. Chang-Diaz, Astronaut Office, NASA, Lyndon B. Johnson Space Center, Houston, TX 77058, USA

1991-130: HIGH CURRENT PULSE HELIUM DISCHARGE AT HIGH PRESSURE; F. G. Bakst, A. M. Voronov, V. N. Zhuravlev, and F. G. Rutberg, VNIIElectromash, Leningrad

1991-132: A LOW ALTITUDE ION-PROPELLED REMOTE SENSING SPACECRAFT; J. Reale, Space Department, Defence Research Agency (Aerospace Division), Royal Aerospace Establishment, Farnborough, Hampshire, United Kingdom

1991-133: SYSTEMS ANALYSIS FOR AN OPERATIONAL EOTV; T. M. Miller, McDonnell Douglas Space Systems Company, Huntington Beach, California

1991-134: OPTIMAL ELECTRIC PROPULSION ORBITAL TRANSFER VEHICLE DESIGN; Y. A. Zakharov, Moscow Aviation Institute, Moscow, USSR

1991-143: PROBLEMS OF ELECTRIC PROPULSION ENDURANCE TESTS; V. I. Baranov, A. I. Vasin, and V. A. Petrosov, Research Institute for Thermal Processes, Moscow; and V. V. Zhurin, Front Range Research, Fort Collins, Colorado

1991-144: SYSTEM PROGRAMMATIC ASPECTS OF THE ION PROPULSION PACKAGE ONBOARD THE ARTEMIS SATELLITE; M. Protto, M. Silvi, S. Greco, Alenia Spazio, H. Kellermeier, M.B.B.

1991-145: ION ENGINE SYSTEM DEVELOPMENT OF ETS-VI; S. Shimada, K. Satoh, Y. Gotoh, E. Nishida, and H. Takegahara, Space Systems Department, Kamakura Works, Mitsubishi Electric Corporation, Kamakura, Kanagawa, Japan; K. Nakamaru, H. Nagano, and K. Terada, National Space Development Agency of Japan, Minato-ku, Tokyo, Japan

1991-146: ELITE PROGRAM OVERVIEW; Major Ed Avila, OLAC Phillips Laboratory, Edwards Air Force Base, CA 93525-5000

1991-147: DEVELOPMENT OF MPD ACRJET SYSTEM EM FOR SFU-1; Yukio Shimizu and Kyoichiro Toki, Institute of Space and Astronautical Science, Kanagawa, Japan, Hiroshi Suzuki, Kazuo Uematsu, Takenori Otsuka, and Kotaro Shiina, Ishikawajima-Harima Heavy Industries Co. Ltd., Tokyo, Japana, and Yoshinori Kunii, Mitsubishi Electric Co., Kanagawa, Japan

1991-149: APPLICATION AND REVIEW OF THE DEVELOPMENT OF THE CLOSED DRIFT HALL THRUSTER; Joseph R. Wetch, and John L. Lawless, International Scientific Products, San Jose, CA 95134; 408-434-9500; and A. S. Koroteev, The Scientific Research Institute of Thermal Processes, Moscow, USSR

1991-150: DERATED ION THRUSTER DESIGN ISSUES; Michael J. Patterson and Vincent K. Rawlin, National Aeronautics and Space Administration, Lewis Research Center

1991-151: NEUTRALIZER OPTIMIZATION; Michael J. Patterson, National Aeronautics and Space Administration, Lewis Research Center, and Kayhan Mohajeri, Department of Physics, Purdue University

1991-152: THE USE OF SUPERCONDUCTIN MAGNETS FOR PLASMA THRUSTERS; D. E. Gonzalez and G. r. Karr, The University of Alabama in Huntsville, Mechanical Engineering Dept., Huntsville, AL 35899

1991-153: THE ADVANCED PROPULSION SPACE TEST FACILITIES AT AEA TECHNOLOGY, CULHAM LABORATORY; M. S. Harvey & Staff of Space Applications Department, AEA Technology, Culham Laboratory, Abingdon, Oxon OX14 3DB, UK

1991-154: ELECTROSTATIC PROPULSION USING C60 MOLEULES; Stephanie D. Leifer, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109; and Winston A. Saunders, California Institute of Technology, Pasadena, CA 91125

1991-155: ARCJET TEST MISSION (ARTEMIS) ON EURECA; Dieter M. Zube, Bernd Glocker, Helmut L. Kurtz, and Ernst W. Messerschmid, Institut für Raumfahrtsysteme, Universität Stuttgart, 7000 Stuttgart 80, F. R. Germany


1991 FILE DIRECTORY

IEPC1991-001.pdf  18:16  7.5M

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IEPC1991-Front.Matter.pdf  18:12  7.8M

IEPC1991-Indexes.pdf  18:09  1.3M

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IEPC1991-Session.Reports.pdf  18:14   27M

IEPC1991-TOC.pdf  18:08  201K

1993 INDEX

1993-001: DEVELOPMENT AND APPLICATION OF ELECTRIC PROPULSION THRUSTERS IN RUSSIA; A. Bober and N. Maslennikov, FAKEL Enterprises, Kaliningrad, Russia; M. Day, Space Systems/Loral, Palo Alto, CA; G. Popov and Yu. Rylov, Moscow Aviation Institute, Moscow, Russia

1993-002: OVERVIEW OF THE BALLISTIC MISSILE DEFENSE ORGANIZATION’S ELECTRIC PROPULSION PROGRAM; Leonard H. Caveny, Ballistic Missile Defense Organization, Innovative Science and Technology, Washington, DC 20301-7100; Francis M. Curran, NASA Lewis Research Center, Cleveland, Ohio 44135; and John R. Brophy, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109

1993-003: EUROPEAN ELECTRIC PROPULSION ACTIVITIES IN THE ERA OF APPLICATION; C. Bartoli and G. Saccoccia, ESA Technical Directorate, ESTEC, Noordwijk, The Netherlands

1993-004: AN OVERVIEW OF THE AIR FORCE’S ELECTRIC PROPULSION PROGRAM; David R. Perkins, Phillips Laboratory, Edwards AFB, California

1993-005: REVIEW OF ELECTRIC PROPULSION ACTIVITIES IN JAPAN; Y. Arakawa, University of Toyko, Tokyo, Japan

1993-007: FLIGHT QUALIFICATIONS OF A 1.8 KW HYDRAZINE ARCJET SYSTEM; R. D. Smith, S. E. Yano, K. Armbruster, and C. R. Roberts, Rocket Research Company, Redmond, WA USA; D. A. Lichtin and J. W. Beck, Martin Marietta Astro Space, Princeton, NJ, USA

1993-008: DEVELOPMENT AND QUALIFICATION TEST OF A SPT ELECTRIC PROPULSION SYSTEM FOR “GALS” SPACECRAFT; A. Bober, K. Kozubsky, G. Komarow, and N. Maslennikov, FAKEL, Kaliningrad Region, Russia; A. Kozlov and A. Romashko, NPO PM, Krasnoyarsk 26, Russia

1993-009: DEVELOPMENT OF ION ENGINE SYSTEM FOR ETS-VI; S. Shimada, K. Satoh, Y. Gotoh, E. Nishida, I. Terukina, and T. Noro, Mitsubishi Electric Corporation, Japan; H. Takegahara, Tokyo Metropolitan Institute of Technology, Hino, Tokyo, Japan; K. Nakamaru and H. Nagano, National Space Development Agency of Japan, Minato-ku, Tokyo, Japan

1993-010: DESIGN, QUALIFICATION, AND ON-ORBIT PERFORMANCE OF THE ATLAS PLASMA CONTRACTOR; J. R. Beattie, Hughes Research Laboratories, Malibu, California; J. A. Marshall, J. L. Burch, and W. C. Gibson, Southwest Research Institute, San Antonio, Texas

1993-011: ELECTRIC PROPULSION INTEGRATION ACTIVITIES ON THE MSTI SPACECRAFT; D. A. Barnhart, J. M. McCombe, and D. L. Tilley, Air Force Phillips Laboratory, Edwards A.F.B., CA

1993-012: LOW POWER ARCJET SYSTEM DESCRIPTION FOR NORTH-SOUTH STATION KEEPING; W. D. Deininger, M. Vulpiani, E. Tosti, and R. Di Stefano, BPD Difesa e Spazio, Colleferro, Italy, E. Detoma and S. Ferrari, FIAT CIEI (SEPA), Torino, Italy, and M. F. Rossi, ASI, Rome, Italy

1993-013: ARCJET PROPULSION SYSTEM STUDY FOR NSSK; F. Scortecci, L d’Agostino, F. d’Auria, and M. Andrenucci, CENTROSPAZIO, Pisa 56014, Italy

1993-015: APPLICATION OF ION PROPULSION SYSTEM TO COMMUNICATIONS SATELLITES; F. Porte, P. Saint-Aubert, D. Mawby, and J. Hsing, Matra Marconi Space, Intelsat  Washington D.C.

1993-016: SPACE-BORNE ASTRONOMICAL GRAVITY-WAVE INTERFEROMETER MISSION (SAGITTARIOUS): THE FIELD EMISSION ELECTRIC PROPULSION (FEEP) OPTION; C. Bartoli, J. Gonzalez, and G. Saccoccia, ESTC, Noordwijk, The Netherlands; M. Andrenucci, University of Pisa, Pisa, Italy; and S. Marcuccio and A. Genovese, CENTROSPAZIO, Pisa, Italy

1993-017: PLASMA THRUSTERS FOR LOW FLYING SATELLITES: A SPACE TELEPHONE SYSTEM APPLICATION; G. A. Dahlen, P. J. Baum, and D.Y. Cheng

1993-018: THE SELECTION FOR NSSK CONTROL SYSTEM OF GEOSYNCHRONUS SATELLITES; Han-Ji Wu, Xue-Zhang Feng, Center for Space Science & Applied Research, Academia Sinica, Beijing 100080, P. R. China

1993-019: ENGINEERING METHODS OF HOLLOW CATHODE CALCULATION; E. P. Vaulin, M. V. Kirushkina, L. A. Latyshev, V. B. Tikhonou, and E. A. Filatova

1993-020: EXTENDED TEST OF A XENON HOLLOW CATHODE FOR A SPACE PLASMA CONTACTOR; Timothy R. Sarver-Verhey, Sverdrup Technology, Inc., NASA Lewis Research Center Group, Brook Park, OH 44142

1993-021: ON THE MECHANISM AND SOME PECULIARITIES OF THE EROSION OF THE ACTIVE SURFACE IN CATHODE-COMPENSATOR OF ELECTRIC PROPULSION; I. M. Yartsev and V. P. Polistchook, Institute for High Temperatures Academy of Science, Moscow, Russia; and V. A. Petrosov, The Scientific-Research Institute of Thermal Processes, Moscow, Russia

1993-022: LOCAL EROSION OF THE CATHODE-COMPENSATOR IN ELECTRIC PROPULSION; V. P. Polistchook and I. M. Yartsev, Institute for High Temperatures, Academy of Science, Moscow, Russia; and V. A. Petrosov, The Scientific Research Institute of Thermal Processes, Moscow, Russia

1993-023: CHARACTERISTICS OF IONS EMITTED FROM HIGH-CURRENT HOLLOW CATHODES; Ikuya Kameyama and Paul J. Wilbur, Colorado State University, Fort Collins, CO 80523

1993-024: THEORETICAL MODELING OF ORIFICED, HOLLOW CATHODE DISCHARGES; A. Salhi and P. J. Turchi, The Ohio State University, Columbus, Ohio

1993-025: EXPERIMENTAL INVESTIGATION OF A HOLLOW CATHODE DISCHARGE; A. Salhi, R. M. Myers, and P. J. Turchi, The Ohio State University, Columbus, Ohio

1993-026: THE STUDY OF THE PHYSICS OF HOLLOW CATHODE DISCHARGES; A. K. Malik, Imperial College, London, UK; and D. G. Feam, Defence Research Agency, Farnborough, Hampshire, UK

1993-028: CATHODE EROSION RESEARCH ON MEDIUM TO HIGH POWER ARCJET THRUSTERS; W. J. Harris, E. A. O’Hair, L. L. Hatfield, and M. Kristiansen, Pulsed Power and Electric Propulsion Laboratory, Texas Tech University, Lubbock, TX 79409

1993-029: HIGH CURRENT CATHODE THERMAL BEHAVIOR, PART II: EXPERIMENTS; J. E. Polk, K. D. Goodfellow, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1993-030: HIGH CURRENT CATHODE THERMAL BEHAVIOR, PART I: THEORY; K. D. Goodfellow and J. E. Polk, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1993-032: C60 MOLECULE AS A PROPELLANT FOR ELECTRIC PROPULSION; Haruki Takegahara and Yoshinori Nakayama, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino, Tokyo, 191, Japan

1993-033: EXPERIMENTAL INVESTIGATION OF FULLERENE PROPELLANT FOR ION PROPULSION; John R. Anderson and Dennis Fitzgerald, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1993-036: DEVELOPMENT OF A MICROWAVE RESONANT CAVITY ELECTROTHERMAL THRUSTER PROTOTYPE; D. J. Sullivan and M. M. Micci, Propulsion Engineering Research Center, Department of Aerospace Engineering, The Pennsylvania State University, University Park, PA 16802, USA

1993-037: PLUME CHARACTERISTICS OF AN ECR PLASMA THRUSTER; D. A. Kaufman and D. G. Goodwin, California Institute of Technology, Pasadena, California

1993-038: ANALYSIS AND EXPERIMENTS OF A WHISTLER-WAVE PLASMA THRUSTER; E. B. Hooper, S. W. Ferguson, M. A. Makowski, and B. W. Stallard, Lawrence Livermore National Laboratory, Livermore, CA 94551; and John L. Power, NASA Lewis Research Center, Cleveland, OH 44135

1993-040: MICROWAVE PLASMA CONTRACTOR; Hitoshi Kuninaka, Institute of Space and Astronautical Science, Yoshinodai, Sagamihara, Kanagawa, Japan; Nobuo Hiroe, Kazuto Kitaoka, and Yoshio Ishikawa, Nihon University, Narashinodai, Funabashi, Chiba, Japan; and Kazutaka Nishiyama, University of Tokyo, Hongo, Bunkyo, Tokyo, Japan

1993-041: PLASMA CONTACTOR DEVICE BASED ON HOLLOW CATHODE TECHNOLOGY FOR SPACECRAFTS CHARGING NEUTRALIZATION AND TETHERED SYSTEM APPLICATIONS: REVIEW OF ITALIAN NATIONAL PROGRAM; G. F. Cirri, G. Matticari, M. Minucci, G. Noci, A. Severi, and P. Amatulli, Proel Tecnologie – Firenze (Italy); and F. Svelto, ASI (Italian Space Agency), Roma (Italy)

1993-042: HOLLOW CATHODE HEATER DEVELOPMENT FOR THE SPACE STATION PLASMA CONTACTOR; George C. Soulas, Sverdrup Technology, Inc., NASA Lewis Research Center Group, Brook Park, Ohio

1993-043: DESIGN OF A HIGH EFFICIENCY POWER PROCESSOR FOR THE RUSSIAN STATIONARY PLASMA THRUSTER (SPT); G. Fischer, T. Colbert, and M. Day, Space Systems/Loral, Palo Alto, CA, USA; J. Kahn and  H. Kaufman, Front Range Research, Fort Collings, CO, USA; K. Kozubsky, and V. Sokolov, Fakel Enterprises, Kaliningrad Region, Russia

1993-044: POWER  ELECTRONICS DEVELOPMENT FOR THE SPT-100 THRUSTER; John A. Hamley, Gerald M. Hill, and John M. Sankovic, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135

1993-045: ARCJET POWER CONDITIONING UNIT: DESIGN CHARACTERISTICS AND PRELIMINARY TESTS; G. Botto and M. Carpita, Ansaldo Ricerchi, Corso Perrone 118, 16161, Genova, Italy; G. Parisi and E. Detoma, FIAT-CIEI, Corso G. Cesare 294, 10154 Torino, Italy; and W. Deininger, BPD Difesa e Spazio, Corso Garibaldi 22, 00034 Colleferro, Roma, Italy

1993-046: A 1.8 kW STATIC ARCJET SIMULATOR; E. Detoma and G. Parisi, FIAT CIEI, SEPA, Corso Giulio Cesare, 300 – 10154 Torino To (Italy); and W. Deininger, BPD Difesa e Spazio, Corso Garibaldi, 22 – 00034 Colleferro Rm (Italy)

1993-047: DEVELOPMENT OF A LOW POWER CONTROL UNIT FOR LOW POWER ARCJET; H. Willenbockel, G. Matthaeus, and M. A. Kinnersley, ERNO Raumfahrttechnik GmbH, Deutsche Aerospace AG, Trauen, Germany

1993-048: THE DESIGN, FABRICATION, AND TEST OF A 26 KW ARCJET AND POWER CONDITIONING UNIT; C. E. Vaughan and R. J. Cassady, Rocket Research Company, Redmond, WA 98073; and J. R. Fisher, Pacific Electro Dynamics, Redmond, WA 98073

1993-049: ACHIEVING RELIABLE, REPEATABLE STARTS OF A 26 KW ARCJET; R. S. Aadland, W. A. Hoskins, and C. E. Vaughan, Rocket Research Company, Redmond, WA 98073; and R. J. Kay, Pacific Electro Dynamics, Redmond, WA 98073

1993-052: DEVELOPMENT OF A POWER ELECTRONICS UNIT FOR THE SPACE STATION PLASMA CONTACTOR; John A. Hamley, Gerald M. Hill and Michael J. Patterson, NASA Lewis Research Center, Cleveland, Ohio; Joseph Saggio Jr. and Fred Terdan, Analex Corporation, Cleveland, Ohio; and Justin D. Mansell, Case Western Reserve University, Cleveland, Ohio

1993-053: POWER PROCESSING UNITS FOR HIGH POWERED NUCLEAR ELECTRIC PROPULSION WITH MPD THRUSTERS; Robert H. Frisbee, Radhe S. L. Das, and Stanley Krauthamer, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

1993-054: SPACE SURVEILLANCE TRACK AND AUTONOMOUS REPOSITION (SSTAR) EXPERIMENT; Lt. Col. S. A. Sneegas, Phillips Laboratory, Kirtland AFB, New Mexico, R. A. Rosenthal, TRW, Redondo Beach, California, and Dr. R. J. Vondra, Phillips Laboratory/ UDRI, Kirtland AFB, New Mexico

1993-055: NEPSTP – AN INTERNATIONAL TESTBED FOR XENON ELECTRIC PROPULSION; Gregg A. Herbert and Glen E. Cameron, The Johns Hopkins University, Applied Physics Laboratory, Laurel, Maryland 20723; and Leonard H. Caveny, Ballistic Missile Defense Organization, Washington, DC 20301-7100

1993-056: DEVELOPMENT AND UTILIZATION OBJECTIVES OF A LOW-POWER ARCJET FOR THE P3-D (OSCAR) SATELLITE; Ernst W. Messerschmid, Dieter M. Zube, and Helmut l. Kurtz, Institut für Raumfahrtsysteme, Universität Stuttgart, Paffenwaldring 31, D-70550 Stuttgart, Federal Republic of Germany; and Kari Meinzer, AMSAT Deutschland e. V., Holderstrauch 10, D-35041 Marburg, Federal Republic of Germany

1993-057: OVERVIEW OF THE AIR FORCE ESEX FLIGHT EXPERIMENT; A. M. Sutton, Phillips Laboratory (AFMC), Edwards AFB, California, USA

1993-058: DEVELOPMENT OF AN MPD THRUSTER SYSTEM FOR THE EPEX SPACE TEST; K. Toki, Y. Shimizu, and K. Kuriki, Institute of Space and Astronautical Science, Kanagawa, Japan; H. Suzuki, Ishikawajima-Harima Heavy Industries Co., Ltd. Tokyo, Japan, and Y. Kunii, Mitsubishi Electric Corporation, Kanagawa, Japan

1993-059: ION PROPULSION: A KEY ENABLER ON ESA’S DRTM PROGRAMME, H. Bassner, Deutsche Aerospace AG, Ottobrunn; M. Silvi, Alenia Spazio, Rome; L. v. Holtz and C. Bartoli, ESTEC, Noordwijk

1993-061: ELECTRIC PROPULSION: THE NEXT REAL BREAKTHROUGH IN SPACE TRANSPORTATION; Robert L. Sackheim and Richard Rosenthal, TRW Space and Electronics Group, Redondo Beach, California

1993-063: TROPIX: A SOLAR ELECTRIC PROPULSION FLIGHT EXPERIMENT; J. Mark Hickman and G. Barry Hillard, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135; Steven R. Oleson, Sverdrup Technology, Inc., Lewis Research Center Group, Brook Park, Ohio 44142

1993-064: NEP EARLY FLIGHT PROGRAM: SYSTEM PERFORMANCE AND DEVELOPMENT CONSIDERATIONS; Michael P. Doherty and Jeffrey A. George, NASA Lewis Research Center, Cleveland, Ohio

1993-065: POTENTIAL NASA EARLY FLIGHT NUCLEAR ELECTRIC PROPULSION MISSIONS; Harvey S. Bloomfield, NASA Lewis Research Center, Cleveland, Ohio

1993-066: NUMERICAL CALCULATIONS OF A CYLINDRICAL MPD THRUSTER; P. C. Sleziona, M. Auweter-Kurtz, and H. O. Schrade; Institut für Raumfahrtsysteme Universität Stuttgart, FRG

1993-068: SPACE CHARGE INSTABILITY, CURRENT CHOPPING AND ANOMALOUS TRANSPORT IN STATIONARY MPD THRUSTER FLOWS; H. P. Wagner, M. Auweter-Kurtz, and E. W. Messerschmid, Institut für Raumfahrtsysteme (IRS), Universität Stuttgart, FRG

1993-069: NONLINEAR DEVELOPMENT OF SPACE CHARGE INSTABILITY IN MPD-THRUSTER FLOWS; M. Maurer, MAN Technologie AG, Munich, Germany; H. J. Kaeppeler, Institut für Raumfahrtsysteme (IRS), Universität Stuttgart, Germany

1993-071: IONIZATION RATE MODELS AND INLET IGNITION IN SELF-FIELD MPD THRUSTERS; E. J. Sheppard and M. Martinez-Sanchez, Space Power and Propulsion Lab, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139, U.S.A.

1993-072: NUMERICAL FLUID SIMULATION OF AN MPD THRUSTER WITH REAL GEOMETRY; G. Caldo, E. Y. Choueiri, A. J. Kelly, and R. G. Jahn, Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Princeton, New Jersey 08544, USA

1993-073: ANALYTICAL STUDY ON NONEQUILIBRIUM FLOWS IN SELF-FIELD MPD THRUSTERS; T. Shoji, K. Ogiwara, and I. Kimura, Department of Aeronautics and Astronautics, School of Engineering, Tokai University, Hiratsuka, Kanagawa, Japan

1993-074: NUMERICAL SIMULATION OF CYLINDRICAL, SELF-FIELD MPD THRUSTERS WITH MULTIPLE PROPELLANTS; Michael R. LaPointe, Sverdrup Technology, Inc. LeRC Group, Brook Park, OH 44142

1993-076: RESEARCH OF PLASMA ACCELERATION PROCESSES IN SELF-FIELD AND APPLIED MAGNETIC FIELD THRUSTERS; V. B. Tikhonov and S. A. Semenihin, Moscow Aviation Institute; V. A. Alexandrov, G. A. Dyakonov, and G. A. Popov, Research Institute of Applied Mechanics and Electrodynamics, Moscow Aviation Institute

1993-077: PLASMA FLOW INVESTIGATION IN MPD-THRUSTER; N. Barabanov, Moscow Aviation Institute, Russia

1993-078: DESIGN AND DEVELOPMENT OF A 3 TO 10 kW AMMONIA ARCJET; K. D. Goodfellow and J. E. Polk, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1993-079: HIGH SPECIFIC POWER AMMONIA AND HYDROGEN ARCJET DEVELOPMENT; G. Aston, J. B. Kolts, and M. B. Aston, Electric Propulsion Laboratory, Inc., Monument, CO 80132

1993-081: A REVIEW OF THE ESA ASTP-3 MPD/ARCJET DEVELOPMENT PROGRAM (1988-1993); W. D. Deininger, BPD Difesa e Spazio, Colleferro, Italy; M. Andrenucci, Centrospazio, Pisa, Italy, and G. Saccoccia, European Space Agency (ESA/ESTEC), Noordwijk, The Netherlands

1993-082: PERFORMANCE TESTING OF A 1 kW ARCJET THRUSTER USING HYDRAZINE; R. Di Stefano, W. D. Deininger, and E. Tosti, BPD Difesa e Spazio, Colleferro, Italy; and K. Armbruster, Rocket Research Company, Redmond, WA, USA

1993-083: INTERMITTENT OPERATION OF A LOW POWER ARCJET; Tetsuya Yamada, Yoshihiro Iwamoto, Kazuhiko Ogiwara, Kyoichiro Toki, and Kyoichi Kuriki, Institute of Space and Astronautical Science, Kanagawa, Japan

1993-084: EXPERIEMENTAL INVESTIGATION ON ARCJETS PERFORMANCE AND POSSIBLE APPLICATION TO CURRENT MISSION CONCEPTS WITH LOW-POWER AVAILABILITY; F. Scorteci and F. Paganucci, Centrospazio, Pisa, Italy; G. Saccoccia and J. Gonzalez, ESA/ESTEC, Noordwijk, The Netherlands

1993-087: DEVELOPMENT AND DEMONSTRATION OF A 600 SECOND MISSION AVERAGE ARCJET; Paul G. Lichon, Rocket Research Company, Redmond, WA 98073; and John M. Sankovic, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH 44135

1993-088: DEVELOPMENT OF A 10 kWe/N RADIATIVELY-COOLED ARCJET TECHNOLOGY; E. Tosti and W. D. Deininger, BPD Difesa e Spazio, Colleferro, Italy

1993-091: PERFORMANCE EVALUATION AND LIFE TESTING OF THE SPT-100; Charles E. Garner, James E. Polk, Lewis C. Pless, Keith D. Goodfellow, and John R. Brophy, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

1993-092: EFFECT OF BACKGROUND NITROGEN AND OXYGEN ON INSULATOR EROSION IN THE SPT-100; J. Kahn and V. Zhurin, Front Range Research, Fort Collins, CO; K. Kozubsky, Fakel Enterprise, Kaliningrad on Baltic Sea, Russia; T. Randolph, Space System/Loral, Palo Alto, CA; V. Kim, RIAME at Moscow Aviation Institute, Moscow, Russia

1993-093: FACILITY EFFECTS ON STATIONARY PLASMA THRUSTER TESTING; T. Randolph and M. Day, Space Systems/Loral, Palo Alto, CA, USA; V. Kim, Research Institute of Applied Mechanics and Electrodynamics, Moscow, Russia; H. Kaufman and V. Zhurin, Front Range Research, Fort Collins, CO, USA; and K. Kozubsky, Fakel, Kaliningrad Region, Russia

1993-094: PERFORMANCE EVALUATION OF THE RUSSIAN SPT-100 THRUSTER AT NASA LeRC; John M. Sankovic, John A. Hamley, and Thomas W. Haag, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135

1993-095: DYNAMIC CHARACTERISTICS OF CLOSED DRIFT THRUSTER; V. Zhurin, J. Kahn, and H. Kaufman, Front Range Research, Fort Collins, Colorado; K. Kozubsky, Fakel Enterprise, Kaliningrad on Baltic Sea, Russia; and M. Day, Space Systems Loral, Palo Alto, California

1993-096: STATIONARY PLASMA THRUSTER PLUME CHARACTERISTICS; Roger M. Myers and David H. Manzella, Sverdrup Technology, Inc. NASA Lewis Research Center Group, Brookpark, OH 44142

1993-097: STATIONARY PLASMA THRUSTER PLUME EMISSIONS; David H. Manzella, Sverdrup Technology Inc., Lewis Research Center Group, Brook Park, Ohio 44142

1993-098: PRELIMINARY FAR-FIELD PLUME SPUTTERING CHARACTERIZATION OF THE STATIONARY PLASMA THRUSTER (SPT-100); Eric J. Pencil, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135

1993-099: PREDICTION OF ELECTRIC THRUSTER LIFETIME; V. I. Baranov, A. I. Vasin, A. A. Kalyaev, and V. A. Petrosov, The Scientific-Research Institute of Thermal Processes, Moscow, Russia

1993-100: ELECTRIC ROCKET ENGINE ACCELERATED TEST CONCEPT; V. I. Baranov, A. I. Vasin, A. A. Kalyaev, and V. A. Petrosov, The Scientific-Research Institute of Thermal Processes, Moscow, Russia

1993-101: STATIONARY PLASMA THRUSTER (SPT) DEVELOPMENT STEPS AND FUTURE PERSPECTIVES; A. J. Morozov, Kurchatov Institute, Moscow, Russia

1993-102: FLIGHT TEST RESULTS OF THE RITA EXPERIMENT ON EURECA; H. Bassner, H. P. Berg, R. Kukies, and H. Müller, DASA, Munich, Germany

1993-104: A COMPREHENSIVE TEST AND EVALUATION PROGRAM FOR THE UK-10 ION ENGINE; M. W. Crofton, Technology Operations, Mechanics & Materials, M5/754, PO Box 92957, The Aerospace Corporation, Los Angeles, California 90009

1993-105: RECENT ION THRUSTER DEVELOPMENTS AT GIESSEN UNIVERSITY; K. H. Groh, P. Fahrenbach, and H. W. Loeb, Institute of Physics, University of Giessen, Heinrich-Buff-Ring 16, 6300 Giessen, Germany

1993-106: FLIGHT QUALIFICATION OF AN 10-mN XENON ION THRUSTER; J. R. Beattie, J. D. Williams, and R. R.  Robson, Hughes Research Laboratories, Malibu, California 90265

1993-107: LOW THRUST ION PROPULSION: DEVELOPMENT ACTIVITIES AT PROEL TECNOLOGIE; G. F. Cirri, G. Matticari, and G. Noci, Proel Tecnologie, Firenze (Italy); G. Perrotta, Alenia Spazio, Roma (Italy), M. F. Rossi and J. Sabbagh, ASI (Italian Space Agency), Roma (Italy)

1993-108: PERFORMANCE OF THE NASA 30 CM ION THRUSTER; Michael J. Patterson and Thomas W. Haag, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio; and Scot A. Hovan, Department of Mechanical Engineering, University of Dayton, Dayton, Ohio

1993-109: REVIEW OF QUALIFICATION ACTIVITIES ON THE NEUTRALIZER FOR THE RIT 10 ION THRUSTER; G. F. Cirri, A. Cipriani, G. Matticari, and A. Severi, Proel Tecnologie, Firenze (Italy); C. Bartoli, G. Saccoccia, and H. Von Rohden, ESA/ESTEC Electric Propulsion Unit, Noordwijk, The Netherlands

1993-110: OPERATING CHARACTERISTICS OF A 15-cm-dia. ION ENGINE FOR SMALL PLANETARY SPACECRAFT; John R. Brophy, Lewis C. Pless, Juergen Mueller, and John R. Anderson, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1993-111: COMPARISON OF EROSION OF CARBON-CARBON AND MOLYBDENUM ION OPTICS; J. S. Meserole and D. E. Hedges, Boeing Defense & Space Group, Seattle, WA 98124

1993-112: FABRICATION OF CARBON-CARBON GRIDS FOR ION OPTICS; Juergen Mueller, David K. Brown, Charles E. Garner, and John R. Brophy, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

1993-115: PERFORMANCE OF HOT CATHODE MPD THRUSTERS; F. Paganucci and M. Andrenucci, Centrospazio, Pisa, Italy

1993-116: EVALUATION OF EXTERNALLY HEATED PULSED MPD THRUSTER CATHODES; Roger M. Myers, Sverdrup Technology, Inc. NASA Lewis Research Center Group, Brook Park, OH 44135; Matthew Domonkos, The University of New Mexico, Albuquerque, NM 87131; and Alec D. Gallimore, The University of Michigan, Ann Arbor, MI 48109

1993-117: HIGH-CURRENT STATIONARY PLASMA ACCELERATOR OF HIGH POWER; V. P. Ageyev and V. G. Ostrovsky, Scientific-Production Association “Energiya,” Kaliningrad, Moscow Region, Russia; and V. A. Petrosov, The Scientific-Research Institute of Thermal Processes, Moscow, Russia

1993-118: CONTROL AND MINIMIZATION OF ANODE FALL IN A QUASI-STEADY NOZZLE-BASED COAXIAL PLASMA THRUSTER; J. T. Scheuer, R. P. Hoyt, K. F. Schoenberg, R. A. Gerwin, R. W. Moses, and I. Henins, Los Alamos National Laboratory, Los Alamos, NM; R. M. Mayo and D. C. Black, North Carolina State University, Raleigh, NC

1993-119: DEVELOPMENT OF A SUPERCONDUCTING ELECTROMAGNET FOR APPLIED FIELD ARCJET THRUSTERS; F. Scortecci and G. Capecchi, CENTROSPAZIO, Pisa, Italy; M. Andrenucci, University of Pisa, Pisa, Italy; G. Mei and R. Garre, EUROPA METALLI-LMI, Fornaci di Barga, Lucca, Italy

1993-120: ROLE OF ANODE THROAT IN MPD ARCJET; I. Funaki, K. Toki, and K. Kuriki, Institute of Space and Astronautical Science, Kanagawa, Japan

1993-122: EXPERIMENTAL COMPARISON OF STEADY STATE NOZZLE TYPE AND CYLINDRICAL MPD THRUSTERS AT HIGH CURRENT LEVELS; Thomas Wegmann, Monika Auweter-Kurtz, Harald Habiger, Helmut L. Kurtz, and Herbert O. Schrade, Institut für Raumfahrtsysteme, Universität Stuttgart, FRG

1993-123: OPTICAL DIAGNOSTICS OF HIGH CURRENT PULSED ARC IN HIGH DENSITY GAS; A. M. Voronov and V. N. Zhuraviev, IPE RAS, 18 Dvortsovaya nab., St. Petersburg, 191065, Russia

1993-124: ELECTROSTATIC PROBES FOR THE INVESTIGATION OF ARC-DRIVEN ELECTRIC PROPULSION DEVICES; H. A. Habiger, M. Auweter-Kurtz, and H. Kurtz, Universität Stuttgart, Stuttgart, Germany

1993-125: MICROINSTABILITES IN HIGH POWER MPD SYSTEMS: PRELIMINARY DIAGNOSTICS, Erik C. Bowman and Dennis L. Tilley

1993-126: CHAMBER EFFECTS ON PLUME EXPANSION FOR A LOW-POWER HYDROGEN ARCJET; Iain D. Boyd, Cornell University, Ithaca, NY 14853; Doug R. Beattie and Mark A. Cappelli, Stanford University, Stanford, CA 94305

1993-127: LASER-INDUCED FLUORESCENCE MEASUREMENTS ON THE PLUME FROM A 1 kW ARCJET OPERATED ON SIMULATED AMMONIA; W. M. Ruyten, University of Tennessee-Calspan, Center for Space Transportation and Applied Research, Tullahoma, Tennessee, 37388-8897; D. Burtner and D. Keefer, Center for Laser Applications; University of Tennessee Space Institute, Tullahoma, Tennessee, 37388-8897

1993-128: TIME RESOLVED MEASUREMENTS OF 1 kW ARCJET PLUMES USING CURRENT MODULATION VELOCIMETRY AND TRIPLE LANGMUIR PROBES; Jeffrey A. Pobst, John H. Schilling, and Daniel A. Erwin, University of Southern California, Department of Aerospace Engineering, Los Angeles, California 90089-1191; Ronald A. Spores, OL-AC Phillips Laboratory, Edwards Air Force Base, California 93524

1993-129: VIBRATIONAL NON-EQUILIBRIUM IN ARCJET FLOWS; V. Babu, S. Aithal, and V. V. Subramaniam, Department of Mechancial Engineering, The Ohio State University, Columbus, Ohio 43210

1993-130: THE USE OF PULSED ELECTRON BEAM FLUORESCENCE FOR ARCJET PLUME DIAGNOSTICS; John H. Schilling, Jeffrey A. Pobst, and Daniel A. Erwin, University of Southern California, Department of Aerospace Engineering, Los Angeles, CA 90089-1191

1993-131: LIF MEASUREMENTS OF SPECIIES VELOCITIES IN AN ARCJET PLUME; John G. Liebeskind, Ronald K. Hanson, and Mark A. Cappelli, High Temperature Gasdynamics Laboratory, Department of Mechanical Engineering, Stanford University, Stanford, CA 94305

1993-132: ARCJET PLUME STUDIES USING MOLECULAR BEAM MASS SPECTROMETRY; James E. Polland, The Aerospace Corporation, Mechanics & Materials Technology Center, P.O. Box 92937-M5/754, Los Angeles, CA 90009

1993-133: OPTICAL MEASUREMENT AND NUMERICAL ANALYSIS OF MEDIUM-POWER ARCJET NON-EQUILIBRIUM FLOWFIELDS; H. Tahara, N. Uda, K. Onoe, Y. Tsubakishita, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Toyonaka, Osaka, Japan

1993-134: EMISSION SPECTROSCOPY OF 1 kWe ARCJET OPERATING WITH SIMULATED HYDRAZINE; E. Tosti and W. D. Deininger, BPD Difesa e Spazio, Colleferro, Italy

1993-135: EFFECTS OF NOZZLE GEOMETRY ON PLUME EXPANSION FOR SMALL THRUSTERS; Donna Zelesnik, Ohio Aerospace Institute, Brook Park, Ohio; Paul F. Penko, NASA Lewis Research Center, Cleveland, Ohio; and Iain D. Boyd, Cornell University, Ithaca, New York

1993-136: INVESTIGATION OF A VERY LOW POWER PULSED ARCJET; Gary F. Willmes and Rodney L. Burton, Department of Aeronautical and Astronautical Engineering, University of Illinois at Urbana-Champaign, Urbana, IL 61801

1993-137: NUMERICAL MODELLING OF RAREFIELD PLASMA PLUME IN NEUTRAL ENVIRONMENT GAS; A. M. Bishaev, V. K. Kalashnikov, and V. Kim, Research Institute of Applied Mechanics and Electrodynamics, Moscow, Russia

1993-138: PLASMA EXPANSION IN A LOW-POWER MPD THRUSTER WITH VARIABLE MAGNETIC NOZZLE; T. M. York and H. Kamhawi, The Ohio State University, Columbus, Ohio 43210

1993-141: MPD THRUSTER PLUME DIAGNOSTICS; M. Andrenucci, University of Pisa, Pisa, Italy; F. Paganucci and A. Turco, CENTROSPAZIO, Pisa, Italy

1993-142: MODELLING OF ION THRUSTER PLUME CONTAMINATION; R. I. Samanta Roy and D. E. Hastings, Space Power and Propulsion Laboratory, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, Massachusetts 02139; N. A. Gatsonis, Applied Physics Laboratory, The Johns Hopkins University, Laurel, Maryland 20723

1993-143: OPTIONS AND TRADEOFFS FOR A SPACEBORNE ARCJET DIAGNOSTIC PACKAGE; S. Ferrari and E. Detoma, FIAT CIEI, SEPA, Corso Giulio Cesare, 300 – 10154 Tornino To (Italy); W. Deininger and E. Tosti, BPD Difesa e Spazio, Corso Garibaldi, 22 – 00034, Colleferro Roma (Italy); F. Scortecci and G. Capecchi, CONSORZIO PISA RICERCHI, CENTROSPAZIO, Via A. Gherardesca, 5-56014, Ospedaletto Pisa (Italy); J. J. Scialdone, NASA – Goddard Space Flight Center, Greenbelt, Maryland 20771 (U.S.A.)

1993-144: RADIO WAVE REFRACTION IN EXHAUST PLASMA PLUMES; F. F. Gabdullin, V. I. Garkusha, A. G. Korsun, and E. M. Tverdokhlebova, Central Research Institute of Machine-Building, Kaliningrad, Moscow Region, Russia

1993-145: RADIO WAVE REFRACTION IN EXHAUST PLASMA PLUMES; F. F. Gabdullin, V. I. Garkusha, A. G. Korsun, and E. M. Tverdokhlebova, Central Research Institute of Machine-Building, Kaliningrad, Moscow Region, Russia

1993-147: ELECTROMAGNETIC INTERFERANCE OF STATIONARY PLASMA THRUSTER; V. I. Brukhty, Scientific-Research Institute of Thermal Processes, Moscow, Russia; K. P. Kirdyashev, Institute of Radioengineering and Electronics, Russian Academy of Sciences, Fryazino, Moscow Region, Russia

1993-148: EXPERIMENTAL AND ANALYTICAL EVALUATION OF ELECTROMAGNETIC RADIATED EMISSIONS FROM ELECTRIC PROPOLUSION SYSTESM; K. P. Kidyashev, Russian Academy of Sciences, Institute of Radioengineering and Electronics, Fryasino, Moscow Region, Russia

1993-149: THE EFFECT OF ALKALI METAL ELECTRIC ROCKET ENGINES ON SPACECRAFT; V. I. Brukhty, V. N. Shutov, and A. B. Sminov, The Scientific-Research Institute of Thermal Processes, Moscow, Russia; M. P. Burgasov and A. A. Chirov, The Moscow Aviation Institute, Moscow, Russia

1993-150: A DOUBLE PENDULUM PRECISION THRUST MEASUREMENT BALANCE; T. F. Yang, Ping Liu, F. R. Chang-Diaz, Harvey Lander, R. A. Childs, H. D. Becker and S. A. Fairfax, MIT Plasma Fusion Center, Cambridge, MA 02139

1993-151: A LARGE HIGH VACUUM, HIGH PUMPING SPEED SPACE SIMULATION CHAMBER FOR ELECTRIC PROPULSION; Stanley P. Grisnik, NASA Lewis Research Center, Brookpark, OH; James E. Parkes, Sverdrup Technology, Inc., Brookpark, OH

1993-154: ION BEAM MODELING IN FEEP THRUSTERS; M. Andrenucci, University of Pisa, Pisa 56100, Italy; A. Ciucci and S. Marcuccio, CENTROSPAZIO, Pisa 56014, Italy

1993-155: EXPERIMENTAL PERFORMANCE OF CONTINUOUS AND PULSED FEEP THRUSTERS; S. Marcuccio and A. Genovese, CENTROSPAZIO, Pisa 56014, Italy; M. Andrenucci, University of Pisa, Pisa 56100, Italy

1993-156: FIELD EMISSION ELECTRIC PROPULSION (FEEP) SYSTEM STUDY; S. Marcuccio and A. Genovese, CENTROSPAZIO, Pisa 56104, Italy; M. Andrenucci, University of Pisa, Pisa 56100, Italy; C. Bartoli, J. Gonzalez, and G. Saccoccia, ESA/ESTEC, Noordwijk, The Netherlands

1993-157: FIELD EMISSION ELECTRIC PROPULSION: EXPERIMENTAL INVESTIGATIONS ON MICROTHRUST FEEP THRUSTERS; J. Gonzalez, G. Saccoccia, and H. von Rohden, ESA/ESTEC, Noordwijk, The Netherlands

1993-158: PROSPECTS OF MICROSTRUCTRED LIQUID METAL ION SOURCES (MILMIS) FOR FIELD EMISSION ELECTRIC PROPULSION (FEEP); J. Mitterauer, Technische Universität Wien, Institut für Allgemeine Elektrotechnik und Elektronik, Gusshausstrasse 27-29, 1040 Wien, Austria

1993-159: EXPERIMENTAL ANALYSIS OF A COAXIAL SOLID-PROPELLANT MPD THRUSTER WITH SEGMENTED ANODES; G. Paccani, Universita’ di Roma “La Sapienza, Rome, Italy

1993-160: DEVELOPMENT AND LABORATORY TEST OF EROSION PULSED PLASMA THRUSTER, DESIGNED FOR THE ATTITUDE CONTROL OF A GEOSTATIONARY SATELLITE; N. N. Antropov, G. A. Popov, A. I. Rudikov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute, Moscow, Russia

1993-165: SEMI-EMPIRICAL INTERIOR BALLISTICS SIMULATION MODEL OF ARC HEATED LIGHT GAS GUN; A. M. Glukhov, IPERAS, 18 Dvortsovaya, St. Petersburg, 191065, Russia

1993-166: USE OF HYDROGEN ARCJET THRUSTERS FOR DIAMOND SYNTHESIS; Mark A. Cappelli, Michaela H. Loh, and John G. Liebeskind, High Temperature Gasdynamics Laboratory, Stanford University, Department of Mechanical Engineering, Stanford, CA 94305-3032

1993-167: ATOMIC OXYGEN SIMULATION USING MPD THRUSTER TECHNOLOGY; S. B. Gabriel, N. J. Wood, G. T. Roberts, and A. R. L. Tatnall, Dept. of Aeronautics and Astronautics, University of Southampton, Southampton, Hampshire, UK

1993-168: APPLICATIONS OF QUASI-STEADY MPD ACRJETS TO MATERIAL PROCESSINGS-CERAMIC COATINGS BY MEANS OF MPD SPRAY; H. Tahara, T. Tsubaki, Y. Kagaya, Y. Tsubakishita, and T. Yoshikawa, Osaka University, Osaka, Japan

1993-169: ION THRUSTER ENDURANCE TEST USING DEVELOPMENT MODEL THRUSTER FOR ETS-VI; S. Shimada, K. Satoh, Y. Gotoh, E. Nishida and T. Nora, Mitsubishi Electric Corporation, Japan; H. Takegahara, Tokyo Metropolitan Institute of Technology, Tokyo, Japan; H. Nagano and K. Nakamaru, National Space Development Agency of Japan

1993-170: 500 HOUR TESTS OF THE T5 ION THRUSTER WITH DUAL AND TRIPLE GRID EXTRACTION SYSTEMS; S. D. Watson, P. Hurford, A. R. Martin, C. R. Banks, R. W. Eaton, M. S. Harvey, W. E. F.L. Moulford, and A. J. Pearce, AEA Technology Space Applications, Culham Laboratory, Abingdon, Oxfordshire, OX14 3DB

1993-171: EROSION MEASUREMENTS FOR TWO AND THREE GRID ION THRUSTER EXTRACTION SYSTEMS; A. R. Martin, C. R. Banks, R. W. Eaton, P. Hurford, W. E. F. L. Moulford and A. J. Pearce, AEA Technology, Space Applications, F4 Culham, Abingdon, Oxon OX14 3DB, UK

1993-172: TEST TO FAILURE OF A TWO GRID 30cm dia ION ACCELERATOR SYSTEM; John R. Brophy, James E. Polk, and Lewis C. Pless; Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1993-173: CHARGE-EXCHANGE GRID EROSION STUDY FOR GROUND-BASED AND SPACE-BASED OPERATIONS OF ION THRUSTERS; Xiaohang Peng, Wilhelmus M. Ruyten, and Dennis Keefer, University of Tennessee-Calspan Center for Space Transportation and Applied Research, Tullahoma, Tennessee 37388

1993-174: EFFECTS OF DESIGN AND OPERATING CONDITIONS ON ACCELERATOR-GRID IMPINGEMENT CURRENT; Jeff M. Monheiser and Paul J. Wilbur, Colorado State University, Fort Collins, CO 80523

1993-175: EROSION CHARACTERISTICS OF TWO-GRID ION ACCELERATING SYSTEMS; V. Rawlin, NASA Lewis, Cleveland, OH

1993-176: PROBABILISTIC ANALYSIS OF ION ENGINE ACCELERATOR GRID LIFE; J. E. Polk, N. R. Moore, L. E. Newlin, J. R. Brophy, and D. H. Ebbeler, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1993-177: ION THRUSTER LIFETIME LIMITATIONS IMPOSED BY SPUTTERING PROCESSES; D. G. Fearn, Defence Research Agency, Farnborough, UK

1993-178: PARTICLE SIMULATION OF GRID EROSION FOR A THREE GRID ION THRUSTER; Quan Zhang, ERC, Inc., Tullahoma, Tennessee 37388; Xiaohang Peng and Dennis Keefer, University of Tennessee-Calspan Center for Space Transportation and Applied Research, University of Tennessee Space Institute, Tullahoma, Tennessee 37388

1993-179: EXTRACTION SYSTEM DESIGN AND MODELLING USING COMPUTER CODES; R. A. Bond and P. M. Latham, AEA Technology, Space Applications, Culham Laboratory, Abingdon, Oxon OX14 3DB, UK

1993-181: NUMERICAL SIMULATION OF THE PERFORMANCE OF A RADIATION-COOLED 1KW DC ARCJET THRUSTER; Hiroyuki Okamota and Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812, Japan; Ken-ichi Tanaka, Central Research Laboratory, Mitsubishi Electric Corporation, Amagasaki, Hyogo 661, Japan; and Alfred Beylich, Stosswellenlabor, Rheinisch-Westfälische Technische Hochschule Aachen, 5100 Aachen, Germany

1993-182: DEVELOPMENT OF A NUMERICAL MODEL OF THE NOZZLE FLOW IN LOW POWER ARCJET THRUSTERS; A. Ciucci, Centrospazio, Pisa, Italy; L. d’Agostino and M. Andrenucci, University of Pisa, Pisa, Italy

1993-183: ON THE EFFECTS OF SWIRL IN ARCJET THRUSTER FLOWS; V. Babu, S. Aithal, and V. V. Subramaniam, Department of Mechanical Engineering, The Ohio State University, Columbus, Ohio 43210

1993-184: BEHAVIOR OF ARC COLUMN IN ARCJET CONSTRICTOR; Tetsuya Yamada, Kyoichiro Toki, and Kyoichi Kuriki, Institute of Space and Astronautical Science, Kanagawa, Japan

1993-185: ANODE HEAT LOSS AND CURRENT DISTRIBUTION IN DC ARCJETS; K. Fujita and Y. Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, Tokyo, Japan

1993-186: EFFECT OF A PULSED MAGNETIC FIELD ON ARCJET OPERATION; Nicholas T. Tiliakos and Rodney L. Burton, Department of Aeronautical and Astronautical Engineering, University of Illinois at Urbana-Champaign, Urbana, IL 61801

1993-187: PERFORMANCE CALCULATION OF ARCJET THRUSTERS – THE THREE CHANNEL MODEL; B. Glocker, H. O. Schrade, and M. Auweter-Kurtz; Institut für Raumfahrtsysteme, Universität Stuttgart

1993-189: THEORETICAL MODELING OF MAGNETOPLASMADYNAMIC ARCJETS; Pavlos G. Mikellides and Peter J. Turchi, Ohio State University, Columbus, OH; and Norman F. Roderick, University of New Mexico, Albuquerque, NM

1993-190: THRUST PRODUCTION THEORY OF ELECTROMAGNET/THERMAL HYBRID ARCJETS; A. Sasoh, Tohoku University, Sendai, Japan

1993-191: CALCULATION OF A NOZZLE TYPE MPD THRUSTER AND COMPARISON WITH MEASUREMENTS; P. C. Sleziona, M. Auweter-Kurtz, C. Boise, H. L. Kurtz, H. O. Schrade, and T. Wegmann, Institut für Raumfahrtsysteme Universität Stuttgart, FRG

1993-194: MECHANISMA OF ANODE POWER DEPOSITION IN A LOW PRESSURE FREE BURING ARC; George C. Soulas, Ohio State University, Columbus, Ohio 43210; and Roger M. Myers, Sverdrup Technology, Inc. NASA Lewis Research Center Group, Brook Park, Ohio 44142

1993-196: AN EXPERIMENTAL STUDY OF LITHIUM DISPENSER CATHODES IN THE MPD THRUSTER; J. S. Fillmore, W. F. von Jaskowsky, A. J. Kelly, and R. G. Jahn, Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Princeton, NJ 08544, USA

1993-197: DIAGNOSTIC EXPERIMENT AND NUMERICAL ANALYSIS OF ONE-DIMENSIONAL MPD FLOWFIELDS; H. Tahara, T. Tsubaki, Y. Kagaya, Y. Tsubakishita, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Toyonaka, Osaka, Japan

1993-198: DEVELOPMENT OF ION THRUSTER SYSTEM FOR INTERPLANETARY MISSIONS; Hitoshi Kuninaka, Institute of Space and Astronautical Science, Yoshinodai, Sagamihara, Kanagawa, Japan; Nobuo Hiroe, Kazuto Kitaoka, and Yoshio Ishikawa, Nihon University, Narashinodai, Funabashi, Chiba, Japan; Kazutaka Nishiyama, University of Tokyo, Hongo Bunkyo, Tokyo, Japan; and Yasuo Horiuchi, NEC, Ikebe, Midori, Yokohama, Kanagawa, Japan

1993-200: A MISSION TO PLUTO USING NUCLEAR ELECTRIC PROPULSION; D. G. Feam, Defence Research Agency, Farnborough

1993-202: MISSION FACTORS AFFECTING COST OPTIMIZATION OF SOLAR ELECTRIC ORBITAL TRANSFER VEHICLES; Todd M. Miller and G. Brian Seaworth, McDonnell Douglas Aerospace, Huntington Beach, California

1993-203: OPERATIONAL REQUIREMENTS FOR COST EFFECTIVE PAYLOAD DELIVERY WITH SOLAR ELECTRIC PROPULSION; K. P. Zondervan and A. K. Chan, The Aerospace Corporation, P. O. Box 92957, M4/943, Los Angeles, CA 90009-2957; C. A. Feuchter, Office of Aerospace Studies, 3550 Aberdeen Ave SE, Kirtland AFB, Albuquerque, NM 87117-5776; and W. B. Smith, Space and Missile Systems Center, Los Angeles AFB, P. O. Box 92960, Los Angeles, CA 90009-2960

1993-204: CENTAUR-DERIVED PROPELLANT SUPPLY SYSTEM FOR A SOLAR ELECTRIC ORBIT TRANSFER VEHICLE; J. R. Schuster, J. R. LeMay, E. P. Morss, and G. E. Williams, General Dynamics Space Systems Division, San Diego, California

1993-205: HIGH ALTITUDE ORBIT RAISING WITH ON-BOARD ELECTRIC POWER; B. Free, Scionics, Inc.

1993-206: EFFECT OF VOLUME CONSIDERATIONS ON THE DESIGN OF AN ELECTRIC ORBITAL TRANSFER VEHICLE; G. Brian Seaworth and Todd M. Miller, McDonnell Douglas Aerospace, Space Systems, Huntington Beach, California

1993-207: THE EFFECT OF SOLAR ARRAY DEGRADATION IN ORBIT-RAISING WITH ELECTRIC PROPULSION; A. M. Fitzgerald, Orbital Sciences Corporation, Space Data Division, Chandler, AZ

1993-208: LOW POWER GROUND BASED LASER ILLUMINATION FOR ELECTRIC PROPULSION APPLICATIONS; M. LaPointe and S. Oleson, Sverdrup Technology, Inc., Brookpark, OH

1993-209: LIQUID SPACE OPTICAL THEORY OF MANNED STARFLIGHT WITH EARTHLY APPLICATIONS; J. H. Bloomer, Discraft Corp., Portland, OR, U.S.A.

1993-210: HIGH SPECIFIC IMPULSE EXPERIMENTS WITH 1.5 AND 5KW THERMAL ARCJETS; M. Riehle, H. L. Kurtz, and M. Auweter-Kurtz, IRS - Institut für Raumfahrtsysteme, Universität Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Germany

1993-211: PERFORMANCE OF ADVANCED CONCEPT HYDROGEN ARCJET ANODES; G. W. Butler, R. J. Cassady, W. A. Hoskins, D. Q. King, and A. E. Kull, Rocket Research Company, Redmond, Washington

1993-213: PARAMETRIC TEST RESULTS OF A LOW POWER ARCJET; G. Capecchi, F. Scortecci, F. Repola, and M. Andrenucci, Centrospazio, Pisa 56104, Italy

1993-214: COMPARISON OF EXPERIMENTAL AND NUMERICAL RESULTS FOR RADIATION COOLED AND WATER COOLED HYDROGEN ARCJETS; Trevor M. Moeller, Dennis Keefer, and Robert P. Rhodes, Center for Laser Applications, The University of Tennessee Space Institute, Tullahoma, TN 37388-8897

1993-215: HYDROGEN ARCJET TECHNOLOGY STATUS; Francis M. Curran, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH 44135; and Leonard H. Caveny, Ballistic Missile Defense Organization, Innovative Science and Technology, Washington, DC 20301-7100

1993-216: MEASUREMENT OF ENERGY DEPOSISTION MODES IN AN INTERMEDIATE POWER HYDROGEN ARCJET; W. A. Hoskins, A. E. Kull, W. M. Nesser, and G. W. Butler, Rocket Research Company, Redmond, WA 98073

1993-217: NON-EQUILIBRIUM MODELING OF HYDROGEN ARCJET THRUSTERS; Robert Rhodes and Dennis Keefer University of Tennessee Space Institute, Center for Laser Applications; Tullahoma, TN 37388-8897

1993-218: NONEQUILIBRIUM NUMERICAL SIMULATION OF RADIATION-COOLED ARCJET THRUSTERS; S. A. Miller and M. Martinez-Sanchez, Space Power and Propulsion Laboratory, Dept. of Aeronautics and Astronautics, MIT, Cambridge, MA 02139

1993-219: AXIAL EMISSION DIAGNOSTICS OF A LOW POWER HYDROGEN ARCJET THRUSTER; P. Victor Storm and Mark A. Cappelli, High Temperature Gasdynamics Laboratory, Department of Mechanical Engineering, Stanford University, Stanford, California, USA

1993-220: A DIRECT COMPARISON OF HYDROGEN ARCJET THRUSTER PROPERTIES TO MODEL PREDICTIONS; M. A. Cappelli, J. G. Liebeskind, and R. K. Hanson, High Temperature Gasdynamics Laboratory, Department of Mechanical Engineering, Stanford University, Stanford, California; G. W. Butler and D. Q. King, Olin Rocket Research Company, Redmond, Washington

1993-221: DEVELOPMENT AND TESTING OF A 100 KW RADIATION COOLED THERMAL HYDROGEN ARCJET THRUSTER; Thomas M. Gölz, Monika Auweter-Kurtz, and Helmut L. Kurtz, Institut für Raumfahrtsysteme, Universität Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Federal Republic of Germany

1993-222: DEVELOPMENT AND INVESTIGATION OF CHARACTERISTICS OF INCREASED POWER SPT MODELS; B. A. Arkhipov, N. A. Maslennikov, and V. M. Murashko, Design Buro “Fakel,” Kaliningrad (obl), Russia; A. N. Veselovzorov, A. I. Morozov, and I. B. Pokrovski, I. V. Kurchalov’s Research Institute of Atomic Energy, Moscow, Russia; V. M. Gavryushin and S. A. Khartov, Moscow Aviation Institute (MAI), Moscow, Russia; V. Kim and V. I. Kozlov, Research Institute of Applied Mechanics and Electrodynamics of MAI, Moscow, Russia

1993-223: DEVELOPMENT STATUS OF THE SPT MK II THRUSTER; D. Valentian, SEP, GPPE, Melun Villaroche, France; A. Bugrova, Mirea, Moscow, Russia; and A. Morozov, Institute of Atomic Energy, Moscow, Russia

1993-225: DEVELOPMENT OF A 4 KW HALL-TYPE ELECTRIC THRUSTER; A. S. Koroteev, V. A. Petrosov, V. I. Baranov, and A. I. Vasin, The Scientific-Research Institute of Thermal Processes, Moscow, Russia; J. R. Wetch, and S. P. Wong, International Scientific Products, San Jose, CA, USA

1993-226: THEORETICAL AND EXPERIMENTAL ANALYSIS OF STATIONARY PLASMA THRUSTER OPERATION; D. Valentian and J. P. Bugeat, SEP, GPPE, Melun Villaroche, France; R. Tchuyan, S. Khartov, L. Latyshev, and V. Sierovaiskiy, Moscow Aviation Institute, Moscow, Russia; G. Cirri, Proel, Florance, Italy

1993-228: ANODE LAYER THRUSTERS, STATE OF THE ART AND PERSPECTIVES; V. I. Garkusha, E. A. Lyapin, A. V. Semyenkin, and S. O. Tverdokhlebov, Central Research Institute of Machine Building, Kaliningrad (Moscow Region), Russia

1993-230: TWO-DIMENSIONAL NUMERICAL MODEL OF PLASMA FLOW IN A HALL THRUSTER; Kimiya Komurasaki, Nagoya University, Chikusa-ku, Nagoya 464-01, Japan; and Yoshihiro Arakawa, University of Tokyo, Bunkyo-ku, Tokyo 113, Japan

1993-231: INVESTIGATION OF EROSION IN ANODE LAYER THRUSTER AND ELABORATION HIGH LIFE DESIGN SCHEME; A. V. Semenkin, Central Research Institute of Machine Building, Kaliningrad (Moscow Region), Russia

1993-232: STUDY OF DOUBLE-STAGE ANODE LAYER THRUSTER USING INERT GASES; Sergey O. Tverdokhlebov, Central Research Institute of Machine Building Kaliningrad (Moscow Region), Russia

1993-233: ON USE OF ALKALI METALS AS SPT PROPELLANTS; V. A. Petrosov, V. I. Baranov, A. I. Vasin, and Yu S. Nazarenko, The Scientific-Research Institute of Thermal Processes, Moscow, Russia

1993-234: MEASUREMENTS OF THE ELECTROMAGNETIC EMISSIONS FROM THE T5 ION THRUSTER; S. Chanda and F. Mawdsley, ERA Technology Ltd., Leatherhead, UK; R. D. Brown, Matra Marconi Space UK Ltd., Portsmouth, UK; S. D. Watson, AEA Technology, Culham Laboratory, Abingdon, UK; A. K. Malik, Imperial College, London, UK; and D. G. Feam, Defence Research Agency, Farnborough, Hampshire, UK

1993-235: BEAM CHARACTERISTICS EVALUATION OF ETS-VI XENON ION THRUSTER; Haruki Takegahara and Yukikazu Kasai, Tokyo Metropolitan Institute of Technology; Yoshifumi Gotoh, Mitsubishi Electric Corporation; Katsuhiro Miyazaki, Yukio Hayakawa, and Shoji Kitamura, National Aerospace Laboratory; Hiroshi Nagano and Kunio Nakamaru, National Space Development Agency of Japan

1993-236: ELECTRIC PROBE MEASUREMENTS IN THE PLUME OF THE UK-10  ION THRUSTER; P.C.T. de Boer, The Aerospace Corporation, P. O. Box 92957, Los Angeles, CA 90009-2957

1993-237: MICROWAVE DIAGNOSTICS FOR ION ENGINES: S. W. Janson, Technology Operations, Mechanics and Materials Technology Center, The Aerospace Corporation, Los Angeles, California

1993-239: THE EFFECT OF PROPELLANT SELECTION ON THE PERFORMANCE OF SPACE MISSIONS USING THE UK-25 INERT GAS ION THRUSTER; C. H. Edwards and S. B. Gabriel, Dept. Aeronautics and Astronautics, University of Southampton, Southampton, Hampshire, S09 5NH, UK

1993-242: PLASMA PARTICLE SIMULATION IN CUSPED ION THRUSTERS; Miharu Hirakawa and Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, Tokyo, Japan

1993-243: PLASMA PROPERTIES AND IGNITION CHARACTERISTICS OF RF ION SOURCE; Haruki Takegahara, Takeshi Ohyama, Kosuke Iwakura, and Toshiaki Iwata, Department of Aerospace Engineering, Faculty of Engineering, Tokyo Metropolitan Institute of Technology, Hino, Asahigaoka 6-6, Tokyo, 191, Japan

1993-244: HIGH SPEED ION SOURCE FOR SPACE EXPERIMENT APPLICATION; V. G. Grigorian, S. A. Kalitin, V. A. Obukhov, and M. M. Shalamov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute, Moscow Aviation Institute, Russia, 125871, Moscow, Volokolamskoe shosse, 4

1993-246: PLASMA CONTRACTOR DEVELOPMENT FOR SPACE STATION; M. J. Patterson, J. A. Hamley, and C. Sarmiento, NASA Lewis, Cleveland, OH; D. Manzella, T. Sarver-Verhey and G. Soulas, Sverdrup Technology, Brookpark, OH; A. Nelson, Purdue University, West Lafayette, IN

1993-247: MAIN FEATURES OF PHYSICAL PROCESSES IN STATIONARY PLASMA THRUSTERS; A. I. Bugrova, A. V. Desiatskov, V. K. Kharchevnikov, and A. I. Morozov, MIREA, Moscow, Russia

1993-249: NUMERICAL SIMULATIONS OF HYDROGEN ARCJET PERFORMANCE; G. W. Butler, A. E. Kull, and D. Q. King, Rocket Research Company, Redmond, Washington

1993-250: POWER CONSOLE DEVELOPMENT FOR NASA’S ELECTRIC PROPULSION OUTREACH PROGRAM; Luis R. Pinero, Michael J. Patterson, and Vincent E. Satterwhite, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135

1993-251: OPERATION OF A BRASSBOARD PCU WITH A LOW POWER ARCJET; R. Di Stefano and W. D. Deininger, BPD Difesa e Spazio, Colleferro, Italy; G. Parisi and E. Detoma, FIAT CIEI – SEPA, Torino, Italy

1993 FILE DIRECTORY

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IEPC1993-Index

IEPC1993-Mailing.List.pdf  17:36  3.3M

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IEPC1993-Vols1-3_Index.pdf 07-Jul-2008 13:40  7.4M

1995 INDEX

1995-01: ELECTRIC PROPULSION DEVELOPMENT AND APPLICATION IN THE UNITED STATES; R. Rhoads Stephenson, JPL California Institute of Technology, USA

1995-02: REVIEW OF ELECTRIC PROPULSION ACTIVITIES IN JAPAN; Shoji Kitamura, National Aerospace Labortory, Japan

1995-04: ADVANCED INTERPLANETARY MISSION OF THE XXI CENTURY USING ELECTRIC PROPULSION; H. Loeb, Institute of Physics, Giessen University, Germany; G. Popov, Research Institute of Applied Mechanics and Electrodynamics, Russia

1995-05: ELECTRIC PROPULSION THRUSTERS AND PLASMODYNAMICS; Alexei Morozov, RSC, Kurchatov Institute, Russia

1995:06: SPT IN RUSSIA – NEW ACHIEVEMENTS; A. S. Bober and N. A. Maslennikov, EDB “Fakel” Kaliningrad, Russia

1995-07: MAI INVESTIGATIONS AND DEVELOPMENT IN THE ERT FIELD; M. P. Burgasov and L. A. Latyshev, MAI, Russia; V. P. Kim, G. A. Popov, and V. B. Tikhonov, RIAME MAI, Russia

1995-08: NIITP’S ACTIVITY IN THE FIELD OF ELECTRIC PROPULSION; A. S. Koroteev and V. A. Petrosov, NIITP, Russia

1995-09: ELECTRIC PROPULSION ACTIVITY IN TSNIMASH; T. I. Garkusha, A. V. Semenkin, and S. G. Mironov, TsNIIMASH, Russia; V. V. Savitsev, and D. Grishin, Moscow State Technology University, Russia

1995-010: VNIIEM ACTIVITY IN THE FIELD OF EPE; Yu. V. Trifonov and V. P. Khodnenko, NPP VNIIEM, Russia; R. S. Salikhov, G. A. Avatinyan, and Yu P. Rylov, NIIEM (Instra. Moscow Region), Russia

1995-011: EXPERIENCE OF FLIGHT OPERATION OF ELECTRIC PROPULSION SUBSYSTEMS WITH STATIONARY PLASMA THRUSTERS ON SPACECRAFTS DEVELOPED BY NPO PM; A. G. Kozlov, V. F. Petrusevitch, V. A. Rayevsky, A. V. Romashko, and Y. M. Yermoshkin, NPO PM (Krasnoyarsk), Russia

1995-012: THE REVIEW OF THE WORKS ON ELECTRICAL PROPULSION THRUSTERS DEVELOPMENT AND INVESTIGATION. CARRIED OUT AT THE DNEPROPETROVSK STATE UNIVERSITY; V. F. Prysniakov, A. N. Petrenko, A. M. Kapulkin, I. N. Statsenko, A. I. Kondratiev, and S. N. Kulagin

1995-014: HIGH POWER ARCJET EXPERIMENTS AND ANALYSIS; Thomas M. Gölz, Monika Auweter-Kurtz, Helmut L. Kurtz, and P. Christian Sleziona, Institut für Raumfahrtsysteme, Universität Stuttgart, Pfaffenwaldring 31, 70550 Stuttgart FRG

1995-015: INVESTIGATION OF ELECTRON ENERGY DISTRIBUTIONS IN AN MPG ARCJET FLOW WITH ELECTROSTATIC PROBES; Harald A. Habiger, Monika Auweter-Kurtz, and Helmut Kurtz, Institut für Raumfahrtsysteme, Universität Stuttgart, Pfaffenwaldring 31, 70550 Stuttgart, Germany

1995-016: PLASMA FEATURES IN A MEDIUM-POWER ARCJET; Hirokazu Tahara, Kazuhito Komiko, Lulu Zhang, Ken-Ichi Onoe, and Takao Yoshikawa, Osaka University, Japan

1995-017:  DEVELOPMENT AND TESTING OF A 300W-CLASS ARCJET; Kazuhiko Ogiwara and Satoshi Hosoda, Tokai University, Japan; Takao Suzuki, Stanford University, Japan; Kyoichiro Toki and Kyoichi Kuriki, Institute of Space and Astronautics Sci., Japan; Shinobu Matsuo, Mitsubishi Heavy, Ind. LTD, Japan; Hideaki Nanri, and Hiroshi Nagano, National Space Develop. Agency of Japan

1995-018: LOW POWER ARCJET PERFORMANCE EVALUATION; Keith A. McFall, Dennis L. Tilley, and Frank S. Gulczinski III, Phillips Laboratory, Edwards AFB, CA 93524

1995-020: NUMERICAL AND EXPERIMENTAL STUDIES OF HYDROGEN AND NITROGEN FLOWS IN RESISTOJET; Iain D. Boyd and Douglas B. VanGilder, School of Mechanical and Aerospace Engineering, Cornell University, Ithaca, NY, USA; Edward j. Beiting and Ronald B. Cohen, Aerospace Corporation, Los Angeles, CA, USA; Eric J. Pencil, NASA Lewis Research Center, Cleveland, OH, USA; and Steven D. Hirsch,  Worcester Polytechnic Institute, Worcester, MA, USA

1995-022:  SIMPLE ESTIMATION OF THE PERFORMANCE OF A LOW POWER ARCJET THRUSTER; Michio Nishida and Hiroyuki Okamoto, Kyushu University, Japan

1995-024: SEMIEMPIRICAL PREDICTION TECHNIQUE OF PERFORMANCE PARAMETERS FOR ARCJET PLASMA GENERATOR; E. P. Vaulin, E. A. Baranova, and J. V. Demonenko, Moscow Aviation Institute, Russia; V. A. Obukhov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute, Moscow, Russia; F. Scortecci, Centrospazio, Pisa, Italy

1995-025: NUMERICAL PREDICTION OF ARCJET PERFORMANCE BASED ON THE CHEMICAL KINETICS AND ELECTRON TEMPERATURE DISPARITY; Kazuhisa Fujita and Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, Hongo 7-3-1, Tokyo, 113 Japan

1995-026: NUMERICAL ANALYSIS OF NONEQUILIBRIUM PLUME OF AN ARCJET THRUSTER; N. Nishida, y. Yamamoto, Kyushu University, Japan; M. Matsumoto, Res. Inst. Ishikawajima-Harima Heavy Ind. Co. Ltd., Japan

1995-028: LASER INDUCED FLUORESCENCE OF GROUND STATE HYDROGEN ATOMS IN AN ARCJET PLUME; Jeffrey A. Pobst, and Ingrid J. Wysong, Ronald A. Spores, Propulsion Directorate, OL-AC Phillips Laboratory, Edwards AFB, CA 93524

1995-029: STUDY AND DIAGNOSTICS OF THE EFFECT OF LENGTH VARIATION IN HALL THRUSTERS; J. Ashkenazy, Y. Raitses, and G. Appelbaum, SOREQ NRC, Israel; and M. Guelman, Tech. I.I.T., Israel

1995-030: PERFORMANCE EVALUATION OF A 4.5 KW SPT THRUSTER; John M. Sankovic and Thomas W. Haag,NASA Lewis R. C. USA; and David H. Manzella, NYMA Inc. USA

1995-031: INVESTIGATION 4.5 KW HIGH EFFICIENCY HALL-TYPE T-160 ELECTRIC THRUSTER; V. A. Petrosov, A. I. Vasin, and V. I. Baranov, NIITP, Russia; J. R. Wetch, E. J. Britt, S. P. Wong, and R. Lin, Inter. Sci. Product, USA

1995-032: INVESTIGATION OF SMALL, CLOSED ELECTRON DRIFT, SPT.; G. Guerrini and M. Bacal, Ecole Polytechnique, France; A. N. Vesselovzorov, RSC “Kurchatov. Inst. “, Russia

1995-033: OPTIMIZATION OF CHANNEL CONFIGURATION OF HALL THRUSTERS; Kenji Mikami, Kimiya Komurasaki, and Toshi Fujiwara, Nagoya Unv., Japan

1995-034: SIMPLIFIED NUMERICAL DESCRIPTION OF SPT OPERATION; David H. Manzella, NYMA Inc. USA

1995-035: DEVELOPMENT OF A SECOND GENERATION OF SPT; J. P. Bugeat and C. Koppel, SEP, France

1995-036: PRESENT AND NEAR FUTURE APPLICATIONS OF SPT M-2 THRUSTERS; D. Valentian and C. Koppel, SEP, France

1995-037: DISSIPATIVE METHOD OF SUPPRESSION OF ELECTRON DRIFT INSTABILITY IN SPT; Aleksandr M. Kapulkin, and Valdimir F. Prisnyakov, Onepropetr. State Univ., Ukraine

1995-038: PHYSICAL AND TECHNICAL BASES OF THE MODERN SPT DEVELOPMENT; V. M. Gavryshin, MAI, Russia; V. Kim and V. I. Kozlov, RIAME MAI, Russia; and N. A. Maslennikov, EDB “Fakel”, Russia

1995-039: THE RESULTS OF 7000-HOUR SPT-100 LIFE TESTING; B. A. Arhipov, A. S. Bober, R. Y. Gnizdor, K. N. Kozubsky, A. I. Korakin, N. A. Maslennikov, and S. Y. Pridannikov, EDB “FAKEL”, Kaliningrad, Russia

1995-041: A 2000 HOURS LIFETIME TEST RESULTS OF 1.3 KW T-100 ELECTRIC THRUSTER; V. A. Petrosov, A. I. Vasin, and V. I. Baranov, NIITP MAI, Russia; J. R. Wetch, E. J. Britt, S. P. Wong, and R. Lin, Inter. Sci, Product, USA

1995-042: THE ELECTRON DYNAMICS IN SPT-CHANNEL AND THE PROBLEM OF ANOMALOUS EROSION; A. I. Morozov, RSC “Kurchatov Institute”, Russia;  V. V. Savelyev, Inst. Appl. Mathem., Russia

1995-043: THE MECHANISM OF ANOMALOUS EROSION IN ACCELERATORS WITH CLOSED DRIFT OF ELECTRONS; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, A. I. Vasin, and Yu. M. Yashnov, NIITP, Russia

1995-044: NEW CONCEPTIONS OF OSCILLATION MECHANISMS IN THE ACCELERATOR WITH CLOSED DRIFT OF ELECTRONS; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, A. I. Vasin, and Yu. M. Yashhnov, NIITP, Russia

1995-045: INVESTIGATION OF THE SPT PERFORMANCE IMPROVEMENT POSSIBLITITY; Vladimir Kim, Vitaly Egorov, Vyacheslav Kozlov, and Garry Popov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), Moscow, Russia; Theodor Colbert and Michael Day, Space Systems/Loral, Palo Alto, USA; Sergei Khartov, Moscow Aviation Institute, Moscow, Russia; Nicolay Maslennikov and Alexander Nesterenko, Design Bureau “Fakel”, Kalinningrad (obl.), Russia

1995-046: INFLUENCE OF VACUUM CONDITIONS ON THE SPT OPERATION; A. I. Bugrova, MIREA, Russia;  A. I. Morozov, RSC “Kurchatov. Inst.”, Russia

1995-047: EXPERIMENTAL DETERMINIATION OF ION ENERGY AT THE OUTLET OF SPT-ATON; A. I. Bugrova, A. V. Desyatskov, and V. K. Kharchevnikov, MIREA, Russia

1995-048: THE POSSIBILITY OF NEARANODE PROCESS CONTROLLING FOR PERSPECTIVE SPT MODELS; A. Jakupov, S. Khartov and L. Latyshev, MAI, Russia

1995-050: ELECTRON-CURRENT GAIN IN DISCHARGE IN A TRANSVERSE MAGNETIC FIELD; A. V. Zharinov, V. I. Lenin All-Russian Electrotechnical Institute, Moscow, Russia

1995-051: EXPERIMENTAL STUDY OF EXHAUST BEAM OF ANODE LAYER THRUSTER; B. S. Borisov, K. K. Mikhaylov, A. V. Rusakov, A. V. Semenkin, and H. O. Chislov, Central Research Institute of Machine Building (TsNIIMASH), Kaliningrad, Moscow Region

1995-052: SOME RESULTS OF INVESTIGATION OF ANODE DESIGN INFLUENCE ON ANODE LAYER THRUSTER CHARACTERISTICS; Sergey N. Kulagin, Ivan N. Statsenko, Vladimir N. Serebryansky, Dnepropetr. State Univ., Ukraine; Alexandr N. Semenkin, TsMIIASH, Russia

1995-054: PROSPECTS FOR USING METALS AS PROPELLANT IN STATIONARY PLASMA ENGINES OF HALL-TYPE; V. G. Gnedenko and V. A. Petrosov, NIITP, Russia; A. V. Trofimov, RSC “Kurchatov Inst.”, Russia

1995-055: THE ENGINEERING METHOD OF THE SPT INTEGRAL PARAMETERS CALCULATIONS; A. Rudikov and V. Tikhonov, RIAME MAI, Russia

1995-056: ON PLASMA FLOW INSTABILILTY IN CDEA (FOR THE EXPERIMENT); E. B. Svirsky, RSC “Kurchatov Institute”, Russia

1995-057: STATIONARY PLASMA HALL THRUSTER LIFETIME PREDICTION; A. A. Kalyaev, V. A. Petrosov, and V. I. Baranov, NIITP, Russia

1995-058: DIFFUSION MODEL OF THE CONDUCTION IN THE IONIZATION ZONE OF THE CLOSED ELECTRON DRIFT ACCELERATOR; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, A. I. Vasin, and Yu. M. Yashnov, NIITP, Russia

1995-059: THE IONIZATION OSCILLATIONS MECHANISM IN ACD; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, A. I. Vasin, and Yu. M. Yashnov; NIITP, Russia

1995-060: THE SPT CHANNEL EROSION MODEL; V. A. Petrosov, V. I. Baranov, A. I. Vasin, A. A. Kaliaev, and Y. S. Nazarenko; NIITP, Russia

1995-061: ELECTRON DISTRIBUTION FUNCTION IN ACCELERATOR WITH CLOSED ELECTRON DRIFT; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, A. I. Vasin, and Yu. M. Yashnov, NIITP, Russia

1995-062: ELECTRON DRIFT OSCILLATIONS OUTSIDE ACCELERATION ZONE OF ACCELERATOR WITH CLOSED ELECTRON DRIFT; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, A. I. Vasin, and Yu. M. Yashnov; NIITP, Russia

1995-063: THERMOVISION STUDY OF TEMPERATURE FIELDS AND RADIATION CHARACTERISTICS OF ELECTRIC THRUSTER T0100 SURFACES; A. F. Anikin, S. M. Bednov, A. N. Golikov, and M. V. Yasinsky, NIITP, Russia

1995-064: OPTIMIZATION OF PLANS FOR ACCELERATED ENDURANCE TESTS FOR RELIABILITY; A. A. Kalyaev and V. G. Lebedev, NIITP, Russia

1995-065: STATIONARY PLASMA HALL THRUSTER ACCEPTANCE ACCELERATED TESTS; A. A. Kalyaev, NIITP, Russia

1995-066: INFLUENCE OF TARGET SPUTTERING ON THRUSTER PARAMETERS; A. I. Bugrova, A. S. Lipatov, and D. V. Churbanov, MIREA, Russia; A. I. Morozov, RSC “Kurchatov Institute”, Russia

1995-067: SPT-ATON TESTS AT KURCHATOV INSTITUTE STANDS; A. I. Bugrova, A. C. Lipatov, V. K. Kharchevnikov, and D. V. Churbanov, MIREA, Russia; A. I. Morozov, RSC “Kurchatov Institute”, Russia

1995-068: LIGHT SPECTRUM OF SPT-ATON PLASMA JET; J. A. Ermakov, M. V. Kozintzeva, and P. V. Kolenko, MIREA, Russia

1995-069: PROBE INVESTIGATIONS OF THE DISCHARGE RECONSTRUCTION AT THE DUSTING OF THE CHANNEL WORK SURFACES; A. I. Bugrova, A. V. Desyatskov, and V. K. Kharchevnikov, MIREA, Russia; A. I. Morozov, RSC “Kurchatov Institute”, Russia

1995-070: CHEMICAL CHARACTERISTICS OF THE FILMS, APPEARED ON THE ANODE SURFACE OF SPT; A. I. Bugrova, A. S. Lipatov, Y. V. Titov, MIREA, Russia; D. Valentian, SEP, France

1995-071: THE INFLUENCE OF INPURITES ON SPT-ATON THRUSTER OPERATION; A. V. Desyatskov, M. V. Kozintzeva, and A. S. Lipatov, MIREA, Russia

1995-072: NEUTRAL DYNAMICS IN SPT CHANNEL; A. P. Ahubin, RSC “Kurchatov Institute”, Russia

1995-073: ELECTROMAGNETIC INTERFERENCE MEASUREMENTS WITHIN THE T-100 ENDURANCE TEST; V. I. Brukhty, NIITP, Russia; K. P. Kirdyashev, O. E. Svetlitskaya, Inst. Radioeng. and Electron. (Fryazino, Moscow Region), Russia

1995-074: OPTMIZATION OF THE PARAMETERS BY PROGRAM FOR (SSTC) OF EPS AND EPT; A. V. Rumiantsev, Kaliningrad State University, Russia

1995-075: LIFETIME OF THE STATIONARY PLASMA THRUSTER; N. A. Maslennikov, EDB “Fakel”, Russia

1995-077: AN OPERATION OPTIMIZING FOR BOTH ELECTRIC POWER AND PROPULSION SYSTEMS EQUIPPED WITH STATIONARY PLASMA THRUSTERS; P. O. Fedorov, A. N. Yatcina, Dnepropetr. State Univ., Ukraine

1995-078: STUDY OF ANODE LAYER THRUSTER OPERATION WITH GAS MIXTURES; A. V. Semenkin, H. O. Chislov, TsNIIMASH, Russia

1995-079: LOW-TEMPERATURE MODE OF ION ACCELERATION IN ANODE LAYER THRUSTER; A. G. Korsun TsNIIMASH, Russia

1995-080: TRANSVERSE EXPANSION OF PLASMA PLUMES AND PLASMOIDS INGECTED FROM ELECTRIC THRUSTERS; A. G. Korsun, TsNIIMASH, Russia

1995-86: A NEW FRENCH FACILITY FOR ION PROPULSION RESEARCH; P. Lasgorceix, M. Raffin, J. C. Lengrand, M. Dudeck, CNRS, France; A. Cadiou, CNES, France

1995-088: FUNDAMENTAL EXPERIMENTS OF C60 APPLICATION TO ION THRUSTER; Y. Nakayama, H. Takegahara, Tokyo Metropolitan Inst. of Tech., Japan

1995-089: 300 HOURS ENDURANCE TEST OF MICROWAVE ION THRUSTER; S. Satori, H. Kuninaka, K. Kuriki, Inst. of Space and Astr. Sci., Japan

1995-090: NUMERICAL SIMULATION OF GRID EROSION FOR ION THRUSTER; T. Shiraishi, Tokyo University, Japan; H. Kuninaka, S. Satori, and K. Kuriki, Inst. of Space and Astr. Sci., Japan

1995-091: EVALUATION OF THE T5 (UK-10) ION THRUSTER: SUMMARY OF PRINCIPAL RESULTS; M. W. Crofton, The Aerospace Corporation, USA

1995-092: PERFORMANCE OF THE PRIMARY RF-ION THRUSTER ESA-XX; P. Fahrenbach, K. H. Groh, and H. W. Loeb, Giessen University, Germany

1995-093: FABRICATION AND TESTING OF CARBON-CARBON COMPOSITE GRIDS FOR A 14 CM ION THRUSTER; S. Kitamura, K. Miyazaki, Y. Hayakawa, and Y. Nakamura, National Aerospace Laboratory, Japan; S. Yamaguchi, Hitachi Research Lab, Hitachi, Ltd., Japan

1995-094: AN ION ENGINE FOR SMALL SATELLITES; O. A. Gorshkov, V. A. Muravlev, NIITP, Russia; V. G. Grigoryan, S. V. Kanev, and V. I. Minakov, MAI, Russia

1995-095: THE NEW HIGH FREQUENCY ION THRUSTER (HFIT) DEVELOPMENT; V. B. Andreev, V. P. Kim, V. I. Kozlov, A. I. Skrylnikov, O. S. Sladkov, and V. N. Trusov, RIAME MAI, Russia; V. G. Grigoryan, MAI, Russia; G. F. Cirri, N. Kutufa, and G. Nocci, PROEL TECHN., Italy

1995-097: PULSED FEEP: NEW EXPERIMENTAL RESULTS; A. Genovese, S. Marcuccio, M. De Sio, CENTROSPAZIO, Italy; M. Andrenucci, Univ. Of Pisa, Italy

1995-098: FEEP THRUSTER PLUME INVESTIGATION WITH LANGMUIR PROBES; S. Marcuccio, A. Genovese, A. Turco, and H. J. Nick, CENTROSPAZIO, Italy; M. Andrenucci, Univ. of Pisa, Italy

1995-099: THE LOW POWER HF ION THRUSTER; T. B. Antonova, G. E. Burgrov, S. G. Kondranin, E. A. Kralkina, V. A. Obukhov, and N. F. Vorobjev, RIAME MAI, Russia; A. F. Alexandrov, Moscow State Univ., Russia; N. Kutufa, G. Noci, PROEL TECHN., Italy; A. A. Rukhadze, Inst. of General Phys. Russia

1995-100: LIFE-TIME TEST OF ESTEC OF THE RIT-10 THRUSTER FOR ARTEMIS; J. Gonzalez, G. Saccoccia, C. Bartoli, and F. van den Bos, ESA/ESTEC, The Netherlands; R. Kukies, H. Muller, Daimber Benz, Germany

1995-102: THE REVEALING OF OPTIMAL REGIMES OF HF LOW POWER UNPUT IN LIMITED MAGNETOACTIVE PLASMA FOR DEVELOPMENT OF HF ION THRUSTER OF THE NEW TYPE; T. B. Antonova, G. E. Bugrov, N. F. Vorobjev, S. G. Kondranin, E. A. Kralkina, and V. A. Obukhov, RIAME MAI, Russia; A. F. Alexandrov and A. V. Kalinin, Moscow State Univ., Russia; A. A. Rukhadze, Inst. of General Phys., Russia

1995-103: STATE OF THE ART AND FUTURE PROSPECTS OF COLLOIDAL ELECTRIC THRUSTERS; A. F. Shtyrlin, MAI, Russia

1995-104: INVESTIGATION OF ALKALI METAL MPD THRUSTERS; V. A. Petrosov, I. B. Safonov, Yu. A. Utkin, and V. N. Shutov, NIITP, Russia

1995-105: THE EXPERIMENTAL PERFORMANCES OF THE 100 KW LI MPD THRUSTER WITH EXTERNAL MAGNETIC FIELD; V. B. Tikhonov and S. A. Semenikhin, MAI, Russia; J. R. Brophy and J. E. Polk, JPL, USA

1995-106: POWERFUL QUASISTATIONARY PLASMA ACCELERATORS; V. V. Chebotarev, I. E. Garkusha, O. E. Kazakov, N. I. Mitina, D. G. Solyakov, V. I. Tereshin, S. A. Trubchaninov, and A. V. Tsarenko, Kharkov Inst. of Physics and Technology, Ukraine; A. I. Morozov, RSC “Kurchatov Institute”, Russia

1995-107: 2 MWE NEP SYSTEM WITH MPD-THRUSTER; Yu. A. Alexeev, M. N. Kazeev, A. S. Kaminski, V. S. Kuznetsov, and V. A. Pavshuk, RSC “Kurchatov Institute”, Russia

1005-108: ELECTROSTATIC INSTABILITIES OF A MAGNETOPLASMADYNAMIC THRUSTER IN THE INHOMOGENEOUS MEDIUM; K. P. Kirdyashev, Inst. Radioeng. and Electron. (Fryazino Moscow Region), Russia; J. V. Kubarev, Acad. of Eng. Sci., Russia

1995-109: EVALUATION OF CATHODE TEMPERATURE DISTRIBUTION IN A CYLINDRICAL MPD THRUSTER; M. W. Winter, M. Auweter-Kurtz, H. L. Kurtz, and P. C. Sleziona, Stuttgart University, Germany

1995-110: CATHODE HEATING EFFECTS ON THE CATHODE REGION PARAMETERS OF AN MPD THRUSTER; F. Paganucci, M. Andrenucci, and NP. Rossetti, CENTROSPAZIO, Italy

1995-111: SIX-COLOR VIDEO PYROMETRY WITH APPLICATION TO MPD THRUSTERS; E. Y. Choueiri, V. P. Chiravalle, G. E. Miller and R. G. Jahn, Princeton Univ., USA

1995-113: MAGNETIC CONTROL OF MPD ACCELERATOR JET PARAMETERS; Yu. V. Kubarev, Acad. of Eng. Sci., Russia; S. E. Rosinksy, Moscow State Acad. Instr. and Inform. Sci., Russia; I. B. Safonov and Yu. A. Utkin, NIITP, Russia

1995-114: PRELIMINARTY RESULTS ON SERVICE LIFE DEVELOPMENT OF PPT SCALE MODEL; N. N. Antropov, V. K. Gundobin, G. A. Popov, A. I. Rudikov, and S. Y. Shibanov, RIAME MAI, Russia

1995-115: PLASMA JET DYNAMIC OF COAXIAL PULSED PLASMA SOURCE OF EROSION TYPE; M. M. Orlov, A. I. Rudikov, L. A. Gomilka, I. G. Krivonosov, V. K. Gundobin, and V. N. Yakovlev, RIAME MAI, Russia

1995-116: PLASMA FEATURES IN QUASISTEADY MPD CHANNELS; H. Tahara, K. Mitsuo, L. Zhang, Y. Kagaya, and T. Yoshikaw, Osaka University, Japan

1995-118: BEHAVIOUR OF QUASI-STEADY ABLATIVE MPD THRUSTERS WITH DIFFERENT PROPELLANTS; G. Paccani and U. Chiarotti, University of Rome, Italy

1995-119: POWER PROPULSION SETS WITH PULSED PLASMA THRUSTER; V. L. Levtov, “Kompozit” Sci. and Prod. Assoc., Russia; V. V. Savitchev, Moscow State Techn. Univ., Russia

1995-120: PROPELLANT IONIZATION IN HIGH POWER MPD THRUSTERS; Ya. A. Alexeev, M. N. Kazeev, RSC “Kurchatove Institute”, Russia

1995-121: MPD THRUSTER WITH EXTERNAL MAGNETIC FIELD AND IONIZATION CHAMBER; V. B. Tikhonov and G. A. Dyakonov, RIAME MAI, Russia

1995-122: MATHEMATICAL SIMULATION FOR PPT OPERATION; L. A. Gomilka, G. A. Popov, and A. I. Rudikov, RIAME MAI, Russia

1995-123: RELEASE INTO THE SPACE OF EXCESS HEAT IN THE PERSPECTIVE HIGH POWER PLANTS; I. G. Panevin, MAI, Russia, B. N. Baushev and A. A. Koroteev, RIAME MAI, Russia

1995-124: POWER PROCESSING UNIT FOR ELECTRICAL PROPULSION THRUSTER SYSTEMS; A. I. Chernishev, Yu. A. Shinyakov, and N. M. Katasonov, GNPP “Polus” (Tomsk), Russia

1995-125: POSSIBLE STRUCTURAL-DESIGN SCHEMES OF SPACECRAFT WITH NUCLEAR-ELECTRIC PROPULSION SYSTEMS; P. V. Andreev, A. Ya. Galkin, G. M. Gryaznov, E. E. Zhabotinsky, and G. A. Zaritsky, “Krasnaya zvezda”, Russia; V. A. Kotin, R. S. Kremev, V. A. Kudryashov, and B. D. Yakovlev, Lavochkin ASSOC., Russia

1995-126: THE PROBLEM OF THE POWER PROCESSING AND TELEMETRY/CONTROL UNIT DESIGN FOR STATIONARY PLASMA THRUSTER; A. N. Petrenko, Dnepropetr. State Univ., Ukraine; J. A. Hamley and J. M. Sankovic, NASA Lewis R. C., USA

1995-128: PROJECT OF MULTIFUNCTION ELECTRIC PROPULSION PLANT FOR TRANSFERRING SPACE VEHICLES TO GEOSTATIONARY ORBIT; V. F. Prisniakov, A. I. Kondratyev, S. F. Lyagushin and I. N. Statsenko, Dnepropetr. State Univ., Ukraine; S. N. Konyukhov, DE “Pivdenne” (Dnepropetrovsk), Ukraine

1995-130: HIGH-TEMPERATURE SYSTEM OF THE ELECTRICAL CURRENT CONVERSION FOR POWERFUL ERT; V. V. Onufryev and S. D. Grishin, Moscow State Techn. Univ., Russia

1995-131: OPTIMAZTION OF THE PARAMETERS OF THE HIGH-TEMPERATURE RADIATION-RESISTANT CURRENT CONVERSION SYSTEMS FOR POWERFUL ERT; V. V. Onufryev, S. D. Grishin, and V. V. Savitchev, Moscow State Techn. Univ., Russia

1995-132: THE BMDO ELECTRIC PROPULSION FLIGHT READINES PROGRAM; L. H. Caveny, BMDO, USA; J. M. Sankovic, NASA Lewis RC, USA; D. M. Allen and G. Herbert, W. J. Shafer Ass., USA; C. E. Garner, JPL, USA

1995-133: THE NASA ELECTRIC PROPULSION PROGRAM; F. M. Curran, NASA Lewis RC, USA; L. W. Callahan, Office of Space Access and Techn., USA

1995-134: AN OVERVIEW OF THE CNES ELECTRIC PROPULSION PROGRAM; A. Cadiou and E. Gengembre, CNES, France

1995-135: ELECTRIC PROPULSION ACTIVITIES STATUS AND PLANS AT BPD. CENTROSPAZIO AND SEPA; W. D. Deininger, BPD Difesa e Spazio, Italy; M. Andrenucci, CENTROSPAZIO, Italy; E. Detoma, Div. SEPA, Italy

1995-136: TTE LEVERAGE OF ELECTRIC PROPULSION: SATELLITE PROPULSION SYSTEM TRADE-OFFS; W. D. Deininger and R. Nasi, BPD Difesa e Spazio, Italy

1995-139: ON-ORBIT PERFORMANCE OF ETS-VI ION ENGINE SUBSYSTEM; H. Hagano and K. Kajiwara, Nat. Space Devel. Agency, Japan; Y. Goton, E. Nishida, and Y. Fujita, Mitsubishi Elec. Corp. Japan

1995-142: THE PROSPECTS OF THE ELESTRIC ROCKET PROPULSION SYSTEM APPLICATIONS IN THE COMPOSITION OF THE SPACE VEHICLE TRANSPORT POWER MODULES; V. A. Menshikov, S. P. Zatserkovny, A. I. Kuzin, A. V. Malygin, K. A. Pavlov, and G. A. Shevtsov, Centr. Sci. Inst. of Space Force of Russia

1995-145: PROSPECTS FOR USE OF HIGH-POWER ION ENGINES IN THE OBJECTS OF DEVELOPING OF NEAR AND FAR SPACE; V. N. Akimov, O. A. Gorshkov, and Yu. M. Es’kov, NIITP, Russia

1995-147: SCALING LAWS FOR PULSED ELECTRIC PROPULSION WITH APPLICATION TO THE PLUTO EXPRESS MISSION; J. K. Ziemer, E. Y. Choueiri, and R. Jahn, Princeton Univ., USA

1995-148: THE CASE FOR SMALL SPACECRAFT: AN INTEGRATED PERSPECITIVE ON ELECTRIC PROPULSION; D. Barnhart, R. Wojnar, D. Tilley, and R. Spores, Phillips Laboratory, Edwards AFB, USA

1995-149: ACTIVE WAY OF REDUCING MICROACCELERATIONS OF SPACECRAFT BY USING ELECTRIC THRUSTERS; K. V. Evdokimov, V. G. Grigoryan, A. A. Izmaylov, S. A Khartov, L. A. Latyshev, and A. V. Shtyrlin, MIA, Russia; S. L. Ivanov and V. A. Kudryashov, NPO Lavochkin, Russia; V. V. Savichev, Moscow State Techn. Univ., Russia

1995-150: RF SHADOWS PRODUCED BY PLASMA PLUMES AND PLASMOIDS OF ELECTRIC THRUSTERS; F. F. Gabdullin, V. I. Garkusha, A. G. Korsun, and E. M. Tverdokhlebova, TsNIIMASH, Russia

1995-151: ELECTROMAGNETIC WAVES RADIATED BY ION BEAM INJECTED TO IONOSPHERE; G. G. Shishkin, RIAME MAI, Russia

1995-152: INTEGRATION OF ELECTROTHERMAL ENGINES WITH “ELECTRO” SPACECRAFT; V. P. Khodnenko, NPP VNIEM, Russia

1995-155: SELECTION OF ELECTRIC THRUSTER OF SUSTAINER PROPULSION SYSTEM FOR MARTIAN ORBITAL AND LANDING MISSION; M. N. Vatel, O. A. Gorshkov, and V. F. Semyonov, NIITP, Russia

1995-156: COMPARATIVE ANALYSIS OF THE PROPULSION SYSTEM FOR THE SMALL SATELLITES; G. Malyshev, V. Kulkov, A. Shtyrlin, I. Vyshedkevich, and R. Bychkov, RIAME MAI, Russia

1995-157: NUMERICAL INVESTIGATION OF COMPRESSION FLOWS IN A PLASMA ACCELERATOR CHANNEL; K. V. Brushlinsky, Inst. Appl. Mathem, Russia; G. A. Kalugin, Moscow Engin. Phys. Inst. Russia

1995-158: NUMERICAL SIMULATION OF MHD FLOWS WITH THE HALL EFFECT IN THE HIGH CURRENT QUASI-STEADY-STATE PLASMA ACCELERATOR (QSPA); K. V. Brushlinksy, K. P. Gorshenin, and T. A. Ratnikova, Inst. Appl. Mathem, Russia

1995-159: PROGRESS IN MODELING PLASMA THRUSTERS AND RELATD PLASMA FLOWS; P. J. Turchi, P. G. Mikellides, K. W. Hohman, R. J. Leiweke, I. G. Mikellides, and C. S. Schmahl, Ohio State University, USA; N. F. Roderick, University of New Mexico, USA; R. E. Peterkin, Phillips Lab., USA

1995-160: AXISYMMETRIC PIC-DSMC SIMULATIONS OF SPT PLUMES; D. Oh and D. Hastings, Massachusetts Inst. of Tech., USA

1995-161: NUMERICAL SIMULATION OF PLASMA FLOW DYNAMICS IN SPT; A. I Morozov, RSC “Kurchatov Institute”, Russia; V. V. Savelyev, Inst. Appl. Math., Russia

1995-162: NUMERICAL STUDY OF ION THRUSTER PLUME-SPACECRAFT INTERACTIONS; R. I. SAMANTA Roy, and D. E. Hastings, Massachusetts Inst. of Tech., USA; N. A. Gatsonis, Worcester Polytech. Inst., USA

1995-163: ION BEAM SIMULATION IN A SPACECRAFT ENVIRONMENT; K. K. Krupnikov, V. N. Mileev, L. S. Novikov, and V. V. Sinolits, Inst. of Nucl. Phys. Moscow State Univ., Russia

1995-164: PARTICLE SIMULATION OF PLASMA PHENOMENA IN HALL THRUSTERS; M. Hirakawa, Tokai University, Japan; Y. Arakawa, University of Tokyo, Japan

1995-168: NUMERICAL INVESTIGATION OF MPD THRUSTERS WITH UNSTRUCTURED MESH METHODS; C. Bole, M. Auweter-Kurtz, H. J. Kaeppeler, and P. C. Sleziona, Stuttgart University, Germany

1995-169: AN EFFICIENT NUMERICAL ANALYSIS OF FULLY IONIZED PLASMA FLOWS IN A SELF-FIELD MPD THRUSTER; T. Miyasaka and T. Fujiwara, Nagoya University, Japan

1995-170: THE NUMERICAL SIMULATION OF A JET OF RAREFIED PLASMA OUTFLOWING FROM THE AXIAL AND RING ORIFICES; L. A. Bazima, A. I. Oransky, and V. A. Pimkin, Khartov Aviation Inst., Ukraine

1995-171: PLUME MODEL OF HALL EFFECT PLASMA THRUSTERS WITH TEMPORAL CONSIDERATION; J. Dickens, M. Kristiansen, and E. O’Hair, Texas Tech. University, USA

1995-172: PROGRAM PACKAGE FOR THE CALCULATION OF SATELLITE ANTENNA PATTERN CHARACTERISTICS DURING THE OPERATION OF VERNIER ENGINES ON THE BASIS OF EP; V. G. Malko and A. P. Plokhikh, RIAME MAI, Russia; G. G. Shishkin, MAI, Russia; A. Soubeyran, Matra Marcony Space Comp., France

1995-173: THE THEORETICAL INVESTIGATION OF SURROUNDING GAS PRESSURE INFLUENCE ON THE SPT PLASMA JET PARAMETERS; A. M. Bishaev, V. K. Kalashnikov, V. Kim, and A. V. Shavikina, RIAME MAI, Russia

1995-174: THE INVESTIGATION OF THE TEMPERATURE FIELD IN THE SPT STRUCTURE ELEMENTS; S. Khartov, V. Serovaisky, A. Smakhtin, and R. Tchuyan, MAI, Russia; D. Valentian, SEP, France

1995-175: THE NUMERICAL MODELING OF PLASMA FLOW IN MPD THRUSTER; N. Barabanov, MAI, Russia

1995-176: NUMERICAL SIMULATION OF THE FLOW STRUCTURE OF THE HEAVY PARTICLES IN SPT; Yu. A. Ermakov, MIREA, Russia

1995-177: MATHEMATICAL MODELING OF CHARGED PARTICLES TRANSFER PROCESSES NEAR THE SURFACE IN JETS OF ELECTRIC PROPULSION ENGINES; M. V. Kotelnikov and A. V. Shankov, MAI, Russia

1995-178: CERAMIC COATINGS USING QUASISTEADY MPD ARCJETS; H. Tahara, K. Mitsuo, L. Zhang, T. Yasui, Y. Kagaya, and T. Yoshikawa, Osaka Univ., Japan

1995-179: A 5, 730-HR CYCLIC ENDURANCE TEST OF THE SPT-100; C. E. Garner, J. R. Brophy, J. E. Polk, and L. C. Pless, JPL, USA; Dan A. Starling, Navai Postgraduate School, USA

1995-180: LARGE RADIO-FREQUENCE ION BEAM SOURCES PRIS 10, RIM 20, RIM 25, RIM 35, AND RIM 12x50 FOR SURFACE TREATMENT; J. Freisinger, A. Kux, and H. W. Loeb, Giessen University, Germany

1995-181: LOW FLOW RATE IMPULSIVE PLASMA ACCELERATOR, ACDE-TYPE FOR TECHNOLOGY PURPOSES; A. N. Veselovzorov and A. A. Pogorelov, RSC “Kurchatov Institute”, Russia

1995-182: MPD-THRUSTER FOR TECHNOLOGY APPLICATIONS; Yu. A. Alexsev and M. N. Kazeev, RSC “Kurchatov Institute”, Russia

1995-185: SOURCE OF INTENSIVE OXYGEN PLASMA FLOWS OF LOW ENERGY FOR TECHNOLOGICAL APPLICATIONS; L. N. Devashova, V. V. Yegorov, B. A. Mednikov, and V. K. Shinin, RIAME MAI, Russia

1995-186: THE DEVELOPMENT OF PLASMA ACCELERATOR WITH INTENSE DIVERGENCE AND HIGH UNIFORMITY OF ION FLOW FOR TECHNOLOGICAL APPLICATIONS; L. N. Devashova, V. V. Yegorov, B. A. Mednikov, and V. K. Shinin, RIAME MAI, Russia

1995-188: IGNITION SYSTEM FOR AUTOMOBILE MOTOR WITH PULSED ACCELERATOR; I. N. Statsenko, V. N. Statsenko, Yu. N. Statsenko, V. I. Zaitsev, and A. A. Krylov, Dnepropetr. State Univ., Ukraine; V. V. Rybakov, MAI, Russia; B. N. Pyatko, Meltopol Motor-Building Plant, Ukraine

1995-189: PLASMA SOURCE USAGE IN VACUUM TECHNOLOGY; B. A. Arkhipov, N. A. Maslennikov, and A. N. Nesterenko, EDB “Fakel”, Russia; V. Kim, RIAME MAI, Russia

1995-190: PLASMA DIAGNOSTICS INSIDE A MICROWAVE DISCHARGE ION THRUSTER USING TUNABLE LASER DIODES; K. Nishiyama, S. Satori, H. Kuniinaka, and K. Kuriki, Inst. of Space and Astronat. Science, Japan; Th. Wegmnn, Stuttgart Univ. Germany

1995-191: NON-STATIONARY ELECTRIC PROBE FOR PLASMA DIAGNOSTIC OF ELECTRIC PROPULSION ENGINES; M. V. Koteinikov, MAI, Russia

1995-192: OPTICAL SPECTROSCOPY ANALYSIS OF A STATIONARY PLASMA THRUSTER; J. Bonnet, P. Leray, and D. Pigache, ONERA, France; J. Bretagne and A. Ricard, Universite Paris, France; M. Lyszyk, SEP, France

1995-194: MULTYPARAMETRIC ANALYZE OF THE EXPERIMENTAL DATA OBTAINED DURING ELECTRIC PROPULSION SYSTEMS TESTING; S. A. Andrianov, S. A. Khartov, and L. A. Latyshev, MAI, Russia; A. V. Malygin, K. A. Pavlov, Centr. Sci. Inst. of Space Forces of Russia

1995-195: LASER INTERFEROMETRY FOR PULSED PLASMA THRUSTER PERFORMANCE MEASUREMENT; E. A. Cubbin, J. K. Ziemer, E. Y. Choueiri, and R. G. Jahn, Princeton University, USA

1995-196: ANALYSIS OF ANODE LAYER THRUSTER GUARD RING EROSION; C. Marrese, L. B. King, and A. C. Galimore, Univ. of Michigan, USA; J. E. Polk and C. E. Garner, JPL, USA; A. Semenkin, V. Garkusha, and S. Tverdoklebov, TsNIIMASH, Russia

1995-197: A WAVEGUIDE IR LASER FOR NEUTRALS AND ION BEAMS DIAGNOSTICS; B. A. Kuzyakov, Inst. of High Temper., Russia

1995-198: REACTIVE PLASMA ACCELERATOR JET POTENTIAL MEASUREMENT BY EMISSIVE PROBE WITH PLASMA ELECTRON HEATING; V. N. Chernik, Inst. of Nuclear Phys., Moscow State Univ., Russia

1995-199: NEUTRALIZER/PLASMA CONTACTOR TECHNOLOGIES: REVIEW OF DEVELOPMENT ACTIVITIES AT PROEL TECHNOLOGIE; A. Severi, G. Matticari, A. Matucci, and M. Municci, PROEL TECHN., Italy; G. Saccoccia, ESTEC-YPE, The Netherlands; F. Svelto, Italian Space Agency, Italy

1995-200: AMPULE CATHODE-NEUTRALIZER; A. V. Khitko, N. V. Maslyany, and V. F. Pridantzev, Dnepropetr, State Univ., Ukraine

1995-201: APPLICATION OF HOLLOW CATHODE IN ARCJET PROPULSION AT LOW AND AVERAGE POWER; E. P. Vaulin, L. V. Feoktistov, and N. V. Petukhov, MAI, Russia; V. A. Obukhov, RIAME MAI, Russia; F. Scortecci, CENTROSPAZIO, Italy

1995-202: HIGH FREQUENCY OSCILLATIONS IN THE HOLLOW CATHODE AND THEIR INFLUENCE ON ITS OPERATION; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, V. I. Vasin, and Yu. M. Yashnov, NIITP, Russia

1995-203: ENERGY SPECTRUM OF ELECTRONS IN A NEAR-CATHODE LAYER; B. B. Rodnevich, NIITP, Russia

1995-204: MONITORING OF ELECTRIC THRUSTER CATHODE-NEUTRALIZER EROSION USING SPECTRAL AND PROBE MEASUREMENTS IN PLASMA; V. I. Baranov, A. I. Vasin, V. A. Petrosov, NIITP, Russia; E. I. Asinovsky, V. V. Markovets, V. P. Polishchuk, I. M. Yartsev, and Yu. V. Vizilter, Inst. High. Temper., Russia

1995-205: THE HIGH EMISSION SELFHEATED ARC DISCHARGE HOLLOW CATHODES; A. I. Oransky, Kharkov Aviation Inst., Ukraine

1995-206: NUMERICAL AND EXPERIMENTAL INVESTIGATIONS OF THEMPERATURE FIELDS AND HEAT FLUXES IN ELECTRIC THRUSTERS; A. F. Anikin, S. M. Bednov, V. I. Baranov, and A. N. Golikov, NIITP, Russia

1995-207: THE MODIFIED BALANCE METHOD OF NEAR-CATHODE PROCESSES CALCULATION CHARACTERISTICS; Y. V. Bruevich, I. P. Nazarenko, and I. G. Panevin, MAI, Russia

1995-208: THE METHOD OF EXPRESS ESTIMATION OF GAS HOLLOW CATHODE EROSION RATE AND RESULTS OF IT APPROBATION; Ye. A. Isayev and A. I. Oransky, Kharkov Aviation Inst., Ukraine

1995-209: THE PECULARITIES OF HOLLOW CATHODES EROSION AT NON-INCANDESCENT SWITCHING ON; N. N. Koshelev, A. V. Loyan, and A. I. Oransky, Kharkov Aviation Institute., Ukraine

1995-210: THE MODEL AND CALCULATION OF HOLLOW CATHODE EROSION; A. S. Dolgov, A. V. Zaharchenko, S. Yu. Nesterenko, and A. I. Oransky, Kharkov Aviation Inst., Ukraine

1995-211: INFLUENCE OF MASS FLOW RATE OF ACTIVATOR ON WORK OF GAS HOLLOW CATHODE; A. V. Khitko, Dnepropetr. State Univ., Ukraine

1995-212: NOVEL ORBIT RAISING STRATEGY MAKES LOW THRUST COMMERCIALLY VIABLE; A. Spitzer, Hughes Aircraft Company, USA

1995-213: ESTIMATE OF THE OPTIMAL MERCURY-RENDEZVOUS LOW-THRUST TRAJECTORY WITH VENUS SWINGBY; M. S. Konstantinov, MAI, Russia

1995-214: ASSOCIATED OPTIMIZATION OF THE LOW-THRUST TRAJECTORY AND PARAMETERS OF THE NUCLEAR POWER PLANT; P. V. Andreev, A. Y. Galkin, G. M. Gryaznov, G. A. Zaritsky, and E. E. Zhabotinsky, “Krasnaya zvezda”,Russia; G. G. Fedotov, M. S. Konstantinov, and V. G. Petukhov, MAI, Russia

1995-215: INTERPLANETARY TRAJECTORY OPTIMISATION CODES FOR ELECTRIC PROPULSION RESEARCH; M. Nakano, Y. Ishijma, and Y. Arakawa, Tokyo Univ., Japan

1995-217: THE PLUTO RENDEZVOUS MISSION WITH SOLAR-NUCLEAR ELECTRIC PROPULSION; R. Z. Akhmetshin, T. M. Eneev,  and G. B. Efimov, Inst. of Appl. Mathem., Russia

1995-220: APPLICATION OF THE POWER-LIMITED PROBLEM TO THE ELECTRIC PROPULSION MISSION DESIGN; G. G. Fedotov, M. S. Konstantinov, and V. G. Petukhov, MAI, Russia

1995-221: ONE NUMERICAL METHOD TO CALCULATE OPTIMAL POWER-LIMITED TRAJECTORIES; V. G. Petukhov, MAI, Russia

1995-222: OPTIMIZATION OF ORBITAL TRANSFERS AND INTERPLANETARY MISSIONS WITH ELECTRIC PROPULSION; Yu. A. Zakharov, MAI, Russia

1995-226: MATHEMATICAL SIMULATION OF ELECTROMAGNETIC PLASMA AND SOLID ARMATURES ACCELERATION IN RAILGUN BORE; M. P. Galanin, E. V. Mayakova, Yu. P. Popov, and S. Khramtsovsky, Inst. Applied Math., Russia; A. V. Plekhanov, “Soyuz”, Russia; V. V. Savitchev, Moscow State Techn. Univ., Russia

1995-228: THE ROLE OF ANALYSIS AND TESTING IN THE SERVICE LIFE ASSESSMENT OF ION ENGINES; J. E. Polk, N. R. Moore, J. R. Brophy, and D. H. Ebbeler, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1995-229: PLASMA SOURCE USAGE IN VACUUM TECHNOLOGY; B. A. Arkhipov, N. A. Maslennikov, and A. N. Nesterenko, EDB “Fakel”, Russia; V. Kim, RIAME MAI, Russia

1995-230: THE DEVELOPMENT INVESTIGATION OF THE CATHODE-COMPENSATOR OF STATIONARY PLASMA THRUSTERS FOR DISCHARGE CURRENTS OF TO 50 A; B. A. Arkhipov, S. S. Kudriavtsev, N. A. Maslennikov, V. M. Murashko, and I. A. Turgeneva, EDB “Fakel”, Russia

1995-231: ELECTRIC PROPULSION SYSTEM FOR SPACECRAFT ACCELERATION AND MANOUEVRING DURING FLIGHT TO ASTEROIDS; B. A. Arkhipov, A. S. Bober, N. A. Maslennikov, EDB “Fakel”, Russia; G. A. Popov, RIAME MAI, Russia

1995-232: FACILITY FOR TESTING ELECTRIC THRUSTERS AND PROPULSION SYSTEMS; A. S. Bober, N. A. Maslennikov, V. A. Ivanov, EDB “Fakel”, Russia

1995-234: THE ROLE OF SPOT MODE TRANSITION IN THE ANODE FALL OF PULSED MPD THRUSTERS; K. D. Diamant, E. y. Choueiri, and R. G. Jahn, Princeton Univ., USA

1995-235: ELECTRIC PROPULSION SYSTEM ON THE SPACEBUS SPACECRAFT FAMILY; M. Perdu, P. Borie, and T. Grassin, Aerospatiale, France

1995-236: A STUDEY OF ALKALI-SEEDED HYDROGEN ARCJET PERFORMANCE; F. Oyerokun, M. Martinez-Sanchez, Massach. Inst. Tech., USA

1995-237: DEVELOPMENT OF A 500 WATT CLASS ARCJET THRUSTER SYSTEM; P. G. Lichon, G. H. McLean, and C. E. Vaughan, OLIN Aerospace Comp., USA; J. M. Sankovic, NASA LeRC, USA

1995-239: ELECTRIC PROPULSION FOR AN INTERPLANETARY ASTROPHYSICS MISSION; B. T. Patel, M. Martinez-Sanchez, and G. R. Ricker, Massach. Inst. of Technology, USA; D. Tilley and D. Barnhart, Phillips Lab., USA; H. Alexander, Orbital Sci. Corp. USA; R. Myers, E. Pencil, G. Horvart, and J. Samella, NASA Lewis RC, USA

1995-240: TWO-DIMENSIONAL HYBRID PARTICLE-IN-CELL (PIC) MODELING OF HALL THRUSTERS; J. M. Fife and M. Martinez-Sanchez, Massach. Inst. of Tech., USA

1995-241: THE EFFECT OF POWER SUPPLY OUTPUT CHARACTERISTICS ON THE OPERATION OF THE SPT-100 THRUSTER; J. A. Hamley and J. M. Sancovic, NASA Lewis RC, USA; A. N. Petrenko, Dnepropetr. State Univ., Ukraine; D. H. Manzella, NYMA Inc., USA; K. C. Cartier, ANALEX Inc., USA

1995-242: PRELIMINARY INVESTIGATION OF THE ORIGINAL 1 KW ARCJET MODEL; V. D. Gratchev, A. G. Klimenko, S. V. Pavlov, and G. Ya. Saveliev, NIITP, Russia

1995-244: THE USA AIR FORCE ELECTRIC PROPULSION PROGRAM; R. A. Spores, Phill. Lab., USA; M. Birkan, AFOSR/NA, USA; R. Cohen, Aerospace Corp., USA; R. Einhorm, US Air Force, USA

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IEPC1995-Index

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notes.txt  19:35   28   

1997 INDEX

1997-001: THE USAF ELECTRIC PROPULSION PROGRAM; Ronald A. Spores, Phillips Laboratory/RKES, Edwards AFB, CA 93524; Ronald B. Cohen, Aerospace Corporation, El Segundo, CA 90009; and Mitat Birkan, AFOSR/NA, Bolling AFB, Washington, DC 20332

1997-002: ELECTRIC PROPULSION IN EUROPE: DEVELOPMENT AND APPLICATIONS; Giorgio Saccoccia, Head of Electric Propulsion Unit, ESA Technical and Operational Support Directorate, ESTEC, Keplerlaan 1, 2200 AG, Noordwijk, The Netherlands

1997-003: NASA’S ELECTRIC PROPULSION PROGRAM; Francis M. Curran and Timothy E. Tyburski, National Aeronautics and Space Administration, Lewis Research Center, 21000 Brookpark Road, Mail Stop 301-3, Cleveland, Ohio, USA, 44135

1997-004: DEVELOPMENT AND APPLICATION OF ELECTRIC THRUSTERS AT EDB “FAKEL”; B. A. Arhipov, V. N. Vinogradov, K. N. Kozubsky, S. S. Kudriavtsev, N. A. Maslennikov, and V. M. Murashko, Experimental Design Bureau “Fakel”, Kaliningrad, Russia

1997-005: AN OVERVIEW OF ELECTRIC PROPULSION ACTIVITIES IN JAPAN; K. Toki, Associate Professor, Institute of Space and Astronautical Science, Sagamihara, Kanagawa, Japan; A. Sasoh, Associate Professor, Institute of Fluid Science, Tohoku University, Sendai, Miyagai, Japan

1997-006: AN OVERVIEW OF ELECTRIC POWER: A KEY TECHNOLOGY FOR ELECTRIC PROPULSION; Gary L. Bennett, Metaspace Enterprises; 5000 Butte Road, Emmett, Idaho 83617-9500, USA; Henry W. Brandhorst, Jr., Space Power Institute, 231 Leach Center, Auburn University, Alabama 36849-5320; C. P. Bankston, Jet Propulsion Laboratory, 4800 Oak Grove Drive, Pasadena, California 91109-8099, USA; and R. J. Sovie, Lewis Research Center, 21000 Brookpark Road, Cleveland, Ohio 44135-3191, USA

1997-007: 100 kW CLASS HYDROGEN ARCJET THRUSTER; Monika Auweter-Kurtz, Thomas Gölz, Harald Habiger, Frank Hammer, Helmut Kurtz, Martin Riehle, and Christian Sleziona; Institut für Raumfahrtsysteme, Universität Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Federal Republic of Germany

1997-008: 1 kW HYDRAZINE ARCJET SYSTEM DEVELOPMENT; Martin Riehle, Helmut L. Kurtz, and Monika Auweter-Kurtz; Institut für Raumfahrtsysteme, Universität Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Germany; and York E. Viertel, Daimler-Benz Aerospace AG, Space Infrastructure Division, Hünefeldstrabe 105, D-28361, Bremen, Germany

1997-010: TESTING OF A 1.8 kW, FLIGHT QUALIFIED HYDRAZINE ARCJET SYSTEM; Gaetano De Lorenzo and William D. Deininger, FiatAvio – Comprensorio BPD, 00034, Colleferro (Rm), Italy; Richard D. Smith, PRIMEX Aerospace Company, Redmond, WA 98076-9709, USA

1997-011: NUMERICAL SIMULATION OF A LOW POWER ARCJET THRUSTER; Andrea Santovincenzo, William D. Deininger, and Gaetano De Lorenzo, FiatAvio – Comprensorio BPD, 00034, Colleferro (Rm), Italy; Vito Salvatore and Annamaria Russo Sorge, DISIS – Dipartimento di Scienza ed Ingegneria dello Spazio, Universita degli Studi “Federico II”, Napoli, Italy

1997-012: STABILITY OF ALKALI-SEEDED HYDROGEN ARCJETS; Folusho Oyerokun, Darrel Robertson, and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, Massachusetts

1997-013: MEASUREMENTS OF ANODE HEAT TRANSFER IN A 1 KW ARCJET; Nicholas T. Tiliakos, Rodney L. Burton, and Herman Krier, University of Illinois at Urbana-Champaign, Urbana, IL 61801

1997-014: METHANE ARCJET DEVELOPMENT; V. Hruby and J. Kolencik, Busek Co. Inc., Natick, MA 01760-1023; M. Martinez-Sanchez, MIT, Cambridge, MA 02139; D. Dvore, Consultant, Rowe, MA 01367; K. D. Annen and R. C. Brown, Aerodyne Research, Inc., Billerica, MA 01821-3976

1997-015: DEVELOPMENT OF AN EFFICIENT THREE-DIMENSIONAL OPTICS CODE; M. Nakano and Y. Arakawa, The University of Tokyo, Hongo 7-3-1, Bunkyo-ku, 113 Japan

1997-016: THE DEVELOPMENT OF THE ESA-XX ION THRUSTER; Helmut Bassner, Space Infrastructure, Diamler-Benz Aerospace AG, Postfach 80 11 69, D-81663 München, Germany; Robert Bond and Vaughan Thompson, AEA Technology plc, Culham Science and Technology Centre, Abingdon, Oxon OX14 3 DB, United Kingdom; and Klaus Groh, University of GieBen, Heinrich-Buff-Ring 16, D. 35392 GieBen, Germany

1997-017: MAPPING THE MAGNETIC FIELD OF THE DERA T5 KAUFMAN-TYPE ION THRUSTER; S. N. Moore, Space Dept. Defence Evaluation & Research Agency, Farnborough, Hampshire, GU14 0LX, United Kingdom

1997-018: COMMERCIALIZED ION PROPULSION FOR NORTH/SOUTH STATIONKEEPING OF COMMUNICATION SATELLITE; H. Bassner and K. Bohnhoff, Diamler-Benz Aerospace AG, Munich, Germany; A. Trivulzio, FIAR S.p.A., Space Division, Milano, Italy

1997-019: PROFILING THE BEAM OF THE T5 ION ENGINE; James E. Pollard, The Aerospace Corporation, P. O. Box 92957, M5-754, Los Angeles, CA 90009

1997-020: MONTE CARLO SIMULATION OF NEUTRAL XENON FLOWS OF ELECTRIC PROPULSION DEVICES; Iain D. Boyd, Douglas B. VanGilder, and Xiaoming Liu, Cornell University, Ithaca, NY 14853

1997-021: ELECTRON TRANSPORT MECHANISM IN A HALL THRUSTER; Miharu Hirakawa, Tokai University, Hiratsuka-shi, Kanagawa, Japan

1997-022: SCALING LAWS FOR HALL THRUSTER PERFORMANCE; A. Fruchtman, Center for Technological Education Holon, 52 Golomb St., P.O. Box 305, Holon 58102, Israel; N. J. Fisch, Princeton Plasma Physics Laboratory, Princeton University, P.O. Box 451, Princeton, NJ 08543, USA; J. Ashkenazy and Y. Raitses, Propulsion Physics Laboratory, Soreq NRC, Yavne 81800, Israel

1997-023: HIGH-VOLTAGE MODE OF THE TAL THRUSTER OPERATION; S. O. Tverdokhlebov and V. I. Garkusha, Central Research Institute of Machine Building, 14170, Korolev, Moscow Region, Russia

1997-024: SOME RESULTS OF THE SPT JET CHARACTERISTICS COMPARISON; Mikhail V. Zikeyev, Moscow State Aviation Institute, Department “Spacecraft Electric Propulsion and Powerplants”, Volokolamskoe shosse, d. 4, Moscow, 12571, Russia

1997-025: CALCULATION OF CHARACTERISTICS OF THE ELECTRIC PROPULSION PLUME INTRINSIC RADIATION; A. P. Plokhikh and G. G. Shishkin, Research Institute of Applied Mechanics and Electrodynamcis of Moscow Aviation Institute, Moscow, Russia

1997-026: EFFECT OF THE PLASMA POTENTIAL OSCILLATIONS AT A THRUSTER OPERATION; A. V. Zharinov, State Researche of Energy Institute, Moscow, Russia; and V. I. Garkusha, Central Researce Institute of Machine Building, Moscow reg., Russia

1997-027: THE I.S.P. SOFTWARE: CALCULATION OF THE SPT JET INFLUENCE; D. Borie, Aérospatiale, Cannes, V. Perrin, Principia, S. Khartov, and A. Nadiradze, MAI Institute, Russia

1997-028: GEOMAGNETIC FIELD PERTURBATION BY A PLASMA PLUME; A. G. Korsun and E. M. Tverdokhlebova, Central Research Institute of Machine Building (TsNIIMASH), Korolev, Moscow region, Russia

1997-031: OPERATIONAL CHARACTERISTICS OF MICROWAVE DISCHARGE NEUTRALIZER; Shin Satori and Hitoshi Kuninaka, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara, Kanagawa, Japan; Motoyuki Ohtaki and Yoshio Ishikawa, Nippon University, 7-24-1, Narashino dai, Funabashi, Chiba, Japan

1009-033: DESIGN AND DEVELOPMENT OF AN ELECTRONIC PRESSURE REGULATOR FOR USE ON ION PROPULSION SYSTEMS; Dr. H. L. Gray, Matra Marconi Space UK, Ltd., Anchorage Road, Portsmouth, Hampshire PO3 5PU, England

1997-035: IEPC 97-035 ELECTROMAGNETIC ACCELRATION IN PLUSED PLASMA THRUSTERS; D. Keefer and R. Rhodes, University of Tennessee Space Institute, Tullahoma, Tennessee 37388

1997-036: NUMERICAL INVESTIGATION OF PULSED PLASMA THRUSTER PLUMES; Xuemin Yin and Nikos A. Gatsonis, Computational Gas & Plasma Dynamics Laboratory, Mechanical Engineering Department, Worcester Polytechnic Institute, Worcester, MA 01609

1997-037: THEORETICAL STUDIES OF A PULSED PLASMA MICROTHRUSTER; P. G. Mikelldes, P. J. Turchi, R. Leiweke, C. S. Schmahl, and I. G. Mikellides

1997-038: DIRECTIONS FOR IMPROVING PPT PERFORMANCE; P. J. Turchi, The Ohio State University, Columbus, Ohio USA

1997-041: THEORECTICAL AND COMPUTATIONAL ANALYSIS OF PULSED PLASMA THRUSTER PLUMES; Nikos A. Gatsonis and Xuemin Yin, Computational Gas & Plasma Dynamics Laboratory, Mechanical Engineering Department, Worcester Polytechnic Institute, Worcester, MA 01609

1997-042: ELECTRICAL POTENTIALS IN THE NSTAR CHARGE EXCHANGE PLUME; Ira Katz and V. A. Davis, Maxwell Technologies Federal Division, 8888 Balboa Ave., San Diego, CA 92123; Joseph Wang and David Brinza, Jet Propulsion Laboratory, 4800 Oak Grove, Pasadena, CA 91109

1997-043: PREDICTIONS OF NSTAR CHARGE EXCHANGE IONS AND CONTAMINATION BACKFLOW; V. A. Davis, Barbara Gardner, and Ira Katz, Maxwell Technologies Federal Division, Inc. 8888 Balboa Ave., San Diego, CA 92123-1506; David Brinza, Jet Propulsion Laboratory, MS 125-177, 4800 Oak Grove Drive, Pasadena, CA 91109

1997-044: NSTAR ION ENGINE XENON FEED SYSTEM: INTRODUCTION TO SYSTEM DESIGN AND DEVELOPMENT; Edward D. Bushway III, Moog, Inc., East Aurora, NY; Carl S. Engelbrecht and Dr. Gani B. Ganapath, Jet Propulsion Laboratory, Pasadena, CA

1997-047: IN SITU, TIME-RESOLVED ACCELERATOR GRID EROSION MEASUREMENTS IN THE NSTAR 8000 HOUR ION ENGINE WEAR TEST; J. E. Polk, J. R. Anderson, J. R. Brophy, V. K. Rawlin, M. J. Patterson and J. Sovey

1997-049: SERVICE LIFE ASSESSMENT FOR ION ENGINES; John R. Anderson, James E. Polk, and John R. Brophy, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA

1997-051: THERMAL ENVIRONMENTAL TESTING OF NSTAR ENGINEERING MODEL ION THRUSTERS; Vincent K. Rawlin and Michael J. Patterson, NASA Lewis Research Center, Cleveland, OH; and Raymond A. Becker, Jet Propulsion Laboratory, Pasadena, CA

1997-052: DEVELOPMENT OF A STATIONARY PLASMA THRUSTER MATHEMATICAL MODEL ON THE BASE OF EXPERIMENTAL DATA; Olexandre N. Petrenko and Olexandre N. Yatcina; Dnepropetrovsk State University, Institute of Physics and Technology, Naukovy Line, 13, 320625 Dnepropetrovsk-10, Ukraine

1997-053: CHARACTERIZATION OF PLASMA INSIDE THE SPT-50 CHANNEL BY ELECTROSTATIC PROBES; G. Guerrini, C. Michaut, and M. Bacal, Laboratoire de Physique des Milieux Ionisés, Laboratoire du C.N.R.S., Ecole Polytechnique, 91128 Palaiseau Cedex, France; M. Dudeck, Laboratoire d’Aéothermique, Meudon and Université Paris 6, France; and A. N. Vesselovzorov, RCC Kurchatov Institute, Moscow, Russia

1997-054: SPATIALLY RESOLVED EMISSION SPECTROSCOPY ALONG A SPT CHANNEL INTERPRETATION OF DATA BY A COLLISIONAL-RADIATIVE MODEL; Philippe Leray, Jean Bonnet, and Daniel Pigache, ONERA (Office National d’Etudes et de Recherche Aérospatiale), BP n72 92322 Chátillon cedex, France; Tiberiu Minea, Jean Bretagne, and Michael Touzeau, Laboratoire de Physique des Gaz et des Plasmas, U. A. CNRS, Bat. 212, Université Paris-Sub, 91405 ORSAY Cedex, France

1997-055: EXTERNAL ANODE LAYER THRUSTER PARAMETERS AT A HIGH SPECIFIC IMPULSE REGIMES; A. Semenkin, Central Research Institute of Machine Building, Korolev, Russia

1997-056: EXPERIMENTAL INVESTIGATION OF THE EFFECT OF CHANNEL MATERIAL ON HALL THRUSTER CHARACTERISTICS; Y. Raitses, J. Ashkenazy, and G. Appelbaum, Propulsion Physics Laboratory, Soreq, Yavne 81800, Israel; and M. Guelman, Faculty of Aerospace Engineering, Technion, IIT, Haifa

1997-058: A STUDY OF A LOW POWER HALL THRUSTER TRANSIENT BEHAVIOR; W. A. Hargus, Jr., N. B. Meezan, and M. A. Cappelli, Mechanical Engineering Department, Thermosciences Division, Stanford University, Stanford, CA 94305

1997-059: PERFORMANCE EVALUATION OF THE SPT-140; David Manzella, NYMA, Inc., Engineering Services Division, Brook Park, Ohio 44142; Charles Sarmiento, John Sankovic, and Tom Haag, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135

1997-060: ENERGY BALANCE AND ROLE OF WALLS IN ACDE; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, A. I. Vasin, and Yu. M. Yashnov, Keldysh Research Center, Moscow, Russia

1997-061: PLASMA DIAGNOSTICS INSIDE A MICROWAVE DISCHARGE ION THRUSTER; K. Nishiyama, The University of Tokyo, Japan; S. Satori, H. Kuninaka, and K. Kuriki, Institute of Space and Astronautical Science, Japan; and Y. Arakawa, The University of Tokyo, Japan

1997-063: NONEQUILIBRIUM HYDROGEN/NITROGEN PLASMAS STUDIES USING A CASCADE ARC; Trevor Moeller, Dennis Keefer, and Robert Rhodes, University of Tennessee Space Institute, B. H. Goethert Parkway, Tullahoma, TN 37388

1997-064: PLUME DIAGNOSTICS OF AN APPLIED FIELD ACRJET BY USING A DIODE-LASER ABSORPTION TECHNIQUE; Kimiya Komurasaki, Teruhito Iida, Daisuke  Kusamoto, Feng Yuan Zhang, Department of Aerospace Engineering, Nagoya University, Furo-cho, Chikusa, Nagoya 464-01, Japan; and Shin Satori, The Institute of Space and Astronautical Science, Yoshinodai, Sagamihara 229, Japan

1997-065: FLAT ORIENTED PROBE IN THE RAREFIELD PLASMA FLOW; Vladimir Kim, Research Institute of Applied Mechanics and Electrodynamics of Moscow State Aviation Institute (RIAME MAI), Moscow, Russia; Vadim A. Kotelnikov and Michael V. Kotelnikov, Moscow State Aviation Institute – Technical University (MAI), Moscow, Russia

1997-066: DEVELOPMENT OF A SINGLE-ORIFICE RETARDING POTENTIAL ANALYZER FOR HALL THRUSTER PLUME CHARACTERIZATION; Colleen M. Marrese, Neha Majumdar, James M. Haas, George Williams, Lyon B. King and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory (PEPL) Dept. of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan

1997-067: OPTICAL DIAGNOSIS OF PLASMA IN A CHANNEL OF HALL THRUSTERS; Daisuke Kusamoto and Kimiya Komurasaki, Department of Aerospace Engineering, Nagoya University, Chikusa, Nagoya 464-01, Japan

1997-068: A REVIEW OF LOW ENERGY SPUTTERING THEORY AND EXPERIMENTS; Olivier B. Duchemin, California Institute of Technology, Pasadena, CA 91125; John R. Brophy and Charles E. Garner, Jet Propulsion Laboratory, Pasadena, CA 91109; Pradosh K. Ray and V. Shutthanandan, Tuskegee University, Tuskegee, AL 36088; and Maris A. Mantenieks, Lewis Research Center, Cleveland, OH 44135

1997-069: ON THE MEASUREMENT OF LOW-ENERGY SPUTTERING YIELD USING RUTHERFORD BACKSCATTERING SPECTROMETRY; V. Shutthanandan and Pradosh K. Ray, College of Engineering, Architecture and Physical Sciences, Tuskegee University, Tuskegee, AL 36088; N. R. Shivaparan and Richard J. Smith, Physics Department, Montana State University, Bozeman, MT 59717; S. Thevuthasan, Environmental Molecular Sciences Laboratory, Pacific Northwest National Laboratory, Richland, WA 99352; and Maris A. Mantenieks, NASA-Lewis Research Center, Cleveland, OH 44135

1997-070: BATCH-FABRICATED RESITOJETS: INITIAL RESULTS; Siegfried W. Janson, Technology Operations, Mechanics and Materials Technology Center, The Aerospace Corporation, Los Angeles, California

1997-071: MICRO-FABRICATED ACCELERATOR GRID SYSTEM FEASILITY ASSESSMENT FOR MICRO-ION ENGINES; Juergen Mueller, William C. Tang, Wen Li, and Andrew P. Wallace, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

1997-072: DESIGN CONSIDERATIONS FOR ION MICROTHRUSTERS; G. J. Yashko, G. B. Giffin, and D. E. Hastings, Massachusetts Institute of Technology, Cambridge, Massachusetts

1997-073: CHANNEL ION SOURCE; Graeme Aston and Martha B. Aston, Electric Propulsion Laboratory, Inc., Monument, CO 80132

1997-074: FULLERENE ION THRUSTER DEVELOPMENT; V. Hruby, J. Monheiser, and J. Kolencik

1997-075: AN INVESTIGATION OF FULLERENE PROPELLANT FOR RF ION THRUSTERS; J. Steven Snyder and Paul J. Wilbur, Colorado State University, Fort Collins, CO 80523; John R. Anderson, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

1997-076: C60 APPLICATION TO ION THRUSTER – INSPECTION OF IONIZED AND EXTRACTED PARTICLE; Yoshinori Nakayama and Haruki Takegahara, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, Asahigaoka 6-6, Hino, Tokyo 191, Japan

1997-077: PRELIMINARY EXPERIMENTAL EVALUATION OF A MINIATURIZED HALL THRUSTER; Vadim Khayms and M. Martinez-Sanchez, Space Systems Laboratory, MIT Department of Aeronautics and Astronautics

1997-078: THE LOW POWER HELIUM PULSED ARCJET; Gary F. Willmes and Rodney L. Burton, Department of Aeronautical and Astronautical Engineering, University of Illinois at Urbana-Champaign, Urbana, IL 61801

1997-079: NEW GENERATION OF ELECTRIC THRUSTERS; Vladimir Grigorian, Konstantin Evdokimov, Avil Izmailov, Sergey Khartov, Leonid Latyshev, and Alexander Shtyrlin, Moscow State Aviation Institute (MAI), Department “Spacecraft Electric Propulsion and Powerplants”, Volokolamskoe shosse, d.4, Moscow, 125871, Russia

1997-081: FLIGHT QUALIFICATION OF THE 1.8 KW MR-509 HYDRAZINE ARCJET SYSTEM; R. D. Smith, C. R. Roberts, and R. S. Aadland, PRIMEX Aerospace Company, Redmond, WA, USA; D. A. Lichtin and K. Davies, Lockheed Martin Corporation

1997-082: FLIGHT QUALIFICATION OF THE 2.2 KW MR-510 HYDRAZINE ARCJET SYSTEM; R. D. Smith, R. S. Aadland, and C. R. Roberts, PRIMEZ Aerospace Company, Redmond, WA, USA; D. A. Lichtin, Lockheed Martin Corporation

1997-084: NUMERICAL SIMULATION OF A NONEDQUILIBRIUM PLASMA FLOW IN A NITROGEN ARCJET THRUSTER USING A THREE-TEMPERATURE KINETIC MODEL; Shigeru Kuchi-ishi and Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-81, Japan

1997-085: GRAPHITE NOZZLE PERFORMANCE INVESTIGATIONS WITH HIGH POWER ARCJETS; Martin Riehle, Helmut L. Kurtz, Frank Hammer and Monika Auweter-Kurtz, Institut für Raumfahrtsysteme, Universität Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Germany

1997-087: SPECTROSCOPIC MEASUREMENT AND NUMERICAL ANALYSIS OF MEDIUM-POWER HYDROGEN/NITROGEN-MIXTURE ARCJET FLOWFIELDS; H. Tahara, T. Yonezawa, Y. Andoh, K. Onoe and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Toyonaka, Osaka, Japan

1997-088: 500-WATT ARCJET SYSTEM DEVELOPMENT AND DEMONSTRATION; Paul G. Lichon, Dennis L. Tilley, and Ron Anderson, PRIMEX Aerospace Company, Redmond, WA 98073; John M. Sankovic, NASA-Lewis Research Center, Cleveland, OH 44135

1997-089: LOW-POWER MICROWAVE ARCJET PERFORMANCE TESTING; D. Nordling and M. M. Micci, Department of Aerospace Engineering and Propulsion Engineering Research Center, The Pennsylvania State University, University Park, PA, USA

1997-090: INTEGRATED DESIGN ARCJETS FOR HIGH PERFORMANCE; G. Aston and M. B. Aston, Electric Propulsion Laboratory, Inc., Monument, CO 80132

1997-091: CENTRALIZED PULSED PLENUM GAS DELIVERY SYSTEM FOR HYDRAZINE ARCJETS; Mary M. Kriebel, Christopher H. McLean, and Ian F. Murray, TRW, Space and Technology Division, Redondo Beach, CA

1997-092: EFFECTS OF PROPELLANT FEED AND MAGNETIC FIELD ON ION THRUSTER PERFORMANCE; Haruki Takegahara, Yasushi Okawa, Takeru Ikeda, and Jun Takahashi, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, Asahigaoka 6-6, Hino, Yokyo 181, Japan

1997-093: FABRICATION OF CARBON-CARBON COMPOSITE ION THRUSTER GRIDS – IMPROVEMENT OF STRUCTURAL STRENGTH; S. Kitamura and Y. Hayakawa, National Aerospace Laboratory, Chofu, Tokyo, Japan; Y. Kasai and T. Ozaki, Mitsubishi Electric Corporation, Kamakura, Kanagawa, Japan

1997-095: FACTORS AFFECTING THE BEAM DIVERGENCE OF A T5 ION ENGINE; David H. Mundy, Space Department, Defence Evaluation and Research Agency, Farnborough, Hampshire, GU14 0LX, UK

1997-096: T5 ION ENGINE PLUME ANALYSIS USING A TIME OF FLIGHT MASS SPECTROMETER; David H. Munday, Space Department, Defence Evaluation and Research Agency, Farnborough, Hampshire, GU14 0LX, UK

1997-098: SCALING OF ION THRUSTERS TO LOW POWER; Michael J. Patterson and Stanley P. Grisnik, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio; George C. Soulas, NYMA, Inc., NASA Lewis Research Center Group, Brook Park, Ohio

1997-099: DEVELOPMENT OF POWER ELECTRONICS FOR A 0.2KW-CLASS ION THRUSTER; Luis R. Piñero and Michael J. Patterson, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio; Glen E. Bowers, Gilcrest Electric, Brook Park, Ohio

1997-100: ELECTRIC PROPULSION DEMONSTARTION MODULE (EPDM) FLIGHT HALL THRUSTER SYSTEM; Peter R. Lynn Jr. and Michael F. Osborn II, Naval Research Laboratory, Washington, D.C.; John M. Sankovic, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio; and Leonard H. Caveny, Ballistic Missile Defence Organization, Washington, D.C.

1997-102: RHETT2/EPDM DEVELOPMENT TESTING; John M. Sankovic, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio; David H. Manzella, NYMA Engineering Services Co., Lewis Research Center Group, Brook Park, Ohio; and Michael F. Osborn II, Naval Research Laboratory, Naval Center for Space Technology, Washington, D.C.

1997-103: RHETT/EPDM FLIGHT HOLLOW CATHODE; David Manzella, NYMA, Inc., Engineering Services Division, Brook Park, Ohio 44142; Michael Patterson, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135; and Michael Pastel, Gilcrest Electric and Supply Company, Brook Park, ,Ohio 44142

1997-104: RHETT/EPDM POWER PROCESSING UNIT; Peter T. Skelly and Robert J. Kay, PRIMEX Aerospace Company, Redmond, WA

1997-105: RHETT/EPDM FLIGHT XENON FLOW SYSTEM DEVELOPMENT; Michael F. Osborn II, Peter R. Lynn Jr., and Ronald L. Sutton, US Naval Research Laboratory (NRL), Washington, D.C. and Charles G. Sota, PRIMEX Aerospace Company, Redmond, WA

1997-106: RHETT/EPDM FLIGHT ANODE LAYER THRUSTER DEVELOPMENT; A. Semenkin, A. Kochergin, V. Garkusha, G. Chislov, and A. Rusakov, Central Research Institute of Machine Building (TsNIIMASH), Russia; S. Tverdokhlebov, TsNIIMASH-EXPORT; C. Sota, Teledesic Corporation, Seattle Wash.

1997-107: RHETT/EPDM PERFORMANCE CHARACTERIZATION; T. Haag, NASA Lewis Research Center and M. Osborn, Naval Research Laboratory

1997-108: RHETT2/EPDM HALL THRUSTER PROPULSION SYSTEM ELECTROMAGNETIC COMPATIBILITY EVALUATION; Charles J. Sarmiento and John M. Sankovic, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio; Joseph Freitas and Peter R. Lynn, Naval Research laboratory, Naval Center for Space Technology, Washington, D.C.

1997-109: RHETT2/RPDM MAGNETIC FIELD INTEGRATION IMPACTS; John M. Sankovic and Eric J. Pencil, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio; and David T. Jacobson, NYMA Engineering Services Co., Lewis Research Center Group, Brook Park, Ohio

1997-111: EXPERIMENTAL AND ANALYTICAL STUDY OF QUASI-STEADY MPD CHANNEL FLOW; K. Mitsuo, H. Tahara, H. Okutani, Y. Kagaya, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Toyonaka, Osaka, Japan

1997-112: NONEQUILIBRIUM FLOW ANALYSIS OF A TWO-DIMENSIONAL MPD ARCJET; I. Funaki, K. Toki, and K. Kuriki, Institute of Space and Astronautical Science, Kanagawa, Japan

1997-113: EXPERIMENTAL AND NUMERICAL INVESTIGATION OF STEADY STATE MPD THRUSTERS; Michael Winter, Christian Boie, Monkia Auweter-Kurtz, and Helmut L. Kurtz, Institut für Raumfahrtsysteme, Universität Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Germany

1997-115: APPLICATION OF ADAPTIVE NUMERICAL SCHEMES FOR MPD THRUSTER SIMULATION; C Boie, H. J. Kaeppeler, P. C. Sleziona and M. Auweter-Kurtz, Institut für Raumfahrtsysteme, Universität Stuttgart, Pfaffenwaldring 31, D-70569 Stuttgart, Germany

1997-116: THE INVESTIGATION OF APPLIED-FIELD MPD THRUSTERS ON THE INTERNATIONAL SPACE STATION; Monika Auweter-Kurtz, Gerd Krülle, and Helmut Kurtz, Institut für Raumfahrtsysteme, Universität Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Germany

1997-117: PERFORMANCE OF 130 KW MPD THRUSTER WITH AN EXTERNAL MAGNETIC FIELD AND LI AS A PROPELLANT; V. B. Tikhonov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute, Moscow, Russia; S. A. Semenikhin, Moscow Aviation Institute, Moscow, Russia; J. R. Brophy, and J. E. Polk, Jet Propulsion Laboratory, California Institute of Technology, USA

1997-118: PLASMA FEATURES NEAR QUASISTEADY MAGNETOPLASMADYNAMIC ARCJET CATHODES; H. Tahara, N. Yamasaki, K. Mitsuo, Y. Kagaya, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Toyonaka, Osaka, Japan

1997-119: TEMPERATURE EFFECTS ON CURRENT EMISSION IN AN ARTIFICIALLY HEATED MPD CATHODE; F. Paganucci, P. Rossetti, and M. Andrenucci, Centrospazio, Via A. Gheradesca, 5-56014 Pisa, Italy

1997-120: ELECTRIC PROPULSION EXPERIMENT (EPEX) OF A REPETITIVELY PULSED MPD THRUSTER SYSTEM ONBOARD SPACE FLYER UNIT (SFU); K. Toki, Associate Professor, Y. Shimizu, Research Engineer and K. Kuriki, Professor, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229, Japan

1997-121: ON THE THRUST OF SELF-FIELD MPD THRUSTERS; Edgar Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Princeton University

1997-122: A COMPACT THRUST STAND FOR PULSED PLASMA THRUSTERS; Michael J. Wilson, Stewart S. Bushman, and Rodney L. Burton, Department of Aeronautical and Astronautical Engineering, University of Illinois at Urbana-Champaign, Urbana, Illinois

1997-123: A SIMPLE MARX POWER SYSTEM FOR PULSED PLASMA THRUSTERS; Ivana Hrbud, M. Frank Rose, and Stephen A. Merryman, Space Power Institute, 231 Leach Center, Auburn University, AL

1997-124: DEVELOPMENT OF EQUATION-OF-STATE AND TRANSPORT PROPERTIES FOR MOLECULAR PLASMAS IN PULSED PLASMA THRUSTERS PART I: A TWO-TEMPERATURE EQUATION OF STATE FOR TEFLON; C. S. Schmahl and P. J. Turchi, The Ohio State University, Columbus, Ohio, USA

1997-125: PPT THERMAL MANAGEMENT; H. Kamhawi and P. J. Turchi, The Ohio State University, Columbus, Ohio USA

1997-126: EXPERIMENTAL INVESTIGATION OF THE LES 8/9 PULSED PLASMA THRUSTER PLUME; Robert Eckman and Nikos A. Gatsonis, Mechanical Engineering Dept., Worcester Polytechnic Institute, Worcester, MA 01609; Roger M. Myers, Primex Aerospace, Redmond, WA 98073; and Eric J. Pencil, NASA Lewis Research Center, Cleveland, OH 44135

1997-127: A PERFORMANCE COMPARISON OF PULSED PLASMA THRUSTER ELECTRODE CONFIGURATIONS; Lynn A. Arrington, NYMA, Inc., Tom W. Haag and Eric J. Pencil, NASA Lewis Research Center, and Nicole J. Meckel, Primex Aerospace, Inc.

1997-128: INVESTIGATION OF PULSED PLASMA THRUSTERS FOR SPACECRAFT ATTITUDE CONTOL; N. J. Meckel, R. J. Cassady, R. D. Osborne, W. A. Hoskins, R. M. Myers, PRIMEX Aerospace Company, Redmond, WA

1997-129: THE EXTREME CONTROL SYSTEM OF ELECTRICAL PROPULSION ENGINE MODULE ON THE BASIS OF SPT-100; Olexandre N. Petrenko and Olexandre N. Yatcina, Dnepropetrovsk State University, Institute of Physics and Technology, Naukovy Line, 13, 320625 Dnepropetrovsk-10, Ukraine

1997-130: MULTIPLE THRUSTER PROPULSION SYSTEMS INTEGRATION STUDY; A. V. Rusakov, A. V. Kochergin, A. V. Semenkin, S. O. Tverdokhlebov, and V. I. Garkusha, Central Research Institute of Machine Building (TsMIIMASH), Korolev, Moscow Region, Russia

1997-131: INVESTIGATION OF TAL OPTICAL EMISSIONS; G. F. Karabadzhak and A. V. Semenkin, Central Research Institute of Machine Building (TsNIIMASH), Korolev, Moscow Region, Russia; S. O. Tverdokhlebov, TsNIMMASH-EXPORT, Korolev, Moscow Region, Russia; and D. H. Manzella, NYMA Inc., NASA LeRC, OH, USA

1997-132: INVESTIGATION OF SPT-200 OPERATING CHARACTERISTICS AT POWER LEVELS UP TO 12 KW; B. Arhipov, L. Krochak, N. Maslennikov, and F. Scortecci, Experimental Design Bureau “Fakel”, Kaliningrad (regional), Russia, CENTROSPAZIO, Pisa, Italy

1997-133: COMPLETE COMPUTATIONAL MODEL OF A HALL THRUSTER FROM THE ACCELERATION CHANNEL THROUGH THE PLUME; Salma Qarnain and Daniel E. Hastings, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA

1997-134: THE PPS 1350 PROGRAM; D. Valentian and N. Maslennikov, SEP, Groupe Petite Propulsion et Equipements, Melun Villaroche, France, Fakel, Kaliningrad, Russia

1997-135: DEVELOPMENT OF A HELIUM CRYOPUMPED FACILITY TO EVALUATE HALL EFFECT THRUSTERS; Christopher H. McLean and Olaf Lesky, TRW, Space and Technology Division, Redondo Beach, CA

1997-137: ENDURANCE TEST OF MICROWAVE DISCHARGE ION THRUSTER SYSTEM FOR ASTEROID SAMPLE RETURN MISSION MUSES-C; Hitoshi Kuninaka, Shin Satori, Ikko Funaki, Yukio Shimizu, and Kyoichiro Toki, Institute of Space and Astronautical Science, Yoshinodai, Sagamihara, Kanagawa 229, Japan

1997-138: THE OPTIMISATION OF THE UK-10 ION THRUSTER EXTRACTION GRID SYSTEM; Robert A. Bond, AEA Technology plc, Culham Science and Technology Centre, Abingdon, Oxon, OX14 3DB, United Kingdom; David G. Fearn, Neil C. Wallace and David H. Mundy, Defence Evaluation and Research Agency, Farnborough, Hants, GU14 0LX, United Kingdom

1997-140: THE FLOW MODELING OF CHARGE EXCHANGE IONS IN THE ION THRUSTER; Ivan V. Gavryushin and Vladimir G. Grigoryan, Department of Spacecraft Electric Propulsion and Powerplants, Moscow State Aviation Institute, Russia, 125871 Moscow, Voloklamskoe shosse, d.4

1997-142: EFFECTS OF DISCHARGE CHAMBER CONFIGURATION ON RF PLASMA PROPERTIES; Toshiaki Iwata and Haruki Takegahara, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino, Tokyo 191, Japan

1997-144: ELECTRIC PROPULSION OPTIONS FOR A MAGNETOSPHERIC MAPPING MISSION; Steven Oleson, NYMA Inc., NASA Lewis Research Center, Brookpark, OH 44142; Chris Russell, University of California, Los Angeles, Institute of Geophysics and Planetary Physics, Los Angeles, CA 90095; Kurt Hack and John Riehl, NASA Lewis Research Center, Cleveland, OH 44135

1997-146: ANALYSIS OF PPT POTENTIALITIES IN SOLVING THE SATELLITE ORBIT CONTROL TASKS; V. Akimov, I. Nagel, and I. Ogloblina, Keldysh Research Center, Moscow; N. Antropov, A. Pokryshkin, G. Popov, and A. Rudikov, Research Institute of Applied Mechanics and Electrodynamics, Moscow

1997-147: POWER PLANT CONTROL SYSTEM OPERATION DURING CHANGING SPACECRAFT POSITION; Avil A. Ismailov, Leonid A. Latyshev, and Evgeniy E. Polovcev, Moscow State Aviation Institute (MAI), Department “Spacecraft Electric Propulsion and Powerplants”, Volokolamskoe shosse, d. 4, Moscow, 125871, Russia

1997-149: RESEARCH OF PERFORMANCE OF SMALL THRUST THRUSTERS WITH A CLOSED DRIFT OF ELECTRONS; Sergey N. Kulagin, Olexandre N. Petrenko, and Andrey V. Khitko, Dnepropetrovsk State University, Naukovy Line 13, 320625 Dnepropetrovsk-10, Ukraine

1997-150: THERMAL ANALYSIS OF THE ANODE LAYER THRUSTER OPERATION; V. Garkusha, S. Semenkin, and S. Tverdokhlebov, Central Researche Institute of Machine Building, Moscow reg., Russia

1997-151: SOME RESULTS OF THE SMALL POWER SPT MODELS CREATION; Aidar B. Jakupov, Sergey A. Khartov, and Achmet M. Yakubov, Moscow State Aviation Institute (MAI), Department “Spacecraft Electric Propulsion and Powerplants”, Volokolamskoe shosse, d. 4, Moscow, 125871, Russia

1997-152: SOME REMARKS ABOUT PUBLISHED DATA CONCERNING THE SPT-100 JET PARAMETERS DISTRIBUTION; Sergey A. Khartov, Andrey B. Nadiradze, Achmet M. Yakubov, and Yulia V. Zikeeva, Moscow State Aviation Institute (MAI), Department “Spacecraft Electric Propulsion and Powerplants”, Volokolamskoe shosse, d. 4, Moscow, 125871, Russia

1997-153: RESEARCH OF THE DYNAMIC PRESSURE DISTRIBUTION IN THE PLUME OF THE SPT; R. Y. Gnizdor, K. N. Kozubsky, A. I. Koryakin, Y. M. Lysikov, A. N. Nesterenko, and S. Y. Pridannikov, Experimental Design Bureau “Fakel”, Kaliningrad, Russia

1997-154: INVESTIGATION OF THE POSSIBILITY TO REDUCE SPT PLUME DIVERGENCE BY OPTIMIZATION OF THE MAGNETIC FIELD TOPOLOGY IN THE ACCELERATING CHANNEL; Michael Day, International Space Technology, Inc., Palo Alto, USA; Vladimir Kim, Vyacheslav Kozlov, Alexei Lazurenko, Garry Popov, and Alexander Skrylnikov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute, (RIAME MAI), Moscow, Russia

1997-156: COMPLEX NUMERIC ANALYSIS OF GAS-DISCHARGE CHAMBER PARAPMETERS; S. V. Kanev, L. A. Latyshev, Moscow State Aviation Institute (MAI), Volokolamskoe sh. 4, MAI, Department 208, 125871, Moscow, Russia

1997-157: INVESTIGATION OF A FULLY INTEGRATED SOLAR STATIONARY PLAZMA PROPULSION SYSTEM FOR GEOSTATIONARY ORBIT INSERTION; M. Konstantinov, V. Kim, and F. Scortecci, Moscow Aviation Institute, Russia, Research Institute of the Applied Mechanics and Electrodynamics, Russia, Centrospazio, Piza, Italy

1997-158: TRAJECTORY ANALYSIS OF ELECTRIC PROPULSION SYSTEM WITH THRUST MISALIGNMENT; M. Nakano and Y. Arakawa, The University of Tokyo, Hongo 7-3-1, Bunkyo-ku, 113, Japan

1997-159: LOW THRUST ION PROPULSION FOR ADVANCED APPLICATIONS ON SMALL SATELLITE CONSTELLATIONS; G. Matticari and G. Noci, LABEN Proel Tecnologie Division, Firenze, Italy; G. Perrotta, Alenia Aerospazio, Roma, Italy, and D. G. Fearn, DERA Space Department, Farnborough, UK

1997-160: SIMPLIFIED APPROACH FOR ASSESSMENT OF LOW-THRUST ELLIPTICAL ORBIT TRANSFERS; James E. Pollard, The Aerospace Corporation, P.O. Box 92958, M5-754, Los Angeles, CA 90009

1997-161: CONCEPT OF ELECTRODYNAMCI PROPULSION SYSTEM FOR STATION KEEPING OF LARGE SPACE STRUCTURES; V. A. Strashinksy, Central Research Institute of Machine Building, (TsNIIMASH), Korolev, Moscow Region, Russia

1997-163: PERFORMANCE CHARACTERISTICS OF A SPACE PLASMA SIMULATOR USING AN ELECTRON CYCLOTRON RESONANCE PLASMA ACCELERATOR AND ITS APPLICATIONS TO MATERIAL AND PLASMA INTERACTION RESEARCH; H. Tahara, L. Zhang, T. Yasui, and T. Yoshikawa, Faculty of Engineering Science, Osaka, University, Toyonaka, Osaka, Japan

1997-164: NON-PROPULSIVE APPLICATION OF THE TAL TECHNOLOGY; Alexander V. Semenkin, Sergey O. Tverdokhlebov, and Valerii I. Garcousha, Central Research Institute of Mashine Building (TSNIIMASH), 141070, Korolev, Moscow Region, Russia and Sergey D. Grishin, Moscow State Bauman Technical University

1997-165: HIGH POWER ABLATIVE PULSED PLASMA THRUSTER FOR TECHNOLOGY APPLICATIONS; Yu. A. Alexeev and M. N. Kazeev, RRC “Kurchatov Institute”, Institute of Nuclear Fusion, Kurchatov sq., 1, Moscow, 123182

1997-166: INTERNATIONAL SPACE STATION CATHODE LIFE TESTING; George C. Soulas and Timothy R. Sarver-Verhey, NYMA, Inc., NASA Lewis Research Center Group, Brook Park, OH 44142

1997-167: SPACE STATION CATHODE IGNITION TEST STATUS AT 32,000 CYCLES; James S. Zakany, PE, NYMA, Inc., Brook Park, OH; Luis R. Pinero, PE, NASA Lewis Research Center, Cleveland, OH

1997-168: 28,000 HOUR XENON HOLLOW CATHODE LIFE TEST RESULTS; Timothy R. Sarver-Verhey, NYMA, Inc., NASA Lewis Research Center Group, Brook Park, OH 44142

1997-170: SPACE STATION CATHODE DESIGN, PERFORMANCE, AND OPERATING SPECIFICATIONS; Michael J. Patterson, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio; Timothy R. Verhey, George Soulas, and James Zakany, NYMA, Inc., NASA Lewis Research Center Group, Brook Park, Ohio

1997-171: THE BEHAVIOR OF HOLLOW THERMO-EMISSION LANTHANUM HEXABORIDE ELEMENTS IN SPT CATHODES IN CONNECTION WITH THE MANUFACTURING METHOD; B. Arhipov, Experimental Design Bureau “Fakel”, Kaliningrad, Russia; V. Paderno, Y. Paderno, and V. Filippov, Institute for Problems of Materials of National Academy Sciences of Ukraine, Kiev, Ukraine

1997-173: EFFECTS OF EXTERNAL FLOW NEAR HIGH-CURRENT HOLLOW CATHODES ON ION-ENERGY DISTRIBUTIONS; Ikuya Kameyama and Paul J. Wilbur, Colorado State University, Fort Collins, CO 80523

1997-175: DEVELOPMENT AND RESEARCH OF HEATERLESS CATHODE-NEUTRALIZER FOR LINEAR HALL THRUSTERS (LHD) AND PLASMA ION THRUSTERS (PIT); B. A. Arkhipov, EDB “Fakel”, Kaliningrad, Russia

1997-176: MAKING FULLERENE ION ENGINES WORK; M. W. Crofton and B. B. Brady, Technology Operations, Mechanics & Materials Technology Center, The Aerospace Corporation, P.O. Box 92957, Los Angeles, California 90009

1997-178: EARTH’S MAGNETIC FIELD EFFECT UPON PLASMA PLUMES EXPANSION; A. G. Korsun, E. M. Tverdokhlebova, and F. F. Gabdullin, Central Research Institute of Machine Building (TsNIIMASH), Korolev, Moscow region, Russia

1997-179:  COMPUTATIONAL MODELING OF EXPANDING PLASMA PLUMES IN SPACE USING A PIC-DSMC ALGORITHM; David Y. Oh and Daniel E. Hastings, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA

1997-180: A NUMERICAL MODEL OF THRUSTER-EXHAUST PLUMES; Ikuya Kameyama, Jeffrey M. Monheiser, and Paul J. Wilbur, Colorado State University, Fort Collins, CO 80523

1997-181: ION THRUSTER PLUME PLASMA INTERACTIONS IN THE SOLAR WIND, Joseph Wang, Jet Propulsion Laboratory, California Institute of Technology, Pasadena

1997-182: HYBRID MONTE CARLO – PARTICLE-IN-CELL SIMULATION OF AN ION THRUSTER PLUME; Douglas B. VanGilder, Gabriel I. Font, and Iain D. Boyd, Cornell University, Ithaca, NY 14853, USA

1997-183: THE EXPRESS/T-160E SPACE FLIGHT TEST PROGRAM; J. K. Koester and C. E. Lazarovici, Space Power Incorporated, San Jose, CA; J. M. Sankovic, NASA Lewis Research Center, Cleveland, OH; G. A. Herbert, Schafer Corporation, Arlington, VA; V. A. Petrosov and V. I. Baranov, Keldysh Research Center, Moscow, Russia; A. Romashko and V. Petrusevitch, NPO-PM, Krasnoyarsk, Russia

1997-184: CONSTRAINTS ON ELECTRICAL POWER SYSTEM DESIGN FROM IPS OPERATION; L. Croci, P. Galantini, and A. Trivulzio, FIAR S.p.A. Space Division – a Finmeccanica Company, Via Montefeltro, 8-20126 Milano; H. Bassner, Daimler-Benz Aerospace AG, Space Infrastructure, Postfach 801168-81663 Munich, Germany

1997-185: NUMERICAL THERMAL MODEL OF A 30-CM NSTAR ION THRUSTER; Jon Van Noord and Alec Gallimore, University of Michigan, Ann Arbor, MI 48109-2118; and Vincent K. Rawlin, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH 44135

1997-186: FEEP THRUSTER PERFORMANCE AT HIGH BACKGROUND PRESSURE; Angelo Genovese, Salvo Marcuccio, Davide Dal Pozzo, and Mariano Andrenucci, Centrospazio, Via Gherardesca 5, 56014 Ospedaletto, Pisa, Italy

1997-189: AN EVALUATION OF HOLLOW CATHODE SCALING TO VERY LOW POWER AND FLOW RATE; Matthew T. Domonkos and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory (PEPL), The University of Michigan, Ann Arbor, MI 48109; and Michael J. Patterson, NASA Lewis Research Center, Cleveland, OH 44135

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1999 INDEX

1999-001: ELECTRIC PROPULSION ACTIVITIES IN U.S. INDUSTRY; Dr. Frank M. Curran, Schafer Corportation, Arlington, VA, USA

1999-002: EUROPEAN ELECTRIC PROPULSION ACTIVITIES AND PROGRAMMES; G. Saccoccia, ESA Technical and Operational Support Directorate, ESTEC, Noordwijk, The Netherlands

1999-003: AN OVERVIEW OF CURRENT NASA ACTIVITIES IN ELECTRIC PROPULSION TECHNOLOGY; John M. Sankovic and John W. Dunning Jr., National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field, Cleveland, Ohio USA, 44135

1999-004: MODERN TRENDS OF ELECTRIC PROPULSION ACTIVITIY IN RUSSIA; Vladimir Kim, Garry Popov, and Victor Tikhonov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), Moscow, Russia; Valery Garkusha, The Central Institute of Mashinebuilding, Korolev of Moscow Region, Russia; Vyacheslav Murashko, Design Bureau Fakel, Kaliningrad (obl.), Russia

1999-006: AN OVERVIEW OF ELECTRIC PROPULSION ACTIVITIES IN JAPAN; Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-8581, Japan; Hirokazu Tahara, Area of Aerospace Engineering, Division of Mechanical Science, Department of Systems and Human Science, Osaka University, Toyonaka, Osaka 560-8531, Japan

1999-007: RESEARCH AND DEVELOPMENT ON PLASMA THRUSTERS IN FRANCE; Anne Cadiou, CNES 18 Avenue Edouard Belin 31401 TOULOUSE CEDEX 4, France; Michael Lyszyk, SNECMA, Division SEP Aerodrome de Melun-Villaroche 77550 MOISSY-CRAMAYEL, France; Michael Dudeck, CNRS Laboratoire d’ Aerothermique 4 ter route des Gardes 92190 Meudon, France

1999-008: ELECTRIC PROPULSION ACTIVITIES AT ONERA; Nelly Dorval, Jean Bonnet, Jean-Pierre Marque, and Daniel Pigache, ONERA – Department de Mesures Physiques, 29 Avenue de la Division Leclerc – 92320 Chatillon, France

1999-010: AN OVERVIEW OF ELECTRIC PROPULSION ACTIVITIES IN CSSAR; Hanji Wu and Anjie Li, Center for Space Science & Applied Research, Chinese Academy of Sciences, Beijing 100080, P. R. China

1999-012: AN EXPERIMENTAL RESEARCH ON A CW CO2 LASER THRUSTER; Kazuhiro Toyoda, Kimiya Komurasaki, and Yoshihiro Arakawa, University of Tokyo, Hongo, Bunkyo-ku, 113-8656, Tokyo, Japan

1999-013: THEORETICAL DESIGN OF A GIGAWATT-LEVEL MPD PLASMA SOURCE FOR STUDIES OF MAGNETIC-NOZZLE CONFINEMENT IN FUSION PROPULSION SYSTEMS; Peter J. Turchi and Pavlos G. Mikellides, Department of Aerospace Engineering, Applied Mechanics and Aviation, The Ohio State University, Columbus, Ohio, USA

1999-014: RESEARCH ON COLLOID THRUSTERS; Manuel Martinez-Sanchex, J. Fernandez de la Mora, V. Hruby, M. Gamero-Castano and V. Khayms

1999-017: PLASMA DIAGNOSTICS OF LASER-SUSTAINED PLASMA IN A CW LASER THRUSTER; Satoshi Hosoda, Kazuhiro Toyoda, Kimiya Komurasaki, and Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

1999-018: CFD ANALYSIS OF PLASMA FLOW IN A LASER THRUSTER; P. Molina-Morales, K. Komurasaki, and Y. Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

1999-019: DEVELOPMENT OF A MHD CODE USING CIP METHOD AND ITS APPLICATION TO A LASER FUSION ROCKET; Toshifumi Kawasaki, Takanobu Muranaka and Hideki Nakashima, Department of Advanced Energy Engineering Science, Kyushu University, 6-1, Kasuga-Kouen, Kasuga, Fukuoka 816-8580, Japan

1999-020: ANALYSIS OF PLASMA BEHAVIOR FOR A MAGNETIC THRUST CHAMBER OF LASER FUSION ROCKET BY USING 3D HYBRID CODE; Hideyuki Uchimura, Takanobu Muranaka and Hideki Nakashima, Department of Advanced Energy Engineering Science, Kyushu University, 6-1 Kasuga-Kouen, Fukuoka 816-8560, Japan

1999-021: RESEARCHES FOR REACHING MINIMUM THRUSTS IN REGULATES MONOFUEL MICRO LIQUID PROPULSION THRUSTERS; N. M. Vertakov, EDB “FAKEL”, Kaliningrad, Russia

1999-022: XENON RESISTOJET DESIGN AND DEVELOPMENT; Kent T. Chojnacki and Robert Reinicke, Space Products Division, Moog, Inc., East Aurora, NY 14052-0018

1999-023: EXPERIMENTS OF ARC-HEATED PLASMA FLOW CHARACTERISTICS; Makoto Hirakawa, Keisuke Ichige, Ken-ichi Abe, and Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-8581, Japan

1999-024: THE OUTPUT PARAMETERS AND ANGULAR PLUME CHARACTERISCTICS OF LOW-POWER HALL THRUSTERS; M. B. Belikov, O. A. Gorshkov, and R. N. Rizakhanov, Keldysh Research Center, 8 Onezhskaya, Moscow 125438, Russia

1999-025: DETECTION OF ABLATOR SPALLATION PHENOMENA AT ARC WIND TUNNEL TESTS; Toshinari Yoshinaka, Masahito Mizuno, and Yoshiki Morino, National Space Development Agency of Japan (NASDA), 2-1-1 Sengen, Tsukuba, Ibaraki, 305, Japan

1999-026: PLASMA JET ENHANCED COMBUSTION OF HYDROGEN IN SUPERSONIC AIR FLOW; Toichi Niyama, Hiroshi Itoh, and Toshio Nagashima, Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

1999-028: DEVELOPMENT OF AN ENGINEERING MODEL OF 1 KW HYDRAZINE ARCJET SYSTEM; H. Suzuki, M. Ishii, T. Ohtsuka, K. Kato, K. Uematsu and S. Morimoto, Ishikawajima-Harima Heavy Industries Co., Ltd., 2-2-1, Otemachi, Chiyoda-ku, Tokyo, 100-8182, Japan; T. Yoshikawa and K. Onoe, Osaka University, 1-12, Machikaneyama-cho, Toyonaka-shi, Osaka, Japan

1999-029: THERMO-CHEMICAL NONEQUILIBRIUM MODELING FOR A NITROGEN ARCJET THRUSTER; Shigeru Kuchi-ishi and Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-8581, Japan

1999-030: FLOW ESTABLISHMENT OVER CONSTRUCTOR IN ARCJET OPERATION; A. Sasoh, Shock Wave Research Center, Institute of Fluid Science, Tohoku University, 2-1-1 Katahira, Aoba-ku, Sendai 980-8577, Japan

1999-031: OBSERVATION AND MODELING OF DC ARCJET FLOWFIELD IN STABLE OPERATION; Hironori Sahara and Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan; Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan; and Kyoichi Kuriki, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, Japan, 6-6, Asahigaoka, Hino, Tokyo 191-0065, Japan

1999-032: PERFORMANCE EVALUATION OF A SMALL SIZE ARCJET THRUSTER; Keisuke Ichige, Makoto Hirakawa, Hisashi Kihara, Ken-ichi Abe, and Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-8581, Japan; Masashi Matsumoto, Fluid Dynamics & Combustion Department, Research Institute, Ishikawajima-Harima Heavy Ind. Co. Ltd., Yokohama, 235-0031, Japan

1999-033: THRUST PERFORMANCE AND THERMAL ANALYSIS OF A LOW POWER ARCJET THRUSTER; Shinsuke Hiratsuka, Ken-ichi Onoe, Hirokazu Tahara, and Takao Yoshikawa, Division of Mechanical Science, Department of Systems and Human Science, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan; Hiroshi Suzuki and Kazuo Uematsu, Ishikawajima-Harima Heavy Industries Co., Ltd, 3-1-15, Toyosu, Koto, Tokyo 135-8732, Japan

1999-034: TWO-DIMENSIONAL NUMERICAL SIMULATIONS OF A CESIUM SEEDED HYDROGEN ARCJET; Darrel Robertson and Manuel Martinez-Sanchez, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, Massachusetts

1999-036: A STUDY ON NOZZLE FLOW QUALITY OF LOW POWER ARCJET THRUSTER FOR IMPROVEMENT OF PROPULSION EFFICIENCY; S. Aso, K. Takayanagi, S. Kuti-Ishi, and K. Sugimoto, Department of Aeronautics and Astronautics, Kyushu University

1999-037: EFFECT OF STRONG MAGNETIC FIELD ON PLASMA JET AT A LOW PRESSURE; Kazuo Koike, Eiji Konno, Norifumi Ono, and Ryoichiro Oshima, Department of Mechanical Engineering, Tohoku Gakuin University, 13-1, Chuo-1, Tagajo, Miyagi, 985-8537, Japan

1999-038: CONTAMINATION ANALYSIS FROM THE ESEX 26 KW AMMONIA ARCJET FLIGHT EXPERIMENT; G. G. Spanjers, J. H. Schiling, S. F. Engelman, M. J. Dulligan, and D. R. Bromaghim, Propulsion Directorate, Air Force Research Laboratory, Edwards AFB, CA

1999-039: DIRECT-CURRENT ARCJET PLASMA FEATURE USING AMMONIA AND MIXTURE OF NITROGEN AND HYDROGEN; Sakae Mitsufuji, Hirokazu Tahara, Tomoki Taniguchi, Ken-ichi Onoe, and Takao Yoshikawa, Division of Mechanical Science, Department of Systems and Human Science, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

1999-040: SIMULTANEOUS MEASUREMENTS OF PLUME TEMPERATURE AND ATOMIC NUMBER DENSITY WITH OPTICAL ABSORPTION TOMOGRAPHY; F. Y. Zhang, T. Fujiwara, T. Miyasaka, and J. Harada, Nagoya University, Nagoya, 464-8603, Japan; K. Komurasaki, University of Tokyo, Tokyo, 113-8656, Japan

1999-041: PLUME MASS SPECTROMETRY AND CALORIMETRY WITH A HYDRAZINE ARCJET THRUSTER; James E. Pollard, The Aerospace Corporation, P.O. Box 92957 – 5/754, Los Angeles, CA 90009, USA; Ideo Masuda, National Space Development Agency of Japan, 2-1-1 Sengen, Tsukuba, Ibaraki, 304-8505, Japan; Yoshifumi Gotoh, Mitsubishi Electric Corporation, 325, Kamimachiya Kamakura, Kanagawa 247, Japan

1999-042: NEAR-FIELD MEASUREMENT AND MODELING RESULTS FOR A FLIGHT-TYPE ARCJET: NH MOLECULE; Mark W. Crofton and Teresa A. Moore, Technology Operations, The Aerospace Corporation, M5/754, P.O. Box 92957, Los Angeles, California, 90009, U.S.A.; Iain D. Boyd, Department of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan, 48109-2140, U.S.A.; Ideo Masuda, DRTS Project Team, National Space Development Agency of Japan, 2-1-1 Sengen, Tsukuba, Ibaraki, 305-8505, Japan; Yoshifumi Gotoh, Space Systems Department, Mitsubishi Electric Corporation, 325, Kamimachiya Kamakura, Kanagawa 247, Japan

1999-043: A SIMPLIFIED MODEL FOR THE PREDICTION OF ARCJET PLUMES; Duane A. Nelson, The Aerospace Corporation, P.O. Box 92957, Los Angeles, CA 90009-2957, USA; Yoshifumi Gotoh, Mitsubishi Electric Corp., Kamakura Works, Japan; Ideo Masuda, National Space Development Agency of Japan, Tsukuba, Ibaraski, Japan

1999-044: AN APPROACH TO ARCJET THRUSTER COMPUTATIONS FOR FASTER CONVERGENCE; Shigeru Kuchi-ishi and Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-8581, Japan

1999-045: SIMPLE ESTIMATION OF THE PERFORMANCE OF A LOW POWER ARCJET THRUSTER WITH DIATOMIC GAS AS PROPELLANT; Masahiko Hayatani and Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-8581, Japan

1999-046: PRELIMINARY TEST OF A LOW-POWER DC ARCJET ANODE; I. Funaki, K. Toki, and Y. Shimizu, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa, 229-8510, Japan; Y. Suwana and H. Takegahara, Tokyo Metropolitan Institute of Technology, 6-6 Asahigaoka, Hino, Tokyo 191-0065, Japan; S. Satori, Hokkaido Institute of Technology, 15-4-1 Macdananayo, Teine, Sapporo, Hokkaido, 006-8585, Japan

1999-047: FLOWFIELD OBSERVATION USING A TWO-DIMENSION-LIKE LOW-POWER DC ARCJET; Hironori Sahara, Satoshi Hosoda, and Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan; Yasuyuki Suwama, Kyoichi Kuriki and Haruki Takegahara, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, Japan, 6-6, Asahigaoka, Hino, Toyko 191-0065, Japan; Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

1999-048: NEAR-FIELD MEASUREMENT AND MODELIG RESULTS FOR A FLIGHT-TYPE ARCJET: HYDROGEN ATOM; Mark W. Crofton and Teresa A. Moore, Technology Operations, The Aerospace Corporation, M5/754, P.O. Box 92957, Los Angeles, California, 90009, U.S.A.; Iain D. Boyd, Department of Aerospace Engineering, University of Michigan, 1320 Beal Avenue, Ann Arbor, Michigan, 48109-2140, U.S.A.; Ideo Masuda, DRTS Project Team, National Space Development Agency of Japan, 2-1-1 Sengen, Tsukuba, Ibaraki, 305-8505, Japan; Yoshifumi Gotoh, Space Systems Department, Mitsubishi Electric Corporation, 325, Kamimachiya Kamakura, kanagawa 247, Japan

1999-049: PERFORMANCE IMPROVEMENT OF VERY LOW POWER ARCJETS; Hideyuki Horisawa, Department of Precision Mechanics, Tokai University, 1117 Kitakaname, Hiratsuka-shi, Kanagawa 259-1292, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo, and Nara Textile Inc., 4-19-4 Nakahara, Isogo, Yokohama 235-0036, Japan

1999-050: OPERATIONAL CHARACTERISTICS OF 1 KW HYDRAZINE DC ARCJET SYSTEM; Masahiro Ishii, Koichiro Kato, and Hiroshi Suzuki, Ishikawajima-Harima Heavy Industries Co., Ltd., 299, Tnogaya, Mizuho-machi, Nishitama-gun, Tokyo 190-1297, Japan; Ken-ichi Kajiwara and Akito Hattori, National Space Development Agency of Japan, 2-4-1, Hamamatsu-cho, Minato-ku, Tokyo 105-6126, japan

1999-051: PLASMIC PROPULSION SYSTEM ON S.T.E.N.T.O.R. Program, Thierry Grassin and Luc Petitjean, Alcatel Space Industries, CNES, Centre Spatial de Toulouse

1999-053: DEVELOPMENT OF XENON ION ENGINE SUBSYSTEM FOR ETS-VIII, Eiji Nishida, Toshiyuki Ozaki, Yukikazu Kasai, and Yoshifumi Gotoh, 325 Kamimachiya, Kamakura, Kanagawa, Japan 247-8520, Mitsubishi Electric Corporation (MELCO); Masafumi Ikeda and Ken-ichi Kajiwara, National Space Development Agency of Japan (NASDA)

1999-054: ELECTRIC PROPULSION SYSTEM FOR ARTEMIS; Rainer Killinger, Helmut Bassner, and Gunther Kienlein, Space Infrastructure; Johann Muller, Dornier Satellite Systems, DaimlerChrysler Aerospace AG, Postfach 80 11 69, D-816633 Munchen, Germany

1999-055: XENON GROUND SUPPORT EQUIPMENT FOR PLASMIC PROPULSION SYSTEM; Patrick Bravais, Alain Teissier, and Frederic Ribas, Air Liquide, DTA; Olivier Dulau, Eric Montfort, and Thierry Grassin, Alcatel Space Industries

1999-056: XENON LOADING DEVICE FOR MUSES-C ION ENGINE SYSTEM; Yukio Shimizu, Hitoshi Kuninaka, and Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

1999-057: ION THRUSTER POINTING MECHANISM (ITAM) FOR ARTEMIS: DESIGN & PERFORMANCE; Manfred Falkner, Austrian Aerospace, Stachegasse 16, A-1120 Vienna, Austria

1999-058: PLASMIC PROPULSION LIFETEST; Nunzia Mattei (ASPI), Xavier Ragot (ASPI), Pierre Dumazert (SNECMA), Eric Klinger (SNECMA), Alcatel Space Industries, 100 Bvd du Midi 06150, Cannes la Bocca Cedex, France, SNECMA division SEP Aerodome de Melun-Villaroche, 77055 Moissy Cramayel Cedex, France

1999-059: POWER PROCESSING UNIT FOR STATIONARY PLASMA THRUSTER; H. Declercq, E. Bourguignon, and T. Scalais, Alcatel ETCA, B.P. 4008, B-6000 Charleroi (BELGIUM); J. J. Digoin, Alcatel Space Industries, BP 99, 06322 Cannes La Bocca Cedex, France

1999-060: PERFORMANCE OF HIGH POWER CAPACITORS FOR PULSED PLASMA THRUSTER APPLICATIONS; Zheng Chen and Henry Brandhorst, Space Power Institute, 231 Leach Center, Auburn University, AL 36849-5320, USA

1999-061: DC-DC CONVERTER FOR HALL THRUSTER PLASMA DISCHARGE; V. Hruby, W. Connolly, J. Monheiser, B. Pote, and C. Freeman, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760-1023

1999-064: A DIGITAL XENON FLOW CONTROLLER BASED ON ChEMS TECHNOLOGY; Joe Cardin, Director, Business Development, Ben Otsap, Chief Engineer, VACCO Industries, South El Monte, CA 91733

1999-065: DEVELOPMENT OF AN ION THRUSTER CONTROL UNIT FOR THE MUSES-C MISSION; Kazutaka Nishiyama and Hitoshi Kuninaka, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

1999-066: DEVELOPMENT OF A “SMART” POWER PROCESSING UNIT FOR HALL EFFECT THRUSTERS; J. Dickens and M. Kristiansen, Texas Tech University, Electrical Engineering Department, Lubbock, TX 79409-3102

1999-069: ONE MILLINEWTON FEEP THRUSTER TESTS; Salvo Marcuccio, Marco Saviozzi, Fabrizio Rugo, and Mariano Andrenucci, Centrospazio, 56014 Ospedaletto, Pisa, Italy

1999-070: BACKFLOW CONTAMINATION OF INDIUM-METAL ION EMITTERS (LMIE): NUMERICAL SIMULATIONS; M. Tajmar, Vienna University of Technology, Institut fur Angewandte Elektronik und Quantenelektronik, GuBhausstrasse 27-29, A-1040 Vienna, Austria; F. Rudenauer and M. Fehringer, Austrian Research Center, A-2444, Seibersdorf, Austria

1999-071: EXPERIMENTAL PERFORMANCE OF A LOW POWER NEUTRALIZER FOR A MICRONEWTON FEEP THRUSTER; Salvo Marcuccio, Gabriele Lorenzi, and Mariano Andrenucci, Centrospazio, 56014 Ospedaletto, Pisa, Italy

1999-072: MICRONEWTON INDIUM ION THRUSTERS; Michael Fehringer, Friedrich Rudenauer, and Wolfgang Steiger, Austrian Research Centre Seibersdorf, A-2444 Seibersdorf

1999-073: PLUME STUDY OF MULTIMODE THRUSTER SPT-140; K. Kozubsky, S. Kudriavtzev, and S. Pridannikov, Fakel, Moskovsky pr. 181, Kaliningrad, 236001, Russia

1999-074: SPT100 PLASMA JET EFFECTS ON GEOSTATIONARY SATELLITE COMMUNICATIONS; Claude Berthou and Denis Pogarieloff, Alcatel Space Industries, 100 Bd du Midi 06156 Cannes la Bocca Cedex, France

1999-076: ANALYSIS OF COLLISION PHENOMENA IN HALL THRUSTER PLUMES; Douglas B. VanGilder and Iain D. Boyd, Mechanical and Aerospace Engineering, Cornell University, Ithaca, NY 14853, U.S.A.

1999-078: CHARACTERIZATION OF THE INTERNAL PLASMA STRUCTURE OF A 5 KW HALL THRUSTER; James M. Haas and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, The University of Michigan, College of Engineering, Ann Arbor, MI 48109, USA

1999-079: EXPERIMENTAL AND NUMERICAL STUDY OF DISTURBANCE FORCES INDUCED BY A SPT100 PLASMA JET; Stephane d’Halewyn, Claude Berthou, Danielle Borie (Alcatel Space Industries), Pascal Lasgorceix, Stephane Bechu, Alain Hauser (Laboratoire d’Aerothermique – CNRS Orleans), Alcatel Space Industries 100 Bd du Midi 06156 Cannes la Bocca Cedex, France

1999-080: PERFORMANCE OF AN 8 KW HALL THRUSTER; B. Pote, V. Hruby, and J. Monheiser, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760-1023, USA

1999-082: EXPERIMENTAL INVESTIGATION NEGATIVE IONS IN SPT THRUSTER CHANNEL; A. I. Bugrova, A. V. Desiatskov, A. I. Morosov, and V. K. Kharchevnikov, MIREA, Russia

1999-083: INVESTIGATION OF XENON ION SPUTTERING OF ONE CERAMIC MATERIAL USED IN SPT DISCHARGE CHAMBER; Y. Garnier, V. Viel, and J-F. Roussel, ONERA-DESP, 2 avenue Belin, BP 4025, 31055 Toulouse Cedex, France; D. Pagnon, L. Magne, and M. Touzeau, LPGP – Universite Paris-Sud, Bat, 210, 91405 Orsay Cedex, France

1999-084: INVESTIGATION OF THE STATIONARY PLASMA THRUSTER (SPT) OUTGASSING AND ITS THERMAL STATE IMPACT ON THRUSTER PERFORMANCE VARIATION IN TIME; Vladimir Kim, Vyacheslav Kozlov, Garry Popov, and Alexander Skrylnikov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), 4, Volokolamskoe shosse, Moscow, 125810, Russia; Konstantin Kozubsky, Design Bureau Fakel, 181, Moskovski Prospect, Kaliningrad, 236001, Russia; and Michal Lyszyk, Societe Europeenne de Propulsion (SEP), division of SNECMA, Aerodrome de Melun-Villaroche-F77550, Moissy-Cramayel-France

1999-086: PERFORMANCE OF STATIONARY PLASMA THRUSTER PPS1350 AND ITS QUALIFICATION STATUS IN RUSSIA; V. Gopantchuk, K. Kozubsky, N. Maslennikov, and S. Pridannikov, Fakel, Moscovsky pr. 181, Kaliningrad 236001, Russia

1999-087: PPS 1350 QUALIFICATIONS STATUS; M. Lyszyk, E. Klinger, O. Secheresse, JP. Bugeat and D. Valentian, SNECMA, Division SEP, Aerodrome de Melun-Villaroche, Moissy-Cramayel, France; A. Cadiou, Th. Beltan and C. Gelas, CNES, Centre Spatial de Toulouse, 18 Avenue Edouard Belin, Toulouse, France

1999-090: PERFORMANCE AND QUALIFCATION STATUS OF MULTIMODE STATIONARY PLASMA THRUSTER SPT-140; R. Gnizdor, K. Kozubsky, N. Maslennikov, V. Murashko, and S. Pridannikov, Fakel, Moscovsky pr. 181, Kaliningrad 236001, Russia; V. Kim, RIAME, Volokolamskoe sh. 4, Moscow 125871, Russia

1999-092: LOW POWER, HALL THRUSTER PROPULSION SYSTEM; V. Hruby, J. Monheiser, B. Pote, C. Freeman, and W. Connolly, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760-1023

1999-094: THE OUTPUT PARAMETERS AND ANGULAR PLUME CHARACTERISTICS OF LOW-POWER HALL THRUSTERS; M. B. Belikov, O. A. Gorshkov, and R. N. Rizakhanov, Keldysh Research Center, 8 Onezhskaya, Moscow 125438, Russia

1999-097: NUMERICAL SIMULATION OF FACILITY EFFECTS ON HALL THRUSTER PERFORMANCE, John Michael Fife and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, Massachusetts

1999-098: COMPUTATION OF HALL THRUSTER PERFORMANCE; L. Garrigues and J.P. Boeuf, Centre de Physique des Plasmas et Applications de Toulouse, Universite Paul Sabatier, 118 route de Narbonne, 31062 Toulouse Cedex 4, France; I. D. Boyd, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109, USA

1999-099: FUNDATMENTAL DESIGN OF HIGHLY EFFECTIVE HALL THRUSTERS; Yuri M. Yashnov, Consultant, Moscow, Russia; J. Kent Koester, John B. McVey, and Edward J. Britt, Space Power, Inc., 1253 Reamwood Ave., Sunnyvale, CA 94089

1999-100: PARTICLE-IN-CELL MODELING OF THRUSTER WITH ANODE LAYER (TAL); James J. Szabo Jr., Manuel Martinez-Sanchez, and Oleg Batishchev, Massachusetts Institute of Technology, Cambridge, Massachusetts, 02139

1999-101: SEGMENTED ELECTRODE HALL THRUSTER OPERATION IN SINGLE AND TWO STAGE REGIMES; N. J. Fisch, Y. Raitses, A. A. Litvak, and L. A. Dorf, Princeton Plasma Physics Laboratory, Princeton University, Princeton, NJ 08540

1999-102: CHARACTERISTICS OF THE SPT100-ML COMPARISONS BETWEEN EXPERIMENTS AND MODELS; L. Garrigues and J. P. Boeuf,  Centre de Physique des Plasmas et Applications de Toulouse, Universite Paul Sabatier, 118 route de Narbonne, 31062 Toulouse Cedex 4, France; C. Perot, N. Gascon, S. Bechu, P. Lasgorceix, and M. Dudeck, Laboratoire d’Aerothermique, 2 rue du crital, 45100 Orleans, France

1999-103: THE PRINCIPLE OF CURRENT MAXIMALITY FOR DISCHARGE SIMULATION IN ACD; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, and A. I. Vasin, Keldysh Research Center, Onezhskaya 8, Moscow, 12548, Russia

1999-104: CHARACTERIZATION OF FMT-2 DISCHARGE CATHODE PLUE; George J. Williams Jr., Timothy B. Smith, Travis A. Patrick, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, The University of Michigan, 1919 Green Rd., Ann Arbor, MI 48105, USA

1999-105: LINEAR 1-D ANALYSIS OF ASCILLATIONS IN HALL THRUSTERS; Reid Noguchi, Graduate Student, MIT, Cambridge, MA, USA; Manuel Martinez-Sanchez, Professor of Aeronautics/Astronautics, MIT, Cambridge, MA, USA; and Eduardo Ahedo, Polytechnical University of Madrid, Spain

1999-106: MEMBRANE OSCILLATIONS IN SPT CHANNEL; A. I. Bugrova, A. S. Lipatov, A. I. Morosov, and V. K. Kharchevnikov, MIREA, Russia

1999-108: STEADY ACCELERATION IN THE HALL THRUSTER; A. Cohen-Zur, Faculty of Aerospace Engineering, Technion – Israel Institute of Technology, Haifa 32000, Israel; A. Fruchtman, Center for Technological Education Holonn, 52 Golomb St., P.O. Box 305 Holon 58102, Israel; and J. Ashkenazy, Propulsion Pysics Laboratory, Soreq NRC, Yavne 81800, Israel

1999-112: ELECTRON CONDUCTIVITY IN ACD; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, and A. I. Vasin, Keldysh Research Center, Onezhskaya 8, Moscow, 125438, Russia

1999-113: DEVELOPMENT OF A 45-DEGREE PARALLEL-PLATE ELECTROSTATIC ENERGY ANALYZER FOR HALL THRUSTER PLUME STUDIES: PRELIMINARY DATA; Richard R. Hofer, James M. Haas, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory (PEPL), Department of Aerospace Engineering, College of Engineering, University of Michigan, Ann Arbor, MI 48109, USA

1999-114: COMPUTATIONAL MODELING OF PLASMA PLUMES IN A VACUUM TANK; Bernard Asare, MIT, Cambridge, MA, USA; and Manuel Martinez-Sanchez, Aeronautics/Astronautics, MIT, Cambridge, MA, USA

1999-117: INVESTIGATION OF POSSIBILITY TO INCREASE THE TRUSTIER EFFICIENCY, DISCHARGE EFFICIENCY AND THE SPD LIFE-TIME BY INFLUENCE TO THE SPEED OF THE NEUTRAL PROPELLANT GAS STREAM; A. V. Loyan and S. A. Oghienko. Scientific & Technological Center of Space Power & Engines at State Aerospace University nm. N. E. Gukovsky “KhAI”, (STC SPE “KhAI”) Kharkov, 310070, Chcalova St., 17, Ukraine

1999-118: STUDY OF PLASMA DYNAMICS IN THE VARIABLE SECTION CHANNEL OF STATIONARY PLASMA THRUSTER; Boris Arhipov, Design Bureau Fakel, Kaliningrad (obl.), Russia; Elena Goghaya, Kaliningrad State University, Kaliningrad (obl.), Russia; and Nikolay Nikulin, Kaliningrad State University, Kaliningrad (obl), Russia

1999-119: INVESTIGATION OF THE STATIONARY PLASMA THRUSTER SCALE IMPACT ON THE ELECTRIC FILTER PARAMETER CHOICE; Vladimir Kim, Vyacheslav Kozlov, Garry Popov, and Alexander Skrylnikov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), 4, Volokolamskoe shosse, Moscow, 125810, Russia

1999-121: RESEARCH AND DEVELOPMENT OF HALL EFFECT THRUSTERS AT OSAKA UNIVERSITY; Daisuke Goto, Hirokazu Tahara, Yohei Nikai, Toshiaki Yasui, and Takao Yoshikawa, Division of Mechanical Science, Department of Systems and Human Service, Graduate School of Engineering Science, Osaka University, 103, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

1999-123: THE OPTIMAL CONTROL OF THRUST VECTOR OF HALL-THRUSTERS; Yuri M. Yashnov, Consultant, Moscow, Russia; J. Kent Koester, John B. McVey, and Edward J. Britt, Space Power Inc., 1253 Reamwood Ave., Sunnyvale, CA, 94089

1999-124: AN EXPERIMENTAL INVESTIGATION OF THE HOLLOW CATHODES FOR LOW-POWER ION THRUSTER; O. A. Gorshkov and V. A. Muravlev, Keldysh Research Center, 8/10, Onezhskaya, Moscow, 12548, Russia

1999-125: THE GENERATION OF HIGH ENERGY IONS IN HOLLOW CATHODE DISCHARGES; Stephen W. Patterson, Plasma Physics Group, Imperial College, London, UK; David G. Fearn, Space Department, Defence Evaluation and Research Agency, Farnborough,, Hants, UK

1999-126: SCENARIO FOR HOLLOW CATHODE END-OF-LIFE; Timothy R. Sarver-Verhey, Dynacs Engineering Co., Inc., NASA Glenn Research Center Group, 2001 Aerospace Parkway, Brook Park, OH 44142

1999-127: PHYSIC-MATHEMATICS MODEL OF A SELF-HEATED HOLLOW CATHODE ELECTRIC DISCHARGE EVOLUTION; Sergiy A. Lobov and Andriy V. Loyan, STC SPE “KhAI”, 17, Chkalova st., 310070, Kharkov, Ukraine

1999-128: HEAT BALANCE IN A NEUTRALIZER CATHODE OF STATIONARY PLASMA THRUSTER (SPT); Dr. B. Arkhipov, EDB FAKEL, Moskovski pr. 181, Kaliningrad 236000, Russia

1999-131: RESEARCHING OF RUNNING-IN, STARTING, TRANSITION THERMAL PROCESSES OF SELF-HEATED HOLLOW CATHODE IN ELECTRIC CURRENT RANGE FROM 5 UP TO 25 A; Sergiy A. Lobov and Andriy V. Loyan, STC SPE “KhAI”, 17, Chkalova st., 310070, Kharkov, Ukraine

1999-133: THE COMPATIBILITY OF HOLLOW CATHODE CHARACTERISTICS WITH A VARIETY OF ION THRUSTER DESIGNS; David G. Fearn, Space Department, Defence Evaluation and Research Agency, Farnborough, Hants, GU14 0LX, UK; Stephen W. Patterson, Plasma Physics Group, Imperial College, London, SW7 2BZ, UK

1999-135: INVESTIGATION OF SELF-HEATE HOLLOW CATHODES OPERATION POSSIBILITY IN WATER MOIST STREAM OF HIGH-PRESSURE CONDITION; N. N. Koshelev and A. V. Loyan, STC SPE “KhAI”, 17, Chkalova st., 310070, Kharkov, Ukraine; V. P. Sklarov and A. A. Tarelin, Machine Problem Institute of Ukrainian Engineer Sciences Academy, ‘MPI UESA”, Ukraine

1999-137: EXPERIMENTAL INVESTIGATION OF A GAS PROPELLANT CONSUMPTION OSCILLATION WHEN SELF-HEATED HOLLOW CATHODE IS STARTING FROM A COLD STATE; Nikolay N. Koshelev, Sergiy A. Lobov, and Andriy V. Loyan, STC SPE “KhAI”, 17, Chkalova st., 310070, Kharkov, Ukraine

1999-138: ANALYZE OF GAS PROPELLANT CONSUMPTION OSCILLATION WHEN THE SELF-HEATED HOLLOW CATHODE IS STARTING “COLD” STATE; Andriy V. Loyan, Scientific and Technological Center of Space Power and Engines at Kharkov Aviation Institute, 17, Chkalova st., Kharkov, 310070, Ukraine

1999-139: DEVELOPMENT STATUS OF A MICROWAVE ION ENGINE SYSTEM FOR THE MUSES-C MISSION; Kyoichiro Toki, Hitoshi Kuninaka, Ikkoh Funaki, Kazutaka Nishiyama, and Yukio Shimizu, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

1999-140: DEVELOPMENT OF AN RF-ION THRUSTER FOR COMMERCIAL APPLICATION; Rainer Killinger and Helmut Bassner, Space Infrastructure; Johann Muller, Dornier Satellite Systems, DaimlerChrysler Aerospace AG, Postfach 80 11 69, D-816633 Munchen, Germany

1999-141: ROLE OF MAGNETIC FIELD IN KAUFMAN TYPE ELECTROSTATIC ION THRUSTERS; A. K. Malik, Plasma Physics, Blackett Laboratory, Imperial College, London, SW7 2AZ

1999-142: 1000-HOUR TEST OF A 35-CM DIAMETER XENON ION THRUSTER; S. Kitamura, Y. Hayakawa, and K. Miyazaki, National Aerospace Laboratory, 7-44-1 Jindaijihigashi-machi, Chofu, Tokyo 182-8522, Japan; H. Yoshida, Y. Yamamoto and K. Akai, Toshida, Y. Yamamoto and K. Akai, Toshiba Corporation, 1 Komukai, Toshiba-cho, Saiwai-ku, Kawasaski, Kanagawa 210-0863, Japan

1999-143: A XENON PROPELLANT MANAGEMENT SUB-UNIT FOR ION PROPULSION; Keith Dyer, VACCO Industries, South El Monte, CA 91733; Anthony Dien, Stanford Mu Corporation, Harbor City, CA 90710; Eiji Nishida and Yukikazu Kasai, Mitsubishi Electric Corp., Kanagawa, Japan; Masafumi Ikeda and Kenishi Kajiwara, NASDA, Japan

1999-144: BEAM INTENSTIY DISTRIBUTION OF A RING-CUSP ION THRUSTER; H. Yoshida, Y. Yamamoto, and K. Akai, Toshiba Corporation, 4-1, Ukishimacho, Kawasakiku, Kawasaki, Kanagawa 210-0862, Japan; Y. Hayakawa, K. Miyazaki and S. Kitamura, National Aerospace Laboratory, 7-44-1, Jindaiji-higashicho, Chofu, Tokyo 182-8522, Japan

1999-145: ION THRUSTER LIFETIME ESTIMATION AND MODELING USING COMPUTER SIMULATION; Masakatsu Nakano, Satellite Venture Business Laboratory, Kyushu Institute of Technology, 1-1, Sensuicho, Tobata-ku, Kitakyushu-Shi, Fukuoka 804-8550, Japan; Yoshihiro Arakawa, Department of Aeronautics and Astronautics, The University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

1999-146: PARTICLE SIMULATION ON ION BEAM EXTRACTION PHENOMENA IN AN ION THRUSTER; Yasushi Okawa and Haruki Takegahara, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino, Tokyo 191-0065, Japan

1999-147: VALIDATION OF A GRID-EROSION SIMULATION BY SHORT-TIME EROSION MEASUREMENTS; M. Tartz, E. Hartmann, R. Deltschew, and H. Neumann, Institut fur Oberflachenmodifizierung (IOM) e. V., Permoserstr, 15, D-04318 Leipzig, Germany

1999-148: APPLICATION OF AMORPHOUS-CARBON GRIDS TO AN ION THRUSTER; Hirohiko Satow and Haruki Takegahara, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino, Tokyo 191-0065, Japan; Takeshi Tachibana, Department of Mechanical and Control Engineering, Kyushu Institute of Technology, 1-1, Sensuityo, Tobata, Kitakyushu, Fukuoka 804-0015, Japan; Katsumi Kawata, Astec Irie Corporation, 1-3-1, Otani, Yahatahigashi, Kitakyushu, Fukuoka 805-0053, Japan

1999-149: TITANIUM OPTICS FOR ION THRUSTERS; George C. Soulas, Dynacs Engineering Co., Inc., NASA Glenn Research Center Group, 2001 Aerospace Parkway, Brook Park, OH 44142, U.S.A.; Thomas W. Haag, Michael J. Patterson, and Vincent K. Rawlin, NASA Glenn Research Center, 21000 Brookpark Road, Cleveland, OH 44135, U.S.A.

1999-150: SIMULATION OF ELECTROMAGNETIC INTERFERENCE INDUCED BY ION THRUSTER PLUME, Masahiro Kajikawa and Mengu Cho, Department of Electrical Engineering, Kyushu Institute of Technology, Tobata-ku, Kitakyushu, Japan 804-8550

1999-151: DEEP SPACE ONE INVESTIGATIONS OF ION PROPULSION PLASMA ENVIRONMENT: INITIAL RESULTS; J. Wang, D. E. Brinza, J. E. Polk, and M. D. Henry, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

1999-153: IMPROVEMENT OF 20 MN XENNON ION THRUSTER; Toshiyuki Ozaki, Yukikazu Kasai, and Eiji Nishida, Space Engineering Department, Kamakura Works, Mitsubishi Electric Corporation, 325 Kamimachiya, Kamakura, Kanagawa 247-8520, Japan

1999-154: PERFORMANCE IMPROVEMENT OF RADIOFREQUENCY ION THRUSTERS – THE EVOLUATION OF THE RIT 15 ION ENGINE; H. J. Leiter, H. W. Loeb and K. H. Schartner, 1st Institute of Physics, Heinrich-Buff-Ring 16, 35392 Giessen, Germany

1999-156: C60 PLASMA AND ION BEAM DIAGNOSTICS IN AN ELECTRON BOMBARDMENT ION THRUSTER; Satoru Sugaya and Haruki Takegahara, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino, Tokyo 191-0065, Japan; Yoshinori Nakayama, Department of Aerospace Engineering, National Defense Academy, Hashirimizu 1-10-20, Yokosuka 239-8686, Japan

1999-157: PLASMA PROPERTIES AROUND THE BAFFLE APERTURE REGION OF THE UK25 ION THRUSTER; David J. Milligan and Stephen B. Gabriel, Astronautics Research Group, School of Engineering, University of Southampton, Highfield, Southampton SO17 1BJ, UK

1999-158: DEVELOPMENT AND PERFORMANCE TESTING OF AN RF-ION THRUSTER FOR PRIMARY PROPULSION; Helmut Bassner, Space Infrastructure, Daimler-Benz Aerospace AG, Postfach 80 11 69, D-81663, Germany; Robert Bond and Vaughan Thompson, AEA Technology plc, Cullham Science and Technology Centre, Abingdon, Oxon OX14 3DB, United Kingdom

1999-159: ENHANCED DISCHARGE PERFORMANCE IN A RING CUSP PLASMA SOURCE; John E. Foster and Michael J. Patterson, NASA Glenn Research Center, 21000 Brookpark Road, Cleveland, OH 44135

1999-160: ELECTION EMISSION MECHANISM OF MICROWAVE DISCHARGE NEUTRALIZER; Noriyoshi Onodera and Haruki Takegahara, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino-shi, Tokyo 191-0065, Japan; Kazutaka Nishiyama, Ikko Funaki, and Hitoshi Kuninaka, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara-shi, Kanagawa 229-8510, Japan

1999-162: NUMERICAL MODELING OF EXTRACTION SYSTEMS IN ION THRUSTERS; V. A. Muravlev and A. A. Shagayda, Keldysh Research Center, Onezhskaya 8/10, Moscow, 125438, Russia

1999-163: INVESTIGATION OF NEAR-CATHODE AREA OF 5-CM ION THRUSTER: A CURRENT STATE OF WORK; O. A. Gorshkov and M. V. Zikeyev, Keldysh Research Center, Onezhskaya 8/10, Moscow, 125438, Russia

1999-164: VERIFICATION TESTS OF 10-CM-DIAM. CARBON-CARBON COMPOSITE GRIDS FOR MICROWAVE DISCHARGE ION THRUSTER; I. Funaki, H. Kuninaka, Y. Shimizu, K. Toki, S. Satori, and K. Nishiyama, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa, 229-8510, Japan

1999-165: SCALING LAW APPLICABLE TO DESIGN OF MPD ARCJET; Yukio Shimizu, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan; Kyoichi Kuriki, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino-shi, Tokyo 191-0065, Japan

1999-166: THERMAL ANALYSIS OF A LORENTZ FORCE ACCELERATOR WITH AN OPEN LITHIUM HEAT PIPE; G. Emsellem, A. D. Kodys, and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), MAE Dept., Princeton University, Princeton, NJ 08544

1999-167: CHARACTERISATION OF A STEADY STATE MPD THRUSTER WITH RADIATION COOLED ANODE; Michael Winter, Monika Auweter-Kurtz, Christian Boie, Jorg Heiermann, and Helmut L. Kurtz; Institut für Raumfahrtsysteme, Universität Stuttgart, Pfaffenwaldring 31, D70550 Stuttgart, Germany

1999-168: NUMERICAL STUDY OF ONSET PHENOMENA IN A 2-DIMENSIONAL AXISYMMETRIC MPD THRUSTER; Takeshi Miyasaka and Toshi Fujiwara, Department of Aerospace Engineering, Nagoya University, Furo-cho Chikusa-ku, Nagoya, 464-8603, Japan

1999-169: RECENT IMPROVEMENTS OF NUMERICAL METHODS FOR THE SIMULATION OF MPD THRUSTER FLOW ON ADAPTIVE MESHES; J. Heiermann, M. Auweter-Kurtz, and H. J. Kaeppeler, Institute for Space Systems, Stuttgart University, 70550 Stuttgart, Germany; A. Eberle, DaimlerChrysler Aerospace AG, Military Aircraft MT-63, 81663 Munich, Germany; U. Iben, Robert Bosch GmbH, 70049 Stuttgart, Germany; and P. C. Sleziona, Institute of Industrial Mathematics, University of Kaiserslautern, 67663 Kaiserslautern, Germany

1999-170: LOW TEMPERATURE CATHODE OPERATION: A SPOT MODEL-PART I; Paola Rossetti, Fabrizio Paganucci, and Mariano Andrenucci, Centrospazio, Via Gherardesca 5, 1-56014, Pisa, Italia

1999-171: ONE-DIMENSIONAL NUMERICAL SIMULATION OF TWO-FLUID NONEQUILIBRIUM PLASMA FLOW IN MPD THRUSTERS; Nobuyuki Fukuoka, Takeshi Miyasaka, and Toshi Fujiwara, Department of Aerospace Engineering, Nagoya University, Furo-cho Chikusa-ku, Nagoya, 464-8603, Japan

1999-172: ELECTRODE POWER LOSS AND THRUSTER PERFORMANCE OF A PULSED MPD ACCELERATOR; Yoichi Kagaya, Hirokazu Tahara, and Takao Yoshikawa, Division of Mechanical Science, Department of Systems and Human Science, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka, 560-8531, Japan

1999-173: CATHODE JET OF MAGNETOPLASMADYNAMIC THRUSTERS; Kazunori Mitsuo, Hirokazu Tahara, Hiroshi Hamano, Yoichi Kagaya, and Takao Yoshikawa, Division of Mechanical Science, Department of Systems and Human Science, Graduate School of Engineering Science, Osaka University, Machikaneyama 1-3, Toyonaka, Osaka 560-8531, Japan

1999-174: TEMPERATURE AND MATERIAL EFFECTS ON THE OPERATION OF MPD CATHODES; Fabrizio Paganucci, Paola Rossetti, and Mariano Andrenucci, Centrospazio, Via Gherardesca 5, 1-56014, Pisa, Italia

1999-175: SUPERSONIC PLASMA FLOW IN A MAGNETIC NOZZLE; Masaki Inutake, Kunihiko Hattori, Akira Ando, Fumio Hori, Taku Sugimura, Kenji Fukushi, Tsutomu Ochiai, Masaya Yamamoto, Tsuyoshi Yagai, Atsushi Imasaki, and Mikirou Yoshinuma, Department of Electrical Engineering, Tohokuu University, Aoba, Sendai, 980-8579, Japan

1999-176: OWN MAGNETIC FIELD IMPACT ON MPD THRUSTERS PERFORMANCE WITH EXTERNAL MAGNETIC FIELD; Victor B. Tikhonov and Sergei A. Semenikhin, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute, Russia, 4, Volokolamskoe shosse, Moscow, 125810, Russia; James E. Polk, Jet Propulsion Laboratory, 4800 Oak Grove Drive, Mail Stop 125-224, Pasadena, CA 91109

1999-177: NUMERICAL ANALYSES OF MHD FLOWS IN AN APPLIED-FIELD MPD ACRJET THRUSTER; Hiroshi Katsurayama, Takeshi Miyasaka, and Toshi Fujiwara, Department of  Aerospace Engineering, Nagoya University, Furo, Chikusa-ku, Nagoya, 464-8603, Japan

1999-179: ARC STRUCTURE IN A COAXIAL MAGNETOPLASMADYNAMIC CHANNEL; Kazunori Mitsuo, Hirokazu Tahara, Taro Kimura, Yoichi Kagaya, and Takao Yoshikawa, Division of Mechanical Science, Department of Systems and Human Science, Graduate School of Engineering Science, Osaka University, Machikaneyama 1-3, Toyonaka, Osaka 560-8531, Japan

1999-180: MACH-PROBE CHARACTERISTICS IN A MAGNETIZED PLASMA FLOW; Akira Ando, Kunihiko Hattori, Masaaki Inutake, Taku Sugimura, Fumio Hori, Kenji Fukushi, Tsutomu Ochiai, Masaya Yamamoto, Tsuyoshi Yagai, Atsushi Imasaki, and Mikirou Yoshinuma, Department of Electrical Engineering, Tohoku University, Aoba, Sendai, 980-8579, Japan

1999-181: DESIGN OF A SOLAR ELECTRIC PROPULSION TRANSFER VEHICLE FOR A NON-NUCLEAR HUMAN MARS EXPLORATION ARCHITECTURE; Leonard A. Dudzinski, Kurt J. Hack, Leon P. Gefert, Thomas W. Kerslake, and Alen W. Hewston NASA John H. Glenn Research Center, 21000 Brookpark Rd, Cleveland, OH USA

1999-182: AN OVERVIEW OF THE ON-ORBIT RESULTS FROM THE ELECTRIC PROPULSION SPACE EXPERIMENT (ESEX), D. R. Bromaghim, J. R. LeDuc, R. M. Salasovich, J. A. Zimmerman, D. C. Matias, A. M. Sutton, G. G. Spanjers, J. M. Fife, W. H. Hargus, and R. A. Spores, USAF Research Laboratory, Edwards AFB, CA; M. J. Dulligan and S. F. Engelman, ERC, Inc., USAF Research Laboratory, Edwards AFB, CA; J. H. Schiling and D. C. White, W. E. Research, LLC, Rosamond, CA; and L. K. Johnson, The Aerospace Corporation, El Segundo, CA

1999-183: TORGUE CONTROL OF HALL PROPELLED SMALL SPACECRAFT; Joseph Ashkenazy and Gabi Appelbaum, Propulsion Physics Laboratory, Soreq NRC, Yavne 81800, Israel; Moshe Guelman and Alex Kogan, Asher Space Research Institute, Technion I.I.T. Haifa 32000, Israel

1999-185: ADVANCED ELECTRIC PROPULSION FOR RLV LAUNCHED GEOSYNCHRONOUS SPACECRAFT; Steven R. Oleson, National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field, Cleveland, OH 44135

1999-186: FEASIBILITY STUDY OF NANOSATELLITE BASED ON COMMERICIAL TECHNOLOGY; Shin Satori, Masahiro Suzuki, Masami Sasaki, Ryuichi Mitsuhasi, and Satoshi Takezawa, Hokkaido Institute of Technology; Hiroyuki Okamoto, Astro Research Company; Shin’ichi Nakasuka, University of  Tokyo; Nobutada Sako, Graduate School of Engineering, University of Tokyo; Tomohiro Isikawa and Atsushi Nagata, Graduate School of Engineering, Hokkaido Institute of Technology

1999-187: TWO NEW SPACECRAFT ARCHITECTURES AND THEIR IMPACTS ON ELECTRIC PROPULSION; Shinichi Nakasuka, Yuichi Tsuda, and Takashi Eijima, Department of Aeronautics and Astronautics, University of Tokyo, Hongo 7-3-1, Bunkyo-ku, Tokyo 113-8656, Japan; Yasuhiro Kawakatsu and Ryuichi Nagashima, Tsukuba Space Center, NASDA, Sengen 2-1-1, Tsukuba, 305-8505, Japan

1999-188: A METHOD OF PLACING A SPACECRAFT ON HIGH ORBIT; V. N. Vinogradov, V. M. Murashko, and A. G. Nattyn, Fakel, Moskovsky pr. 181, Kaliningrad 236001, Russia

1999-189: VERY LONG RANGE EXPLORATION BY MEANS OF ELECTRIC PROPULSION AND COMETARY RESOURCE UTILIZATION; P. J. Turchi and C. A. Scharlemann, Aerospace Engineering, Applied Mechanics and Aviation Department, The Ohio State University, Columbus, Ohio, USA

1999-190: THE PRELIMINARY STUDY ON THE EFFECTIVE UTILIZATION OF A LUNAR-DERIVED PROPELLANT (LOX); R. Nagashima, Y. Kawakatsu, and T. Yokoyama, National Space Development Agency of Japan, Tsukuba Space Center, 2-1-1, Sengen, Tsukuba-City, Ibaraki, 305-0047, Japan; S. Nakasuka, University of Tokyo, Department of Aeronautics and Astronautics, 7-3-1, Hongo, Bunkyo-ku, Tokyo, 113-8656, Japan

1999-191: APPLICATION OF DC ARCJET FOR LOW EARTH ORBIT SPACECRAFT; Yoshinori Kunii, Space Systems Department, Mitsubishi Electric Corporation, 325 Kamimachiya, Kamakura, 247-8520, Japan; Kyoichiro Toki, The Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, 229-8510, Japan

1999-192: PULSED PLASMA THRUSTERS FOR SPACECRAFT ATTITUDE AND ORBIT CONTROL SYSTEM; N. N. Antropov, G. A. Diakonov, V. Kim, G. A. Popov, and A. I. Pokryshkin, Research Institute of Applied Mechanics and Electrodynamics, 4, Volokolamskoye shosse, Moscow, 125810, Russia; M. N. Kazeev, Russian Research Centre “Kurchatov Institute”, 1, Kurchatov sq., Moscow, 123182, Russia; and V. P. Khodnenko, All-Russian Research Institute of Electromechanics, 10100, P.O. Box 496, Moscow, Russia

1999-194: EVALUATION OF ELECTRODYNAMIC TETHER PROPULSION TO OTV; Masaya Kozakai and Haruki Takegahara, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino-shi, Tokyo 191-0065, Japan; Yoshiki Yamagiwa and Ryosuke Tuyuki, Shizuoka University, 3-5-1, Johoku, Hamamatsu-shi, Shizuoka 432-8561, Japan; Ryoichiro Yasumitsu, University of Tokyo, 7-3-1, Hongo, Bunko-ku, Tokyo 113-8654, Japan; Atsushi Nakajima, National Aerospace Laboratory, 7-44-1, Jindaiji Higashi-machi, Chofu, Tokyo 182-8522, Japan

1999-195: NON-CHEMICAL PROPULSION ABILITIES FOR NEAR-EARTH MISSIONS; V. A. Nevrovsky, Moscow State University of Aircraft Technology, Orshanskaya str. 3, 121552 Moscow, Russia

1999-196: NITRATING BY MPD THRUSTER – IS THE ECOLOGICAL CLEAN ALTERNATIVE TO CHEMICAL-THERMAL METHODS OF STRENGTHENING; Nikolay V. Bilan, Andriy V. Loyan, Sergey V. Muchin, and Oleg P. Rubalov, STC SPE “KhAI”, 17, Chkalova st., 310070, Kharkov, Ukraine

1999-197: DEVELOPMENT OF AN ELECTROMAGNETIC ACCELERATION PLASMA GENERATOR FOR ZIRCONIA AND TITANIUM NITRIDE COATINGS; Tetsuji Shibata, Hirokazu Tahara, Toshiaki Yasui, Yoichi Kagaya, and Takao Yoshikawa, Division of Mechanical Science, Department of Systems and Human Science, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

1999-198: HIGH TEMPERATURE PLASMA FURNACE USING GAS TUNNEL TYPE PLASMA JET AND ITSIAPPLICATION TO SURFACE MODICIFICATION; Akira Kobayashi, Joining and Welding Research Institute, Osaka University, 11-1 Mihogaoka, Ibaraki, Osaka 567-0047, Japan

1999-199: DEVELOPMENT OF 30-CM LONG LINEAR SPUTTERING SOURCE USING ECR DISCHARGE; Toshiaki Yasui, Tomohiro Matsumoto, Hirokazu Tahara and Takao Yoshikawa, Division of Mechanical Engineering, Department of Systems and Human Science, Graduate School of Engineering Science, Osaka University, 1-3 Machikaneyama, Toyonaka, Osaka 560-8531, Japan

1999-201: EFFECTS OF ADDITION OF HYDROGEN TO NITROGEN PLASMA DURING NITRIDING OF TITANIUM AND SACM645 STEEL USING SUPERSONIC EXPANDING PLASMA JETS; Y. Ando, S. Tobe, H. Tahara, and T. Yoshikawa, Ashikaga Institute of Technology, 268-1 Omae, Ashikaga, Tochigi 326-8558, Japan; Osaka University, 1-3 Machikaneyama, Toyonaka, Osaka, 560-8531, Japan

1999-202: DEVELOPMENT OF LARGE SIZE ION SOURCE FOR ION SHOWER DOPING; H. Kuwabara, I. Nakamoto, Y. Kawaskai, Electric System Development Department Mechatronics Development Center, Ishikawajima-Harima Heavy Industries Co. Ltd., Japan, 1-15, Toyosu 3-Chome, Koto-ku, Tokyo 135-8732, Japan

1999-203: A STUDY OF PULSED PLASMA ACCELERATOR WITH METAL PROPELLANT FOR SPACE AND TECHNOLOGY APPLICATION; Leonid N. Lesnevsky and Vladimir N. Tyurin, Moscow State Aviation Institute (MAI), 4 Volokolamskoye shosse, Moscow, 125871, Russia

1999-205: QUANTITATIVE RADIATION MEASUREMENTS OF THE PULSED PLASMA MICROTHRUSTER; Tomokazu Umeki and Peter J. Turchi, The Ohio State University, Columbus, Ohio, USA

1999-206: VISUALIZATION OF CURRENT SHEET CANTING IN A PULSED PLASMA ACCELERATOR; T. E. Markusic and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey 08544

1999-207: PERFORMANCE STUDY OF HIGH POWER ABLATIVE PULSED PLASMA THRUSTER; Y. A. Alexeev and M. N. Kazeev, Institute of Nuclear Fusion of RRC “Kurchatov Institute”, 1. Pl. Kurchatova, Moscow, 123182, Russia

1999-208: AN ACCURATE CHARACTERISTICS-SPLITTING SCHEME FOR NUMERICAL SOLUTION OF MHD EQUATIONS; K. Sankaran and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey 08544

1999-209: COMPARING THE PERFORMANCE OF CO-AXIAL AND PARALLEL-PLATE GAS-FED PPTS; J. K. Ziemer and E. Y. Choueiri, MAE Dept., Princeton University, Princeton, New Jersey 08544; D. Birx, Science Research Laboratory Inc., Sommerville, MA 02143

1999-210: DESIGN OPERATION, AND INVESTIGATION OF AN INDUCTIVELY-DRIVEN, COAXIAL PULSED PLASMA THRUSTER; H. Kamhawi, P. J. Turchi, I. G. Mikellides, and P. G. Mikellides, The Ohio State University, Columbus, Ohio USA

1999-211: OPTIMIZATION OF PULSED PLASMA THRUSTERS IN RECTANGULAR AND COAXIAL GEOMETRIES; I. G. Mikellides and P. J. Turchi, The Ohio State University, Columbus, Ohio, USA

1999-213: PARTICULATE INTERACTION WITH PLASMA IN A PULSED PLASMA THRUSTER; Michael Keidar and Iain D. Boyd, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109, USA; Isak I. Beilis, Electrical Discharge and Plasma Laboratory, Tel Aviv University, P. O. B. 39040, Tel Aviv 69978, Israel

1999-214: A MODEL OF AN ELECTRICAL DISCHARGE IN A CO-AXIAL PULSED PLASMA THRUSTER; Michael Keidar and Iain D. Boyd, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109, USA; Isak I. Beilis, Electrical Discharge and Plasma Laboratory, Department of Interdisciplinary Studies, Fleischman Faculty of Engineering, Tel Aviv University, P. O. B. 39040, Tel Aviv 69978, Israel

1999-216: PLASMA AND FIELD RESPONSES TO HIGH POTENTIAL SYSTEM IN SPACE; Hideyuki Usui, Hiroshi Matsumoto, and Yoshiharu Omura, Radio Atmospheric Science Center, Kyoto University, Gokasho, Uji, Kyoto 611-0011, Japan

1999-217: COMPUTATION OF CURRENT TO A MOVING BARE TETHER; Tatsuo Onishi and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, Massachusetts, USA; David L. Cooke, Air Force Research Laboratory, Space Vehicle Directorate, Hanscom AFB, MA, USA

1999-218: HOLLOW-CATHODE PLASMA CONTACTING INSIGHTS GAINED FORM THE ELCTRODYNAMIC TETHHER MISSION; P. J. Wilbur and D. Burtner, Colorado State University, Fort Collins, Colorado 80523

1999-219: PERFORMANCE OF ELECTRODYNAMIC TETHER ORBIT TRANSFER SYSTEM WITH CONSIDERATION OF LIFETIME BY THE IMPACT OF DEBRIS; Yoshiki Yamagiwa, Yukitaka Sakata, and Tatsuya Hashimoto, Faculty of Engineering, Shizuoka University, 3-5-1, Johoku, Hamamatsu, Shizuoka, 432-8561, Japan

1999-220: SYSTEM CONSIDERATIONS OF ELECTRODYNAMIC-TETHER PROPULSION TECHNOLOGY AND FUTURE PLANS; Brian E. Gilchrist, Sven G. Bilen, and Nestor R. Voronka, Space Physics Research Laboratory, University of Michigan, Ann Arbor, MI 48109-2143; Les Johnson, NASA Marshall Space Flight Center, Huntsville, AL 35812; Enrico C. Lorenzini, Harvard-Smithsonian Center for Astrophysics, Cambridge, MA 02318

1999-221: COMPARISON BETWEEN PLASMA PLUME THEORETICAL MODELS AND EXPERIMENTAL DATA; A. G. Korsun, B. S. Borisov, E. M. Tverdokhlebova, and F. F. Gabdullin, Central Research Institute of Machine Building (TsNIIMASH), Korolev, Moscow Region, Russia

1999-222: THE REACTION YIELD OF GRAPHITE WITH HYPERTHERMAL ATOMIC OXYGEN IN A LOW EARTH ORBITAL SPACE ENVIRONMENT; Hiroshi Kinoshita and Masatake Umeno, Department of Material and Life Science, Graduate School of Engineering, Osaka University, 2-1 Yamada-oka, Suita, Osaka 565-0871, Japan; Masahito Tagawa and Nobuo Ohmae, Department of Mechanical Engineering, Faculty of Engineering, Kobe University, 1-1 Rokko-dai, Nada, Kobe 657-8501, Japan

1999-223: EXPERIMENTAL DETERMINATION OF SPUTTERING COEFFICIENTS ISP SOFTWARE: NUMERICAL CALCULATION OF MATERIAL EROSION; I. Jouin, V. Perrin, D. Borie (Alcatel Space Industries), V. Huchet (Teuchos PACA), S. Khartov, A. Nadiradze, I. Shkarban, A. Semenov, and A. Chirov. (Moscow Aviation Institute), Alcatel Space Industries – 100, Bd du Midi BP 99 -06156 Cannes – France

1999-224: GROUND EXPERIMENTS OF INTERACTION BETWEEN PLASMA FLOW AND NEGATIVELY BIASED OR CHARGED MATERIALS; Daiki Matsuyama, Hirokazu Tahara, Takashi Matsuda, Toshiaki Yasui, and Takao Yoshikawa, Division of Mechanical Science, Department of Systems and Human Science, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

1999-226: PLUME MEASUREMENT OF PLASMA PROPULSION SYSTEM; Taizou Noutsuka, Yoshiyuki Takao, Tomoya Hida, Yoshiki Yano, Gen Kantou, Kazuhiko Uemura, and Hideki Nakashima, Department of Advanced Energy Engineering Science, Kyushu University, 6-1 Kasuga-Kouen Kasuga, Fukuoka 816-8580, Japan

1999-227: ICRF WAVE PROPAGATION AND ABSORPTION IN A MICROWAVE DISCHARGE ION THRUSTER; Yoshitaka Mori, Yoshiyuki Takao and Hideki Nakashima, Department of Advanced Energy Engineering Science, Kyushu University, 6-1 Kasuga-Kouen, Fukuoka 816-8580, Japan

1999-228: INTERACTION BETWEEN PLASMA PLUME OF ELECTRIC PROPULSION AND SPACECRAFT COMMUNICATION; Noriyoshi Onodera and Haruki Takegahara, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino-shi, Tokyo 191-0065, Japan; Ikko Funaki and Hitoshi Kuninaka, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihra-shi, Kanagawa 229-8510, Japan

1999-229: MATHEMATICAL MODELING OF INTERACTION OF THE ELECTRIC PROPULSION AND SPACECRAFT RADIOTEXNICAL SYSTEMS; I. P. Kozlov, Research Institute of Applied Mechanics and Electrodynamics (RIAME), 4 Volokolamskoye sh., Moscow, 125810

1999-230: OPTICAL MEASUREMENT OF CHARGING AND DISCHARGING PROCESSES ON INSULATOR SURFACE IN SIMULATED LOW EARTH ORBIT PLASMA ENVIRONMENT; Ko Shiraishi, Mengu Cho, and Masayuki Hikita, Department of Electrical Engineering, Kyushu Institute of Technology, Tobata-ku, Kitakyushu, Japan 804-8550

1999-232: CONTAMINATION SENSOR FOR ELECTRIC PROPULSION AND SOLID ROCKET MOTOR; Kazutaka Nishiyama, Ikkoh Funaki, and Hitoshi Kuninaka, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

1999-233: ISAS HIGH ENTHALPY FLOW FACILITY FOR THERMAL PROTECTION MATERIAL TESTS; Tetsuya Yamada, Naohiro Suzuki, and Yoshifumi Inatani, Division for Space Propulsion Systems, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

1999-235: EXPERIMENTAL ANALYSIS OF A SOLID PROPELLANT MPD THRUSTER WITH DIFFERENT ANODE RADII; Giorgio Paccani and Luigi Petrucci, Universita degli Studi di Roma “La Sapienza”, Rome, Italy; and William D. Deininger, Ball Aerospace & Technologies Corp., Boulder, CO, USA

1999-238: PRELIMINARY DEVELOPMENT STATUS OF THE IUA’S P4S-1 ABLATIVE PULSED PLASMA THRUSTER; Hector H. Brito, Roque O. De Alessandro, and Carlos A. Dominguez, Centro de Investigaciones Aplicadas, Instituto Universitario Aeronautico, Ruta 20, Km 6.5, 5022 Cordoba, Argentina

1999-241: MICROWAVE TELEMETRY BREAKDOWN CAUSED BY ROCKET PLUME; Takashi Abe, Kazuhisa Fujita, Hiroyuki Ogawa, and Ikkoh Funaki, The Institute of Space and Astronautical Science, Kanagawa 229-8510, Japan

1999-242: A MODEL FOR THE CHARACTERIATION OF PLASMA INSIDE THE STATIONARY PLASMA THRUSTER; K Makowski, Z. Peradynski, and S. Barral, Institute of Fundamental Technological Research, Polish Academy of Sciences, Swietokrzyska 21, 00-049 Warsaw, Poland; M. Dudeck, Laboratoire d’Aerothermique du CNRS, 1C, avenue de la Recherche Scientifique, 45071 Orleans Cedex 2, France

1999-244: DESIGN AND MANUFACTURE OF THE ETS VIII COMPOSITE OVERWRAPPED XENON PRESSURE VESSEL; Walter H. Tam, Pressure Systems, Inc.; Mark D. Drey and Arthur C. Jackson, Programmed Composites, Inc.; Eiji Nishida and Yukikazu Kasai, Mitsubishi Electric Corporation; and Akio Tsujihata and Kenichi Kajiwara, National Space Development Agency of Japan

1999-245: PARAMETRIC INVESTIGATIONS OF SEGMENTED ELECTRODE HALL THRUSTER; Y. Raitses, L. A. Dorf, A. A. Litvak, and N. J. Fisch, Princeton Plasma Physics Laboratory, Princeton University, Princeton, NJ 08540

1999 FILE DIRECTORY (add "199" to begining of file name)

9001.pdf  14:58  1.2M

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9245.pdf  11:16  1.4M

2001 INDEX

2001-001: NASA’S NEW EMPHASIS ON IN-SPACE PROPULSION TECHNOLOGY RESEARCH; Les Johnson, Advanced Space Transportation Program/TD15, Marshall Space Flight Center, Marshall Space Flight Center, Alabama 35812, USA

2001-002: NASA’S ELECTRIC PROPULSION PROGRAM; John W. Dunning Jr., Scott Benson, Steven Oleson, National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field, Cleveland, Ohio USA 44135

2001-003: OVERVIEW OF THE USAF ELECTRIC PROPULSION PROGRAM; Ronald A. Spores and Gregory G. Spanjers, Air Force Research Laboratory Propulsion Directorate, Edwards AFB, CA 93524; Mitat Birkan, Air Force Office of Scientific Research, Bolling AFB, Washington, DC 20332; and Major Timothy J. Lawrence, European Office of Aerospace Research and Development, London, NW1 5TH UK

2001-004: AN OVERVIEW OF ELECTRIC AND ADVANCED PROPULSION ACTIVITIES IN JAPAN; Haruki Takegahara, Tokyo Metropolitan Institute of Technology, Dept. of Aerospace Eng., Asahigaoka 6, Hino, Tokyo 191-0065, Japan

2001-005: ELECTRIC PROPULSION ACTIVITY IN RUSSIA; Vladimir Kim and Garri Popov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), 5, Leningradskoye shosse, P.O. Box 43, Moscow 125080, Russa; Boris Arkhipov and Vyacheslav Murashko, “Fakel” Design Bureau, Kaliningrad, Russia; Oleg Gorshkov and Anatoly Koroteyev, Keldysh Research Center; Valery Garkusha, Alexander Semenkin, and Sergei Tverdokhlebov, Tsentral Institute of Machinebuilding, Moscow, Russia

2001-006: EUROPEAN ELECTRIC PROPULSION ACTIVITIES AND PROGRAMMES; G. Saccoccia, ESA Technical and Operational Support Directorate, ESTEC, Noordwijk, The Netherlands

2001-007: AN OVERVIEW OF ELECTRIC PROPULSION ACTIVITIES IN CHINA; Xiaolu Kang, Zhaoling Wang and Nanhao Wang, Shanghai Spaceflight Power Machinery Institute, Shanghai, P. R. China, 200233; Anjie Li, Center for Space Science and Applied Research of CAS (CSSAR); Guofu Wu, Lanzhou Institute of Physics (LIP); Gengwang Mao, Northwestern Polytechnical University (NPU); Haibin Tang, Beijing University of Aeronautics and Astronautics (BUAA); and Wenhuua Zhao, Tsinghua University

2001-008: AN OVERVIEW OF THE CNES ELECTRIC PROPULSION PROGRAM; Anne Cadiou, Cécile Gelas, Franck Darnon, Laurent Jolivet, and Nicolas Pillet, CNES, 18 Avenue Edouard Belin, 31401 Toulouse Cedex 4

2001-010: THE DEVELOPMENT AND QUALIFICATION OF A 4.5 KW HALL THRUSTER PROPULSION SYSTEM FOR GEO SATELLITE APPLICATIONS; Jack Fisher, Alfred Wilson, David King, Steve Meyer, Carl Engelbrecht and Kristi de Grys, General Dynamics Space Propulsion Systems; 1141 Willows Road N.E., P.O. Box 97009, Redmond, WA 9807309709; Lance Werthman, Lockheed Martin Space Systems Company, 1111 Lockheed Martin Way, Sunnyvale, CA 94089

2001-011: DEVELOPMENT AND TESTING OF A 4500 WATT FLIGHT TYPE HALL THRUSTER AND CATHODE; Kristi de Grys, Nicole Meckel, George Callis, Doug Greisen, Andrew Hoskins, David King, and Fred Wilson, General Dynamics Space Propulsion Systems, 11441 Willows Road N.E., P.O. Box 97009; Lance Werthman, and Vadim Khaymas, Lockheed Martin Space Systems Company, 1111 Lockheed Martin Way, Sunnyvale, CA 94089

2001-012: PERFECTING OF THE TECHNOLOGICAL SOLUTIONS AT MANUFACTURING OF A ET MT 12; A.N. Tarasov, V. M. Murashko, and A. G. Niatin, OKb “Fakel”, Kaliningrad, Russian Federation

2001-013: OPERATING ENVELOPES OF THRUSTERS WITH ANODE LAYER; A. V. Semenkin, S. O. Tverdokhlebov, V. I. Garkusha, A. V. Kochergin, G. O. Chislov, B. V. Shumkin, A. V. Solodukhin, and L. E. Zakharenkov

2001-015: A CONCEPT OF DEVELOPMENT OF ELECTRIC THRUSTERS WITH THRUST VECTOR CONTROL; Valery Petrosov, Keldysh Research Center, Moscow, Russia

2001-017: CHARACTERIZATION OF THE PLASMA IN A HALL THRUSTER; E. Ahedo, P. Martínez Cerezo, and J. M. Gallardo, E.T.S.I. Aeronáuticos, Univ. Politécnica, 28040 Madrid, Spain; M. Martínez-Sánchez, Dep. Of Aeronautics & Astronautics, M.I.T., Cambridge, MA 02139

2001-018: AZIMUTHAL NON-UNIFORMITIES IN ACCELERATORS WITH CLOSED ELECTRON DRIFT; Vladimir Baranov, Yuri Nazarenko, and Valery Petrosov, Keldysh Research Center, Moscow, Russia

2001-019: DECONVOLUTION OF AXIAL VELOCITY DISTRIBUTIONS FROM HALL THRUSTER LIF SPECTRA; Timothy B. Smith, Daniel A. Herman, Alec D. Gallimore, and R. Paul Drake, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Rm. B107, 1919 Green Rd., Ann Arbor, MI 48105

2001-020: A COMPARISON OF NUDE AND COLLIMATED FARADAY PROBES FOR USE WITH HALL THRUSTERS; Richard R. Hofer, Mitchell L. R. Walker, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, University of Michigan, College of Engineering, Ann Arbor, MI 48109, USA

2001-021: DETERMINATION OF THE IONIZATION AND ACCELERATION ZONES IN A STATIONARY PLASMA THRUSTER; N. Dorval, J. Bonnet, J. P. Marque, and E. Rosencher, ONERA/DMPH, Chemin de la Huniére, 91761 Palaiseau (France); S. Chable and F. Rogier, ONERA/DTIM, 2 avenue E. Belin, 31055, Toulouse (France); and P. Lasgorceix, LAMO, 3 avenue de la Recherche Scientifique, 45071, Orléans Cedex 2 (France)

2001-022: A 1-D TIME-DEPENDENT MODEL OF A HALL THRUSTER WITH SIDE WALLS; Peter S. Rostler, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760

2001-023: A NUMERICAL STUDY OF THE EFFECT OF CHANNEL INSULATOR DISCONTINUITY ON HALL THRUSTER DISCHARGE; Summer Locke and Uri Shumlak, Department of Aeronautics and Astronautics, University of Washington, BOX 352250, Seattle, WA 98145-2400; J. M. Fife, Electric Propulsion Group, Air Force Research Laboratory, AFRL/PRRS, 1 Ara Road, Edwards AFB, CA 93524-7190

2001-024: A STATIONARY HYDRODYNAMIC MODEL FOR HALL THRUSTER; Vasily Lobzin, Institute of Terrestrial Magnetism, Ionosphere and Radio Wave Propagation, Russian Academy of Sciences, Troitsk, Moscow region, Russia, 142190; Nicolas Gascon, Thermosciences Division, Mechanical Engineering Department, Stanford University, Stanford, California 94305-3032; Vladimir Krasnoselskikh, Laboratoire de Physique et Chimie de l’Environnement, Centre National de la Recherche Scientifique, 3A, Avenue de la Recherche Scientifique, 45071 Orléans CEDEX 2; Michael Dudeck, Laboratoire d’ Aérothermique, Centre National de la Recherche Scientifique, 1C, Avenue de la Recherche Scientifique, 45071 Orléans CEDEX 2

2001-025: ABOUT THE DOUBLE-HUMPED ELECTRON DISTRIBUTION FUNCTION IN HALL THRUSTERS; S. Barral, Z. Peradzynski,  and K. Makowski, Institute of Fundamental Technological Research, Swietokrzyska 21, 00049 Warsaw, Polad; M. Dudeck, CNRS Laboratoire d’ Aerothermique, 1c avenue de la Recherche Scientifique, 45071 Orleans, France

2001-026: ANALYSIS OF THE STEADY-STATE AXIAL FLOW IN THE HALL THRUSTER; Avi Cohen-Zur and Alon Gany, Faculty of Aerospace Engineering, Technion – Israel Institute of Technology, Haifa 32000, Israel; Amnon Fruchtman, Holon Academic Institute of Technology, P. O. Box 305, Holon 58102, Israel; Joseph Ashkenazy, Propulsion Physics Laboratory, Soreq NRC, Yavne 81800, Israel

2001-027: NUMBERICAL STUDY OF THE CURRENT-VOLTAGE CHARACTERISTIC OF HALL THRUSTERS; S. Barral, K. Makowski, Institute of Fundamental Technological Research – PAS, Swietokrzyska 21, 00-049 Warsaw, Poland; Z. Peradzynski, Dept. of Mathematics, Informatic and Mechanics of Warsaw University, Banacha 2, 00-097 Warsaw, Poland; N. Gascon, Stanford University, Mechanical Engineering Department, Stanford – California, 94305-3032, USA; M. Dudeck, CNRS Laboratoire d’Aeothermique, 1c avenue de la Recherche Scientifique, 45071 Orleans, France

2001-028: PARAMETRIC STUDY OF A STATIONARY PLASMA THRUSTER USING A TWO-DIMENSIONAL HYBRID MODEL; G.J.M. Hagelaar, J. Bareilles, L. Garrigues, and J. P. Boeuf, CPAT, Batiment 3R2, Université Paul Sabatier, 118 Route de Narbonne, 31062 Toulouse, France

2001-029: MAGNETIC SYSTEM FOR HALL THRUSTERS EVALUATION AND DESIGN; V. I. Garkusha and A. V. Semenkin, Central Research Institute of Machine Building, Korolev, Russia

2001-030: EXPERIMENTAL INVESTIGATION OF A HALL THRUSTER INTERNAL MAGNETIC FIELD TOPOGRAPHY; Peter Y. Peterson, Alec D. Gallimore, and James M. Haas, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, The University of Michigan, College of Engineering, Ann Arbor, MI 48109 USA

2001-032: PARAMETERS OF D-80 ANODE LAYER THRUSTER IN ONE- AND TWO- STAGE OPERATION MODES; A. E. Solodukhin, A. V. Semenkin, S. O. Tverdohlebov and A. V. Kochergin, Central Research Institute of Machine Building, Korolev, Moscow Reg., Russia

2001-035: PERFORMANCE OF A HIGH SPECIFIC IMPLUSE HALL THRUSTER; Bruce Pote and Rachel Tedrake, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760-1023

2001-036: A HIGH SPECIFIC IMPLUSE TWO-STAGE HALL THRUSTER WITH PLASMA LENS FOCUSING; Richard R. Hofer, Peter Y. Peterson, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, University of Michigan, College of Engineering, Ann Arbor, MI 48109, USA; Robert S. Jankovsky, NASA Glenn Research Center, Cleveland, OH 44135, USA

2001-037: PIC SIMULATION OF HIGH SPECIFIC IMPLUSE HALL EFFECT THRUSTER; Vincent Blateau, Manuel Martinez-Sanchez, Oleg Batishchev, and James Szabo, Massachusetts Institute of Technology, 77 Massachusetts Avenue, Cambridge, MA 02139

2001-038: PARAMETRIC INVESTIGATIONS OF MINIATURIZED CYLINDRICAL AND ANNULAR HALL THRUSTERS; A. Smirnov, Y. Raitses, and N. J. Fisch, Princeton University Plasma Physics Laboratory, P.O. Box 451, Princeton, NJ 08543

2001-039: LINEAR GEOMETRY HALL THRUSTER WITH BORON NITRIDE AND DIAMOND WALLS; Nathan B. Meezan, Nicolas Gascon, and Mark A. Cappelli, Thermosciences Division, Mechanical Engineering Department, Stanford University, Stanford, CA 94305-3032

2001-041: STUDY OF LOW POWER TAL CHARACTERISTICS; L. Zakharenkov, G. Chislov, and A. Semenkin, Central Research Institute of Machine Building (TsNIIMASH), Russia 141070, Korolev City, Moscow region, Pionerskaya str., 4; T. Lawrence, European Office of Aerospace Research and Development

2001-042: THRUST PERFORMANCE AND PLASMA CHARACTERISTICS OF LOW POWER HALL THRUSTERS; Hirokazu Tahara, Daisuke Goto, Toshiaki Yasui, and Takao Yoshikawa, Division of Mechanical Science, Dept. of Systems, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

2001-044: HALL THRUSTER PLUME MEASUREMENTS ON-BOARD THE RUSSIAN EXPRESS SATELLITES; David Manzella, The University of Toledo, Toledo, OH 43606; Robert Jankovsky and Frederick Elliott, NASA John H. Glenn Research Center, Cleveland, OH 44135; Ioannis Mikellides and Gary Jongeward, Science Applications International Corporation, San Diego, CA 92121; and Doug Allen, Schafer Corporation, Dayton, OH 45431

2001-045: CHARACTERIZING VACUUM FACILITY BACKPRESSURE EFFECTS ON THE PERFORMANCE OF A HALL THRUSTER; Richard R. Hofer, Peter Y. Peterson, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, University of Michigan, College of Engineering, Ann Arbor, MI 48109, USA

2001-048: THE WEAR OF THE CHANNEL WALLS IN HALL THRUSTERS; Vladimir Baranov, Yuri Nazarenko, and Valery Petrosov, Keldysh Research Center, Moscow, Russia

2001-049: DEVELOPMENT OF A FINITE ELEMENT BASED HALL THRUSTER MODEL FOR SPUTTER YIELD PREDICTION; Subrata Roy and Birendra Pandey, Computational Plasma Dynamics Research Laboratory, Kettering University, 1700 West Third Avenue, Flint, MI 48504

2001-051: A KINETIC STUDY OF ELECTRON-WALL COLLISIONS IN A HALL THRUSTER; Nathan B. Meezan and Mark A. Cappelli, Stanford University, Department of Mechanical Engineering, Stanford, CA 94305-3032

2001-053: OPTICAL EMISSION OF A HALL THRUSTER PLUME IN SPACE CONDITION; Georgie Karabadzhak, Flur Gabdullin, Anatoli Korsun, Yuri Plastinin and Ekaterina Tverdokhlebova, Central Research Institute of Machine-Building (TSNIIMASH); Pionerskaya Street, 4, Korolev, Moscow region, Russia, 141070

2001-054: SIMULATIONS FOR A SHUTTLE-BASED HALL THRUSTER PLUME EXPERIMENT; Shannon Y. Cheng and Manuel Martinez-Sanchez, Space Propulsion Laboratory, Massachusetts Institute of Technology, Cambridge, MA 02139

2001-055: INFLUENCE OF DISCHARGE OSCILLATION ON HALL THRUSTER PERFORMANCE; Naoji Yamamoto, Takafumi Nakagawa, Kimiya Komurasaki, and Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, Hongo 7-3-1, Bunkyo-ku, Tokyo, 113-8656, Japan

2001-056: LOW FREQUENCY PLASMA WAVE DISPERSION AND PROPAGATION IN HALL THRUSTERS; Nicolas Gascon, Nathan B. Meezan, and Mark A. Cappelli, Thermosciences Division, Mechanical Engineering Department, Stanford University, Stanford, CA 94305-3032

2001-057: METHODS OF CONTROLLING LOW-FREQUENCY OSCILLATION IN A HALL THRUSTER; Takeshi Furukawa, Takeshi Miyasaka and Toshi Fujiwara, Department of Aerospace Engineering, Nagoya University, Furo, Chikusa-ku Nagoya 464-8603, Japan

2001-058: ANALYSIS OF COMMUNICATION SIGNAL MODULATION INDUCED BY PERIODIC HALL THRUSTER PLUME INSTABILITIES; Joseph T. Loane and J. William Meyer, Lockheed Martin Space Systems Company, Sunnyvale, CA 94089; Gary A. Hallock and James C. Wiley, The University of Texas, Austin, TX 78712

2001-059: INSIGHTS ON PHYSICS OF HALL THRUSTERS THROUGH FAST CURRENT INTERRUPTIONS AND DISCHARGE TRANSIENTS; Mathieu Prioul and André Bouchoule, GREMI Université d’Orléans, BP 6744, 45 067 Orléans, France; Stéphanie Roche, Lionel Magne, Daniel Pagnon and Michael Touzeau, LPGP, Université Paris XI ORSAY, 91 405 Orsay, France; Pascal Lasgorceix, Laboratoire Aérothermique, CNRS, 45 067 Orléans, France

2001-060: MEASUREMENTS OF PLASMA POTENTIAL DISTRIBUTION IN SEGMENTED ELECTRODE HALL THRUSTER; Y. Raitses, D. Staack, and N. J. Fisch, Princeton University Plasma Physics Laboratory, P.O. Box 451, Princeton, NJ 08543

2001-062: ANALYSES OF THE PLASMA FLOW AND PRESHEATH STRUCTURE IN HALL THRUSTERS; Michael Keidar and Iain D. Boyd, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109; Isak I. Beilis, Electrical Discharge and Plasma Laboratory, Tel Aviv University, Tel Aviv 69978, Israel

2001-063: PRELIMINARY STUDY OF ARCJET NEUTRALIZATION OF HALL THRUSTER CLUSTERS; Quentin E. Walker and Mark A. Cappelli, Thermosciences Division, Mechanical Engineering Department, Stanford University, Building 520, Stanford, CA 94309-3032; William A. Hargus, Jr., ARFL, Edwards Air Force Base, Building 8895, Edwards, CA 93524; John Schilling, W.E. Research LLC, Rosemond, CA 93560

2001-064: THE RESULTS OF TESTING AND EFFECTIVENESS OF THE KR-XE MIXTURE APPLICATION IN SPT; B. A. Arkhipov, A. I. Koryakin, V. M. Murashko, A. N. Nesterenko, and I. A. Khoromsky, EDB “Fakel”, Moskovsky pr. 181, Kaliningrad, Russia; V. Kim, V. I. Kozlov, G. A. Popov, and A. I. Skrylnikov, RIAME, Moscow Volokolamskoye sh., 4, Russia

2001-065: INVESTIGATION OF SPT PERFORMANCE AND PARTICULARITIES OF IT’S OPERATION WITH KR AND KR/XE MIXTURES; Vladimir Kim, Garry Popov, Vyacheslav Kozlov, Alexander Skrylnikov, and Dmitry Grdlichko, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI); 5, Leningradskoye shosse, post box 43, Moscow, 125080, Russia

2001-066: HALL THRUSTERS OPERATING IN PULSED MODE; Vlad Hruby, Bruce Pote, Manuel Gamero-Castaño, George Kolencik, Larry Byrne, Rachel Tedrake and Mary Delishatsios, Buseck Co. Inc., 11 Tech Circle, Natick, MA 01760-1023

2001-068: THE MAIN REGULARITY OF AN IGNITION IN A SPT; Sergiy A. Oghienko and Andriy A. Rybakov, National Aerospace University by him N. E. Joukovski “The Kharkov aviation institute”, 17, Chkalova St. Kharkov, 61070, Ukraine

2001-069: PRELIMINARY STUDY OF AN ECR DISCHARGE HALL THRUSTER; Pedro Molina-Morales, Hitoshi Kuninaka, and Kyoichiro Toki, Institute of Space and Astronautical Science (ISAS), 3-1-1 Yoshinodai, Sagamihara, Kanagawa, 229-8510, Japan; Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Toyko 113-8656, Japan

2001-070: DEVELOPMENT OF ELECTRIC PROPULSION STANDARDS – CURRENT STATUS AND FURTHER ACTIVITY; A Semenkin, Central Research Institute of Machine Building (TsNIIMASH); V. Kim, Research Institute of Applied Mechanic and Electro-dynamic (RIAME); O. Gorshkov, Keldysh Research Center; R. Jankovsky, NASA Glenn Research Center

2001-072: THERMAL CHARACTERIZATION AND MODELING OF A LOW-POWER LABORATORY MODEL TAL; John Walter and James Dickens, Department of Electrical and Computer Engineering, Texas Tech University, MS 3102, Lubbock, Texas 79409

2001-073: INVESTIGATION OF THE BORON NITRIDE BASED CERAMICS SPUTTERING YIELD UNDER IT’S BOMBARDMENT BY XE AND KR IONS; Vladmir Kim, Vyacheslav Kozlov, Alexander Semenov, and Igor Shkarban, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), 5, Leningradskoye shosse, post box 43, Moscow, 125080, Russia

2001-074: OVERVIEW OF HALL CURRENT THRUSTER INTEGRATION ACTIVITIES OF LOCKHEED MARTIN SPACE SYSTEMS COMPANY; Vadim Khayms, Keith Kannenberg, Bill Meyer, and Lance Werthman, Lockheed Martin Space Systems Company, 1111 Lockheed Martin Way, Sunnyvale, CA 94086

2001-075: DEMONSTRATION OF THE NSTAR ION PROPULSION SYSTEM ON THE DEEP SPACE ONE MISSION; J. E. Polk, D. Brinza R. Y. Kakuda, J. R. Brophy, I. Katz and J. R. Anderson, Jet Propulsion Laboratory, M/S 125-109, 4800 Oak Grove Drive, Pasadena, CA 91109; V. K. Rawlin, M. J. Patterson, J. Sovey and J. Hamley, NASA Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH 44130

2001-076: LONG DURATION GROUND TESTING OF THE DEEP SPACE 1 FLIGHT SPARE ION THRUSTER – THE FIRST 15600 HOURS; John R. Anderson, Keith D. Goodfellow, and James E. Polk, Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109; Vincent K. Rawlin and James S. Sovey, NASA Glenn Research Center, 21000 Brook Park Road, Cleveland, Ohio 44135

2001-081: IMPROVING THE TOTAL IMPULSE CAPABILITY OF THE NSTAR ION THRUSTER WITH THICK-ACCELERATOR-GRID ION OPTICS; George C. Soulas, NASA Glenn Research Center, M.S. 301-3, 21000 Brookpark Road, Cleveland, OH 44135, U.S.A.

2001-082: RESULTS OF THE 15000 HOURS LIFETIME TEST FOR THE RITA ION PROPULSION ON ESA’S ARTEMIS SATELLITE; Rainer Killinger, Helmut Bassner, Ralf Kukies, and Hans Leiter, Astrium GmbH, Post Box 80 11 69, D-816633 Müchen, Germany

2001-083: RESULTS OF A 35-CM XENON ION THRUSTER ENDURANCE TEST; Shoji Kitamura, National Aerospace Laboratory of Japan, 7-44-1 Jindaijihigashi-Machi, Chofu, Tokyo 182-8522, Japan; Yukio Hayakawa and Katsuhiro Miyazaki, National Aerospace Laboratory of Japan, 7-44-1 Jindaijihigashi-Machi, Chofu, Tokyo, 182-8522, Japan; Ken’ichi Kajiwara, National Space Development Agency of Japan, 2-1-1 Sengen, Tsukuba, Ibaraki 305-8505, Japan; Hideki Yoshida, Yuuko Yamamoto, and Kouseki Akai, Toshiba Corporation, 4-1 Ukishima-Cho, Kawasaki-Ku, Kawasaki, Kanagawa, 210-0862, Japan

2001-084: A GRID LIFETIME MODEL FOR A 3-GRID ION ENGINE; Masakatsu Nakano, Japan Science and Technology Corporation, Kakuda Space Propulsion Laboratory, National Aerospace Laboratory, 1 Kogenesawa, Kimigaya, Kakuda-shi, Miyagi, 981-1525, Japan

2001-085: THREE-DIMENSIONAL PARTICLE SIMULATIONS OF NSTAR ION OPTICS; Joseph Wang, Dept. Aerospace & Ocean Engineering, Virginia Polytechnic Institute and State University; James Polk, John Brophy, and Ira Katz, Jet Propulsion Laboratory, California Institute of Technology

2001-086: RETENTION OF SPUTTERED MOLYBDENUM ON ION ENGINE DISCHARGE CHAMBER SURFACES; James S. Sovey, Joyce A. Dever, and John L. Power, National Aeronautics and Space Administration, Glenn Research Center, MS 301-3, 21000 Brookpark Road, Cleveland, Ohio 44135

2001-088: ION PROPULSION DEVELOPMENT ACTIVITIES AT THE NASA GLENN RESEARCH CENTER; Michael J. Patterson, Matthew T. Domonkos, John E. Foster, Thomas W. Haag, Maris A. Mantenieks, Luis R. Pinero, Vincent K. Rawlin, George C. Soulas, and James S. Sovey, National Aeronautics and Space Administration, Glenn Research Center, MS 301-3, 21000 Brookpark Road, Cleveland, Ohio 44135; Christian Carpenter, Scott D. Kovaleski, and Robert F. Roman, QSS Group, Inc., Cleveland, Ohio; George Williams, Ohio Aerospace Institute, Cleveland, Ohio

2001-089: NEXT-GENERATION 5/10 KW ION PROPULSION DEVELOPMENT STATUS; Michael J. Patterson, John E. Foster, Thomas Haag, Luis Pinero, Vincent K. Rawlin, George C. Soulas, and Michelle S. Doehne, National Aeronautics and Space Administration, Glenn Research Center, MS 301-3, 21000 Brookpark Road, Cleveland, Ohio 44135; Robert F. Roman, QSS Group Inc., Cleveland, Ohio

2001-090:  DESIGN AND PERFORMANCE OF 40 CM ION OPTICS; George C. Soulas, NASA Glenn Research Center, M.S. 301-3, 21000 Brookpark Road, Cleveland, OH 44135, U.S.A.

2001-091: ELECTRON BACKSTREAMING MITIGATION VIA A MAGNETIC GRID; John E. Foster, Robert F. Roman, George C. Soulas, and Michael J. Patterson, National Aeronautics and Space Administration, Glenn Research Center, MS 301-3, 21000 Brookpark Road, Cleveland, Ohio, 44135

2001-092: PERFORMANCE EVALUATION OF TITANIUM ION OPTICS FOR THE NASA 30 CM ION THRUSTER; George C. Soulas, NASA Glenn Research Center, M.S. 301-3, 21000 Brookpark Road, Cleveland, OH 44135, U.S.A.

2001-094: CARBON-BASED ION OPTICS DEVELOPMENT AT NASA GRC; Thomas Haag, Michael Patterson, Vince Rawlin, and George Soulas, National Aeronautics and Space Administration, Glenn Research Center, Cleveland, OH 44135

2001-095: LIGHTWEIGHT ION ENGINE BODY; Y. Robert Yamaki and Timothy R. Knowles, Energy Science Laboratories, Inc., 6888 Nancy Ridge Drive, San Diego, CA 92121; Keith D. Goodfellow, Jet Propulsion Laboratory, California Institute of Technology, MS 125-109, 4800 Oak Grove Drive, Pasadena, CA 91106

2001-096: STATUS OF ION ENGINE DEVELOPMENT FOR HIGH POWER, HIGH SPECIFIC IMPULSE MISSIONS; Vincent K. Rawlin and Luis R. Piñero, National Aeronautics and Space Administration, Glenn Research Center MS 301-3, 21000 Brookpark Rd., Cleveland, OH 44135; George J. Williams, Ohio Aerospace Institute, NASA Glenn Group MS 301-3, 21000 Brookpark Rd., Cleveland, OH 44135; Robert F. Roman, QSS Group, Inc., Glenn Research Center MS 16-1, 21000 Brookpark Rd., Cleveland, OH 44135

2001-097: NUMERICAL ANALYSIS OF ION BEAM EXTRACTION PHENOMENA IN AN ION THRUSTER; Yasushi Okawa, Satellite Venture Business Laboratory, Kyushu Institute of Technology, 1-1, Sensuicho, Tobata, Kitakyushu, Fukuoka 804-8550, Japan; Haruki Takegahara, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino, Tokyo 191-0065, Japan; Takeshi Tachibana, Department of Mechanical Engineering, Kyushu Institute of Technology

2001-098: A STUDY OF HIGH SPECIFIC IMPULSE ION THRUSTER OPTICS; Paul J. Wilbur, Joshua Miller, and Cody Farnell, Department of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523; Vincent K. Rawlin, NASA Glenn Research Center, Cleveland, OH 44135

2001-099: NUMERICAL SIMULATION OF HIGH SPECIFIC IMPULSE ION THRUSTER OPTICS; Yoshinori Nakayama and Paul J. Wilbur, Department of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523

2001-100: NUMERICAL MODELING OFNEUTRAL AND CHARGED PARTICLES WITHIN A GRIDDED ION THRUSTER; M. Jugroot and J. K. Harvey, Department of Aeronautics, Imperial College of Science, Technology and Medicine, SW7 2BY London, United Kingdom

2001-101: PARTICLE SIMULATION FOR ION THRUSTER GRID DESIGN; Yasutaka Inanaga, Environmental Technology and System Department, Advanced Technology R&D Center, Mitsubishi Electric Corporation, 8-1-1, Tsukaguchihonmachi, Amagasaki, Hyogo 661-8861, Japan; Toshiyuki Ozaki, Space Engineering Department, Kamakura Works, Mitsubishi Electric Corporation, 325, Kamimachiya, Kamakura, Kanagawa 247-8520, Japan

2001-102: DEVELOPMENT STATUS OF 20 MN CLASS XENON ION THRUSTER FOR ETS-8; Toshiyuki Ozaki and Yoshifumi Gotoh, Space Engineering Department, Kamakura Works, Mitsubishi Electric Corporation, 325 Kamimachiya, Kamakura, Kanagawa 247-8520, Japan; Takashi Itoh, Engineering Test Satellite-VIII Project Team, Office of Satellite Systems, National Space Development Agency of Japan (NASDA), 2-1-1, Sengen, Tsukuba-shi, Ibaraki 305-8505, Japan; Ken-ichi Kajiwara, Satellite Systems Engineering Department, Office of Satellite Systems, NASDA, 2-1-1, Sengen, Tsukuba-shi, Ibaraki 305-8505, Japan

2001-103: 20MN-CLASS MICROWAVE DISCHARGE ION THRUSTER; Ikkoh Funaki, Institute of Engineering Mechanics and Systems, University of Tsukuba, Tsukuba, Ibaraki, 305-8573, Japan; Kazutaka Nishiyama, Hitoshi Kuninaka, Kyoichiro Toki, Yukio Shhimizu, and Hanya Toki, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2001-104: DEVELOPMENT OF THE RADIO FREQUENY ION THRUSTER RIT XT – A STATUS REPORT; Hans J. Leiter, Rainer Killinger, Helmut Bassner, Johann Müller, and Ralf Kukies, Astrium GmbH, Post Box 80 11 69, D-816633 Müchen, Germany

2001-105: DEVELOPMENT STEPS OF THE RF-ION THRUSTERS RIT; Helmut Bassner, Rainer Killinger, Hans Leiter, and Johann Müller, Astrium GmbH, Post Box 80 11 69, D-816633 Müchen, Germany

2001-106: A STUDY ON MICROWAVE DISCHARGE ION THRUSTER; Takashi Miyamoto, Kazuya Yamawaki, Hideto Ikeda, and Hideki Nakashima, Department of Advanced Energy Engineering Science, Kyushu University, Kasuga, Fukuoka 816-8580, Japan; Yoshiyuki Takao, Department of Computer and Control Enginerring, Oita National College of Technology, 1666 Maki, Oita 870-0152, Japan

2001-107: PERFORMANCE TEST OF VARIOUS DISCHARGE CHAMBER CONFIGURATIONS FOR ECR DISCHARGE ION THRUSTER; Haruya Toki and Hajime Fujita, Graduate School of Science and Technology Nihon University, 1-8-14 Kanda Surugadai, Chiyoda, Tokyo, 101-8308, Japan; Kazutaka Nishiyama, Hitoshi Kuninaka, and Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa, 229-8510, Japan; Ikkoh Funaki, Institute of Engineering and Systems Tsukuba University, 1-1-1 Tennodai, Tsukuba, Ibaraki, 305-8573, Japan

2001-108: HIGH PERFORMANCE, LOW POWER ION PROPULSION SYSTEM DESIGN CONCEPT; Nicole J. Meckel, Robert J. Kay, and Carl S. Engelbrecht, General Dynamics, Space Propulsion Systems, P.O. Box 97009; Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, The University of Michigan, Francois-Xavier Bagnoud Building, 1320 Beal Avenue, Ann Arbor, MI 48109-2140; James C. Dickens, Texas Tech University, Department of Electrical and Computer Engineering, Box 43102, Lubbock, TX 79409-3102; Michael J. Patterson, Power and On-Board Propulsion Technology Division, NASA Glenn Research Center, Mail Stop 301-3, Cleveland, OH 44135

2001-110: DSMC-PIC ANALYSIS OF A PLUME FROM A SMALL ION ENGINE; Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-8581, Japan; Toru Hyakutake, Department of Mechanical Engineering, Okayama University, Okayama 700-8530, Japan; Hitoshi Kuninaka and Kyoichiro Toki, Institute of Space and Astronautical Science, Sagamihara, Kanagawa 229-8510, Japan

2001-111: THE INFLUENCE OF CHARGE-EXCHANGE IONS ON THE BEAM DIVERGENCE OF AN ION THRUSTER; David H. Mundy and David G. Fearn, Space Department, QinetiQ, Farnborough, Hants, GU14 0LX, UK; Robert A. Bond, AEA Technology Space, Culham Science Centre, Abingdon, Oxon, OX14 3ED, UK

2001-112: MEASUREMENTS OF THE ELECTROMAGNETIC EMISSIONS FROM THE MUSES-C ION ENGINE SYSTEM; Kazutaka Nishiyama, Yukio Shimizu, Ikkoh Funaki, Hitoshi Kuninaka, Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa, Japan 2298510

2001-113: MOLECULAR DYNAMICS SIMULATION OF LOW-ENERGY SPUTTERING OF MOLYBDENUM WITH XENON IONS; Pradosh K. Ray, Mechanical Engineering Department, Tuskegee University, Tuskegee, AL 36088

2001-114: THRUST-VECTOR TILTING CAUSED BY GRID MISALIGNMENT; M. Tartz, E. Hartmann, R. Deltschew, and H. Neumann, Institut für Oberflächenmodifizierung e. V. (IOM), Permoserstr. 15, D-04318 Leipzig, Germany

2001-115: ION THRUSTER THRUST VECTORING REQUIREMENTS AND TECHNIQUES; David G. Fearn, Space Department, QinetiQ, Farnborough, Hants, GU12 0LX, UK

2001-116: OPERATIONAL FEATURES OF A LINEAR SLIT COLLOID MICROTHRUSTER; Julius Perel and John F. Mahoney, Phrasor Scientific Incorporated, Duarte, CA 91010

2001-117: EFFECTS OF ION IMPLANTED C AND N ON THE SPUTTER BEHAVIORS OF TI AND MO GRID MATERIALS; Paul J. Wilbur and Joshua Miller, Department of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523; Don L. Williamson, Department of Physics, Colorado School of Mines, Golden, CO 80401

2001-118: SPUTTER CHARACTERISTICS OF CARBON-CARBON COMPOUND MATERIAL; R. Deltschew, M. Tartz, V. Plicht, E. Hartmann, and H. Neumann, Institut für Oberflächenmodifizierung e. V. (IOM), Permoserstr. 15, D-04318 Leipzig, Germany; H. J. Leiter, Astrium GmbH, Space Infrastructure, PF 80 11 69, D-81663 Müchen, Germany; J. Esch, Schunk Kohlenstofftechnik GmbH, Rodheimer Straße 59, D-35452 Heuchelheim, Germany

2001-120: A STUDY OF LOW-POWER MPD ARCJETS FOR FUTURE HIGH-POWER EVOLUTION; Kyoichiro Toki and Yukio Shimizu, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2001-123: DEVELOPMENT AND TESTING OF A NEW TYPE OF MPD THRUSTER; V.B. Tikhonov, N. N. Antropov, G. A. Dyakonov, and V. A. Obukhov, RIAME MAI, 125080 Moscow, PB 43, Russi;, F. Paganucci, P. Rossetti, and M. Andrenucci, CENTROSPAZIO, Via Gherardesca, 5, 56014, Pisa, Italy

2001-124: DESIGN AND OPERATION OF MW-CLASS MPD THRUSTERS PART I: NUMERICAL MODELING; Pavlos G. Mikellides, Ohio Aerospace Institute, 22800 Cedar Point Dr., Cleveland, OH 44142

2001-127: PARALLELIZATION AND VALIDATION OF MHD CODE FOR THE SIMULATION OF SELF-FIELD MPDT FLOWS; K. Sankaran, S. C. Jardin, and E. Y. Choueiri, Princeton University, Princeton, New Jersey 08544

2001-128: NUMERICAL SIMULATION OF HIGH POWER STEADY STATE MPD THRUSTERS; Jörg Heiermann and Monika Auweter-Kurtz, Institut für Raumfahrtsysteme, Universität Stuttgart, Pfaffenwaldring 31, 70550 Stuttgart, Germany

2001-130: EFFECT OF APPLIED MAGNETIC FIELD ON ARCJET THRUSTER; Takeshi Miyasaka, Department of Aerospace Engineering, Nagoya University, Furo, Chikusa, Nagoya 464-8603, Japan; Hiroshi Katsurayama, Department of Aeronautics and Astronautics, University of Tokyo, Hongo, Bunkyo, Tokyo 113-8656, Japan; Toshi Fujiwara, Department of Aerospace Engineering, Nagoya University, Furo, Chikusa, Nagoya 464-8603, Japan

2001-131: EFFECT OF STRONG MAGNETIC FIELD ON TEMPERATURE DISTRIBUTION IN PLASMA JET; Kazuo Koike and Norifumi Ono, Department of Mechanical Engineering, Tohoku Gakuin University, 1-13-1, Chuo, Tagojo, Miyagi 985-8537, Japan; Takashi Uno, Sayama Precision Co., Ltd, 2-15-1, Fujimi, Sayama, Saitama 350-1393, Japan

2001-132: PERFORMANCE OF AN APPLIED FIELD MPD THRUSTER; F. Paganucci, P. Rossetti, and M. Andrenucci, Centrospazio, Via Gherardesca 5, I-56014, Pisa, Italia; V. B. Tikhonov and V. A. Obukhov, RIAME-MAI, Volokolamskoe shosse, 4, 125810, Moscow, Russia

2001-133: EXHAUST PLUME CHARACTERISTICS OF QUASI-STEADY MPD THRUSTERS; Hirokazu Tahara, Yoichi Kagaya, and Takao Yoshikawa, Division of Mechanical Science, Dept. of Systems and Human Science, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

2001-134: OPERATION OF AN MPD THRUSTER WITH A TYPE B CATHODE; Paola Rossetti, Fabrizio Paganucci and Mariano Andrenucci, Centrospazio, Via Gherardesca 5, I-56014, Pisa, Italia

2001-135: PLASMA DIAGNOSTICS IN AN APPLIED FIELD MPD THRUSTER; G. Serianni and N. Vianello, Consorzio RFX, Associazione Euratom-ENEA sulla Fusione, Corso Stati Uniti, 4, 35127 Padova, Italy; F. Paganucci, P. Rossetti, and M. Andrenucci, CENTROSPAZIO, Via A. Gherardesca, 5, 56014 Pisa; V. Antoni and M. Bagatin, Consorizo RFX, Associazione Euratom-ENEA sulla Fusione, INFM, Unitá di Padova, Sez. A, Italy

2001-139: SELF-APPLIED MAGNETIC FIELD INTENSITY EFFECTS ON SOLID PROPELLANT MPD THRUSTER PERFORMANCE; Luigi Petrucci and Giorgio Paccani, Universitá degli Studi di Roma “La Sapienza”, Dipartimento Meccanica e Aeronautica, Via Eudossiana 18, 00184 Rome, Italy

2001-140: SELF-APPLIED MAGNETIC FIELD EFFECTS ON SOLID PROPELLANT MPD THRUSTER PERFORMANCE; Giorgio Paccani  and Luigi Petrucci, Universitá degli Studi di Roma “La Sapienza”, Dipartimento Meccanica e Aeronautica, Via Eudossiana 18, 00184 Rome, Italy

2001-142: ATTILA-ADJUSTABLE THROTTLE INDUCTIVELY AFTERBURNING ARC JET; Stefan Laure, Dr. Laure Plasmatechnologie GmbH, Stuttgart, Germany; Jörg Heiermann, Monika Auweter-Kurtz, and Helmut Kurtz, Institut für Raumfahrtsysteme (IRS), Universität Stuttgart, Germany

2001-145: PERFORMANCES AND DESIGN STUDIES STATUS OF THE P4S-1 THRUSTER; H. Brito, Instituto Universitario Aeronáutico, Av. Fuerza Aérea Argentina, km 5.5, (5016) Córdoba, Argentina; S. Elaskar, Instituto Universitario Aeronáutico, Departmento de Aeronáutica, Universidad Nacional de Córdoba, Av. Velez Sarfield 1600, (5000), Córdoba, Argentina; C. Brito, ENSAE, Toulouse, France, R. Ballete, Departmento de Aeronáutica, Universidad Nacional de Córdoba, Av. Velez Sarfield 1600, (5000), Córdoba, Argentina

2001-146: SIMPLE AND EFFICIENT CIRCUIT FOR THE INITIATION PROCESS OF AN ABLATIVE PULSED PLASMA THRUSTER (APPT); Roberto Manno, Carlos Fiala, and Carlos Bortis, Facultad de Ingeniería, Ruta 35 Km 601 (5800), Río Cuarto Argentina, Universidad Nacional de Río Cuarto

2001-147: EVALUATION OF ALTERNATE PROPELLANTS FOR PULSED PLASMA THRUSTERS; Eric J. Pencil and Hani Kamhawi, National Aeronautics and Space Administration, Glenn Research Center, 21000 Brookpark Road, Cleveland, OH 44135

2001-148: IMPACT OF PERFORMANCE SCALING ON MISSION ANALYSIS FOR GAS-FED PULSED PLASMA THRUSTERS; John K. Ziemer, Jet Propulsion Laboratory, M/S 125-109; California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109; Rodney A. Petr, Science Research Laboratory, Inc., Sommerville, MA 02143

2001-150: DEVELOPMENT OF A MULTIPLEXED COAXIAL PULSED PLASMA THRUSTER; Darren M. King, Wayne C. Solomon, and David L. Carroll, CU Aerospace, Urbana, IL 61802; Rodney L. Burton, Erik L. Antonsen, and Filip Rysanek, University of Illinois at Urbana-Champaign, Urbana, IL 61801; John Frus, Unison Industries, Jacksonville, FL 32256

2001-151: PERFORMANCE AND HEAT LOSS OF A COAXIAL TEFLON PULSED PLASMA THRUSTER; Filip Rysanek and Rodney Burton, University of Illinois Urbana-Champaign, 306 Talbot Lab, 104 South Wright St., Urbana, IL 61801

2001-152: PERFORMANCE IMPROVEMENT OF PULSED PLASMA THRUSTER FOR MICRO SATELLITE; Miwa Igarashi, Naoki Kumagai, Kensuke Sato, Kouji Tamura, and Hanuki Takegahara, Tokyo Metropolitan Institute of Technology, Asahigaoka 6-6, Hino, Tokyo 191-0065, Japan; Hiroyuki Okamoto, Astro Research Corporation, Kugenuma Tachibana 1-1-4, Fujisawa, Kanagawa, 251-0024, Japan; Takashi Wakizono, HI-SERVE Corporation, Totohara 780-7, Akiruno, Tokyo, 190-0152, Japan; Hidekazu Hashimoto, National Space Development Agency of Japan, Office of Research and Development, Advanced Mission Research Center, Micro Space Systems Laboratory, Sengen, 2-1-1, Tsukuba, Ibaraki 305-0047, Japan

2001-153: EVALUATION OF PULSED PLASMA THRUSTER SYSTEM FOR µ-LAB SAT II; Haruki Takegahara, Miwa Igarashi, Naoki Kumagai, Kensuke Sato, and Kouji Tamura, Tokyo Metropolitan Institute of Technology, Dept. of Aerospace Eng., Asahigaoka 6-6, Hino, Tokyo 191-0065, Japan; Mitsuteru Sugiki, Astro Research Corporation, Kugenuma Tachibana 1-1-4, Fujisawa, Kanagawa, 251-0024, Japan; Hidekazu Hashimoto, National Space Development Agency of Japan, Advanced Mission Research Center, Micro Space Systems Laboratory, Sengen, 2-1-1, Tsukuba, Ibaraki 305-0047, Japan

2001-154: A HIGH-ORDER DISCONTINUOUS GALERKIN METHOD FOR MODELING MICRO-PULSED PLASMA THRUSTERS; G. Lin and G. E. Karniadakis, Division of Applied Mathematics, Brown University, Providence, RI 02912

2001-155: ANALYSES OF TEFLON SURFACE CHARRING AND NEAR FIELD PLUME OF A MICRO-PULSED PLASMA THRUSTER; Michael Keidar and Ian D. Boyd, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109; Frank S. Gulczinski III, Erik L. Antonsen and Gregory G. Spanjers, Air Force Research Laboratory, Propulsion Directorate, Electric Propulsion Laboratory, Edwards AFB, CA 93524

2001-156: DOUBLE DISCHARGE OPERATION FOR PULSED PLASMA THRSUTERS; Maki Okada, Yasushi Okawa, and Takeshi Tachibana, Kyushu Institute of Technology, 1-1, Sensuicho, Tobata, Kitakyushu 804-8550, Japan

2001-157: HIGH RESOLUTION LASER DIAGNOSTICS IN MILLIMETER-SCALE MICRO PULSED PLASMA THRUSTERS; Erik L. Antonsen and Rodney L. Burton, University of Illinois at Urbana-Champaign, IL 61801; Gregory G. Spanjers, AFRL Propulsion Directorate, Edwards AFB, CA 93524

2001-159: TWO-DIMENSIONAL NUMERICAL SIMULATION OF COAXIAL APPT; G. A. Popov, Research Institute of Applied Mechanics and Electrodynamics, 4, Volokolamskoye shosse, Moscow, 125810, Russia; M. N. Kazeev and V. F. Kozlov, Russian Research Centre “Kurchatov Institute,” 1, Kurchatov sq,. Moscow, 123182, Russia

2001-161: SOLUTION OF REAL MAGNETOGASDYNAMICS EQUATIONS USING A TVD SCHEME AS A TOOL FOR ELECTRIC PROPULSION; Sergio A. Elaskar, Departamento de Aeronáutica, Universidad Nacional de Córdoba, Av. Velez Sarfield 1601,Córdoba (5000), Argentina; Hector H. Brito, Centro de Investigaciones Aplicadas, Instituto Universitario Aeronáutico, Ruto 20, km. 5.5, Córdoba (5022), Argentina

2001-162: EXPERIMENTAL AND THEORETICAL INVESTIGATION OF A COAXIAL INVERSE-PINCH PULSED PLASMA THRUSTER II; Hani Kamhawi, The Ohio State University, Columbus, OH 43220; Pavlos G. Mikelides, Ohio Aerospace Institute, Brook Park, OH 44142; Peter J. Turchi, Los Alamos National Laboratory

2001-163: EXPERIMENTAL STUDY OF PLASMA PARAMETERS IN HIGH-EFFICIENCY PULSED PLASMA THRUSTERS; Garri Popov, Nikolay Antropov, Grigory Dyakonov, Michail Orlov, Valery Tyutin, and Vladimir Yakovlev, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), 5, Leningradskoye shosse, post box 43, Moscow, 125080, Russia

2001-165: THE AFRL TECHSAT 21 PROPULSION SUBSYSTEM DEVELOPMENT PROGRAM; Daron R. Bromaghim and Greg G. Spanjers, Air Force Research Laboratory, AFRL/PRSS, 1 Ara Road, Edwards AFB, CA 93524-7013; Lee K. Johnson, The Jet Propulsion Laboratory, M/S 125-721, 4800 Oak Grove Drive, Pasadena, CA 91106; Ricardo Gorecki, F. Dong Tan, and Robert Vondra, TRW, One Space Park, Redondo Beach, CA, 90278; Bruce Pote, Busek Co., Inc., 11 Tech Circle, Natick, MA, 01760; Joe Barbarits, Moog, Inc., Space Products Division, East Aurora, NY 14052

2001-166: AFRL MICROPPT DEVELOPMENT FOR THE TECHSAT 21 FLIGHT; Gregory G. Spanjers, Daron R. Bromaghim, Capt. James Lake, and Michael Dulligan, AFRL Propulsion Directorate, Edwards AFB, CA 93524; David White, John H. Schiling, and Stewart  Bushman, W.E. Research, Rosamond, CA

2001-167: PLASMA PROPULSION ON STENTOR SATELLITE: IN FLIGHT ACCEPTANCE OPERATIONS AND EXPERIMENTAL PROGRAM; Franck Darnon, Luc Petitjean, Jean-Pierre Diris, Jacques Hoarau, and Louis Torres Centre National d’Etudes Spatiales, 18 av. E. Belin, 31401 Toulouse, France; Thierry Grassin, Alcatel Space, 100 Bd du Midi, 06159 Cannes, France

2001-169: PROPULSION INSTRUMENTS FOR SMALL HALL THRUSTER INTEGRATION; Lee. K. Johnson and David G. Conroy, The Jet Propulsion Laboratory, M/S 125-109, 4800 Oak Grove Drive, Pasadena, CA 91109-8099; Greg G. Spanjers and Daron R. Bromaghim, Air Force Research Laboratory, AFRL/PRSS, 1 Ara Road, Edwards AFB, CA 93524-7013

2001-170: CONCEPTUAL DESIGN OF A SYNERGISTIC PROPULSION SYSTEM FOR THE INTERNATIONAL SPACE STATION (ISS); Jochen Wilms, Arndt Hinüber, Godehard Nentwig, and Monkia Auweter-Kurtz, Institut für Raumfahrtsysteme (Space Systems Institute), Pfaffenwaldring 31, D-70550 Stuttgart, Germany

2001-172: SYSTEMS-LEVEL TRADE STUDIES OF A DUAL-MODE SPT FOR GEOSYNCHRONOUS COMMUNICATIONS SATELLITES; J. Steven Snyder, Tom Randolph, David Oh, Birgit Sauer, and Guenter Fischer, Space Systems/Loral, 3825 Fabian Way, Palo Alto, CA

2001-173: ANALYTIC OPTIMIZATION OF MIXED CHEMICAL-ELECTRIC ORBIT RAISING MISSIONS; David Y. Oh, Glenn Santiago, Space Systems/Loral, 3825 Fabian Way M/S G-80, Palo Alto, CA

2001-174: TECHNOLOGICAL READINESS OF MICROWAVE ION ENGINE SYSTEM FOR MUSES-C MISSION; Kyoichiro Toki, Hitoshi Kuninaka, Kazutaka Nishiyama, and Yukio Shimizu, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan; Ikkoh Funaki, University of Tsukuba, 1-1-1, Tennodai, Tsukuba, Ibraki 305-8577, Japan

2001-175: EVALUATING ADVANCED PROPULSION SYSTEMS FOR THE TITAN EXPLORER MISSION; Muriel Noca and Robert Frisbee, Jet Propulsion Laboratory, California Institute of Technology, MS 301-180, MS 125-109, 4800 Oak Grove Drive, Pasadena, CA 91106; Les Johnson and Larry Kos, Mail Code TD15, Bldg. 4203, Mail Code TD30, Bldg. 4203, Marshall Space Flight Center, Huntsville, AL 35812; Leon Gefert and Len Dudzinski, NASA Glenn Research Center, MS 86-15, 21000 Brookpark Rd., Cleveland, Ohio 44135

2001-176: ION PROPULSION TECHNOLOGY FOR FAST MISSIONS TO PLUTO; Dave Rodgers and John Brophy, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

2001-177: A POSSIBLE ASTEROID RENDEZVOUS MISSION LAUNCHED AS AN ARIANE 5 AUXILIARY PAYLOAD; David G. Fearn, Space Department, QinetiQ, Farnborough, Hants, GU14 0LX, UK; Nigel S. Wells, Space Department QinetiQ, Farnborough, Hants, GU14 0LX, UK

2001-179: OUTER PLANET EXPLORATION WITH ADVANCED RADIOISOTOPE ELECTRIC PROPULSION; Steve Oleson, Leon Gefert, Michael Patterson, Jeffrey Schreiber, and Scott Benson, National Aeronautics and Space Administration, Glenn Research Center, MS 500-203, 21000 Brookpark Rd., Cleveland, OH 44135; Jim McAdams and Paul Ostdiek, The Johns Hopkins University, Applied Physics Laboratory, 11100 Johns Hopkins Road, Laurel, MD 20723-6099

2001-181: OPTIMIZATION OF ELECTRIC THRUSTERS FOR PRIMARY PROPULSION BASED ON THE ROCKET EQUATION; Monkia Auweter-Kurtz and Helmut Kurtz, Institut für Raumfahrtsysteme, Universität Stuttgart, Pfaffenwaldring 31, 70550 Stuttgart, Germany

2001-182: ABLATIVE PULSED PLASMA THRUSTER SYSTEM OPTIMIZATION FOR MICROSATELLITES; Paolo Gessini, Astronautics Research Group, School of Engineering Sciences, University of Southampton, Highfield, Southampton, Hants, SO17 1BJ, United Kingdom; Giorgio Paccani, Dipartimento di Meccanica e Aeronautica, Universitá degli Studi di Roma “La Sapienza”, Via Eudossiana 18, 00184 Rome, Italy

2001-187: ELECTRIC PROPULSION FOR A REUSABLE SPACE CARGO; Ivo Vieira, GoLP – Grupo de Lasers e Plasmas, Centro de Fisica de Plasmas, Complexo Interdisciplinar, Piso 2, Instituto Superior Ténico, Av. Rovisco Pais, 1049-001, Lisboa - Portugal

2001-191: EVAPORATION – TYPE RESISTOR THRUSTER WITH THERMAL CATALYTIC DECOMPOSITION OF HYDRAZINE; V.N. Vinogradov, B. E. Didenko, V. M. Murashko, and A. G. Njatin, EDB FAKEL, Russian Federation, Kaliningrad, 236000, Moskovsky prospect, 181

2001-192: MULTI-HOUR TEST OF TUNSTEN ANODES FOR A LOW POWER DC ARCJET; Kiyoshi Kinefuchi, Ikkoh Funaki and Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagaw, 229-8510, Japan; Yasuyuki Suwama, NEC Aerospace Systems, LTD., 1-10 Nisshin, Fuchu, Tokyo, 183-8501, Japan; Kenichi Okamoto, Allied Material Corporation, 2 Iwasekoshi-machi, Toyama-shi, Toyama, 931-8371, Japan

2001-193: NUMERICAL STUDIES ON EFFECT OF NOZZLE GEOMETRY AND OF FLOW CONTINUITY ON THRUST PERFORMANCE; S. Hatta and S. Aso, Space Transportation Systemd Engineering Laboratory, Department of Aeronautics and Astronautics, Kyushu University, 6-10-1 Hakozaki, Higashi-ku, Fukuoka-shi, 812-8581, Japan

2001-194: NON-EQUILIBRIUM NUMERICAL STUDY OF A TWO-STAGE MICROWAVE ELECTROTHERMAL THRUSTER; V. P. Chiravalle, R. B. Miles and E. Y. Choueiri, Princeton University, Princeton, NJ 08544

2001-195: DIAGNOSTICS OF ATOMIC OXYGEN IN ARC-HEATER PLUMES; Makoto Matsui, Kimiya Komurasaki, and Yoshihiro Arakawa, University of Tokyo, 7-3-1 Hongo, Bunkyo, Tokyo 113-8656, Japan; Masahito Mizuno, National Aerospace Laboratory of Japan (NAL), 7-44-1 Jindaiji Higashi-machi, Chofu, Tokyo, 182-8522, Japan

2001-196: CHARACTERISTICS OF TIN COATINGS BY GAS TUNNEL TYPE PLASMA REACTIVE SPRAYING; Akira Kobayashi, Joining and Welding Research Institute, Osaka University, 11-1 Mihogaoka, Ibaraki, Osaka 567-0047, Japan

2001-200: COMPUTER MODELING OF THE LABORATORY TESTING OF MINI-MAGNETOSPHERIC PLASMA PROPULSION (M2P2); R. M. Winglee and  P. Euripides, Department of Earth and Space Sciences, Univeristy of Washington, Seattle, WA 98145-1650;  J. Slough and T. Ziemba, Department of Aeronautics and Astronautics, University of Washington, Seattle, WA 98195-2400

2001-201: PARAMETERIZATION OF THE LABORATORY PERFORMANCE OF THE MINI-MAGNETOSPHERIC PLASMA PROPULSION (M2P2) PROTOTYPE; T. M. Ziemba and J. Slough, Department of Aeronautics and Astronautics, University of Washington, Box 352400, Seattle, WA 98195-2400; R. M. Winglee and P. Euripides, Department of Earth and Space Science, University of Washington, Box 351650, Seattle, WA 98195-2400

2001-202: HIGH BETA PLASMA FOR INFLATION OF A DIPOLAR MAGNETIC FIELD AS A MAGNETIC SAIL; John Slough, Redmond Plasma Physics Laboratory, University of Washington, 14700 NE 95th Street, Redmond, WA 98052

2001-205: PRESSURE WAVES IN A FAR-FIELD REPETITIVE PULSE LASER THRUSTER; Koichi Mori, Hiroshi Katsurayama, Kimiya Komuraski, and Yoshihiro Arakawa, University of Tokyo, Hongo 7-3-1, Bunkyo, Tokyo 113-8656, Japan

2001-207: THRUST MEASUREMENT OF A CW LASER THRUSTER IN VACUUM; Kazuhiro Toyoda, Kyushu Institute of Technology, Komurasaki Kimiya and Yoshihiro Arakawa, University of Tokyo

2001-208: NUMERICAL STUDY OF PLASMA PRODUCTION IN THE VASIMR THRUSTER; Oleg Batishchev and Kim Molvig, Massachusetts Institute of Technology, Nuclear Engineering Department, MIT NW 16-258, 167 Albany St., Cambridge, MA 02139, USA

2001-209: ION ACCELERATION BY BEATING ELECTROSTATIC WAVES: CRITERIA FOR REGULAR AND STOCHASTIC ACCELERATION; R. Spektor and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey 08544

2001-210: THE POTENTIAL FOR COMPACT HELICON WAVE SOURCES FOR ELECTRIC PROPULSION; Jim Gilland, Ohio Aerospace Institute, NASA Glenn Research Center, Cleveland, OH 44142

2001-211: A THEORETICAL ANALYSIS OF VACUUM ARC THRUSTER PERFORMANCE; James E. Polk, Mike Sekerak, and John K. Ziemer, Jet Propulsion Laboratory, M/S 125-109, 4800 Oak Grove Drive, Pasadena, CA 91109, Jochen Schein, Niansheng Qi and Robert Binder, Alameda Applied Sciences Corp, 2235 Polvorosa Ave. San Leandro, CA 94577; André Anders, Lawrence Berkeley National Laboratory, 1 Cyclotron Road, Berkeley, CA 94720

2001-214: OPPOSED-CAVITY SOLAR THERMAL THRUSTER MADE OF SINGLE CRYSTAL TUNGSTEN; Hironori Sahara, Japan Science and Technology Corporation (JST), 7-44-1, Jindaiji-Higashi-Machi, Chofu, Tokyo, 182-8522, Japan; Morio Shimizu, National Aerospace Laboratory of Japan (NAL), Japan; Tadayuki Fujii, National Institute of Materials Science (NIMS), Japan, Ken-ichi Okamoto, Shigehiko Takaoka, Allied Material Corporation, Japan; Yoshihiro Nakamura, Hosei University, Japan

2001-220: A DIODE-LASER-DRIVEN MICROTHRUSTER; Claude R. Phipps, Photonic Associates, 200A Ojo de la Vaca Road, Santa Fe, NM 87508; James R. Luke and G. Glen McDuff, UNM/New Mexico Engineering Research Institute, 901 University Blvd. SE, Albuquerque, NM 87106-4339

2001-221: COMPACT PLASMA ACCELERATOR FOR MICRO-PROPULSION APPLICATIONS; John e. Foster, NASA Glenn Research Center, Cleveland, OH 44135, USA

2001-223: DIODE LASER DRIVEN MICROTHRUSTER PROTOTYPE; James R. Luke, UNM/New Mexico Engineering Research Institute, 901 University Blvd. SE, Albuquerque, NM 87109-4339; Claude R. Phipps, Photonic Associates, 200A Ojo de la Vaca Road, Sante Fe, NM 87505; G. Glen McDuff, UNM/New Mexico Engineering Research Institute, 901 University Blvd. SE, Albuquerque, NM 87106-4339

2001-224: DEVELOPMENT OF MICROWAVE ENGINE; Shin Satori, Hokkaido Institute of Technology, Hiroyuki Okamoto, Ted Mitsuteru Sugiki, and Yasumasa Ito, Astro Research Corporation; Yoshinori Aoki, Atsushi Nagata, and Takayoshi Kizaki, Advanced Technology Institute, 7-15-4-1, Maeda, Teine, Sapporo, Hokkaido 006-8585, Japan

2001-226: HOLLOW CATHODE MICRO-THRUSTER PERFORMANCE; Michael J. Patterson and John E. Foster, National Aeronautics and Space Administration, Glenn Research Center, MS 301-3, 21000 Brookpark Road, Cleveland, OH 44135

2001-228: LOW MASS VACUUM ARC THRUSTER SYSTEM FOR STATION KEEPING MISSION; Jochen Schein, Niansheng Qi, Robert Binder, and Mahadevan Krishnan, Alameda Applied Sciences Corp, 2235 Polvorosa Ave, San Leandro, CA 94577; John K. Ziemer and James E. Polk, NASA Jet Propulsion Laboratory, 4800 Oak Grove Drive, Pasadena, CA 91109; André Anders, Lawrence Berkeley National Laboratory, 1 Cyclotron Road, Berkeley, CA 94720

2001-231: STUDY OF VERY LOW-POWER DC PLASMA-JET MICROTHRUSTERS; Hideyuki Horisawa, Department of Aerospace Engineering, Tokai University, 1117 Kitakaname, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo, and Nara Textile Inc., 4-19-4 Nakahara, Isogo, Yokohama, 235-0036, Japan

2001-232: TEMPERATURE AND POWER PREDICTIONS FOR FLIGHT-TESTING THE FREE MOLECULE MICRO-RESISTOJET; Joyce Wong and Helen Reed, Arizona State University, Mechanical & Aerospace Engineering, Campus Box 6106; Andrew Ketsdever, Air Force Research Laboratory, Propulsion Directorate, Edwards AFB, CA 93524

2001-233: THE HOLLOW CATHODE AS A MIRCO-ION THRUSTER; Paolo Gessini and Stephen B. Gabriel, Astronautics Research Group, School of Engineering Sciences, University of Southampton, Highfield, Southampton, Hants, SO17 1BJ, United Kingdom; David G. Fearn, Space Department, Y72 Building, QinetiQ, Farnborough, Hants, GU14 0LX, United Kingdom

2001-234: CONCEPTUAL DESIGN OF AN ION MICROTHRUSTER; K. G. Hutchison and S. B. Gabriel, School of Engineering Sciences, University of Southampton, Southampton, Hants, SO17 3QX, UK

2001-235: A TORSIONAL BALANCE THAT RESOLVES SUB-MICRO-NEWTON FORCES; Manuel Gamero-Castaño and Vlad Hruby, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760-1023; Manuel Martinez-Sánchez, Massachusetts Institute of Technology, 77 Massachusetts Ave., 37-401, Cambridge, MA 02139

2001-236: ACCURATE MEASUREMENT OF NANO-NEWTON THRUST FOR MICROPROPULSION SYSTEM CHARACTERIZATION; Andrew J. Jamison and E. P. Muntz, Department of Aerospace and Mechanical Engineering, University of Southern California, Los Angeles, CA 90089-1191; Andrew D. Ketsdever, Air Force Research Laboratory, Propulsion Directorate, Edwards AFB, CA 93524

2001-238: PERFORMANCE MEASUREMENTS USING A SUB-MICRONEWTON RESOLUTION THRUST STAND; John K. Ziemer, Jet Propulsion Laboratory, M/S 125-109, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109

2001-240: PROPULSIVE SMALL EXPANDABLE DEPLOYER SYSTEM (PROSEDS): PREPARING FOR FLIGHT; Brian Gilchrist, Space Physics Research Laboratory, University of Michigan, Ann Arbor, MI 48109-2143; Judy Balance, Leslie Curtis, Les Johnson, Jason Vaughn, and Ken Welzyn, Marshall Space Flight Center, National Aeronautics and Space Administration, Huntsville, AL 35812

2001-242: EVALUATION OF PLASMA CONTACTOR GROUND EXPERIMENTS FOR ELECTRODYNAMIC TETHER; Masaya Kozakai and Haruki Takegahara, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino, Tokyo 191-0065, Japan

2001-243: KINETIC MODELING OF THE ELECTRON CURRENT COLLECTION TO A MOVING BARE ELECTRODYNAMIC TETHER; Eric Choiniére and Brian E. Gilchrist, Radiation Laboratory, EECS Department, University of Michigan, 1301 Beal Avenue, Ann Arbor, MI 48109-2122

2001-244: PERFORMANCE OF ELECTRODYNAMIC TETHER DE-ORBIT SYSTEM ON ELLIPTICAL ORBIT; Yoshiki Yamagiwa, Ryosuke Tuyuki, Shinichi Takenaka and Eiji Hiragi, Faculty of Engineering, Shizuoka University, 3-5-1, Johoku, Hamamatsu, Shizuoka 432-8561, Japan

2001-245: PIC COMPUTATION OF ELECTRON CURRENT COLLECTION TO A MOVING BARE TETHER IN THE MESOTHERMAL CONDITION; Tatsuo Onishi and Manuel Martínez-Sánchez, Massachusetts Institute of  Technology, Cambridge, Massachusetts, USA; David L. Cooke, Air Force Research Laboratory, Space Vehicle Directorate, Hanscom AFB, MA, USA; Juan R. Sanmartín, Universidad Politécnica de Madrid, Spain

2001-251: A HALL-EFFECT THRUSTER PLUME AND SPACECRAFT INTERACTIONS MODELING PACKAGE; I. G. Mikellides, G. A. Jongeward, G. A., B. M. Gardner, I. Katz, M. J. Mandell and V. A. Davis, Science Applications International Corporation, 9455 Towne Center Drive, MS W2076, San Diego, CA 92121

2001-252: CORRELATION OF HOLLOW CATHODE ASSEMBLY AND PLASMA CONTACTOR DATA FROM GROUND TESTING AND IN-SPACE OPERATION ON THE INTERNATIONL SPACE STATION; Scott D. Kovaleski, QSS Group, Inc., NASA Glenn Research Center Group, 21000 Brookpark Rd, MS 301-3, Cleveland, OH 44135; Michael J. Patterson and George C. Soulas, NASA Glenn Research Center, 21000 Brookpark Rd., MS 301-3, Cleveland, OH 44135

2001-254: EXPANSION OF SECONDARY PLASMA GENERATED IN AN EP PLUME. THEORY AND EXPERIMENT; B. S. Borisov, A. G. Korsun, F. F. Gabdullin, N. V. Kozyrev, A. V. Semenkin, and E. M. Tverdokhlebova, Central Research Institute of Machine Building (TSNIIMASH), 141070 Korolev, Moscow region, Russia

2001-257: METHODS FOR INVESTIGATING THE INFLUENCE OF SELF-INDUCED ELECTROMAGNETIC EMISSION OF ELECTRIC PROPULSIONS UPON THE SENSITIVITY CHARACTERISTICS OF ONBOARD RADIO SYSTEMS OF SPACECRAFTS; A. P. Plokhikh, N. A. Vazhenin, and G. V. Soganova, Research Institute of Applied Mechanics and Electrodynamics (RIAME), P.O. Box 43, Moscow 125080, Russia

2001-258: MITIGATION PROCESS OF SPACECRAFT NEGATIVE CHARGING BY PLASMA FLOW; Hirokazu Tahara, Daiki Matsuyama, Toshiaki Yasui and Takao Yoshikawa, Division of Mechanical Science, Dept. of Systems and Human Science, Graduate School of Engineering Science, Osaka University, 1-3 Machikaneyama Toyonaka, Osaka 560-8531, Japan

2001-260: PLASMA PLUME FAR FIELD ANALYSIS; J. Ashkenazy, Propulsion Physics Laboratory, Soreq NRC, Yavne 81800, Israel; A. Fruchtman, Holon Academic Institute of Technology, Holon 58102, Israel

2001-261: SOLUTION OF REAL MAGNETOGASDYNAMICS EQUATIONS USING A TVD SCHEME AS A TOOL FOR ELECTRIC PROPULSION; Sergio A. Elaskar, Departamento de Aeronáutica, Universidad Nacional de Córdoba Av. Velez Sarfield 1601, Córdoba (5000), Argentina; Héctor H. Brito, Centro de Investigaciones Aplicadas, Instituto Universitario Aeronáutico, Ruta 20 km, 5.5, Córdoba (5022), Argentina

2001-262: PPS EFFEXTS ON SATELLITES ANALYSES AND TOOLS IN ALCATEL SPACE INDUSTRIES; V. Perrin, D. Pogarieloff, P. Métois, and S. Brosse, Alcatel Space Industries, 100 Bd du Midi 06156 Cannes la Bocca Cedex, France

2001-264: PIC SIMULATIONS OF SPACECRAFT CHARGING AND ITS NEUTRALIZATION PROCESS BY PLASMA EMISSION; Hideyuki Usui, Hiroshi Matsumoto, Makoto Yasugi, and Yoshiharu Omura, Radio Science Center for Space and Atmosphere, Kyoto University, Gokasho, Uji, Kyoto 611-0011, Japan

2001-270: RECENT DEVELOPMENT ACTIVITIES IN HOLLOW CATHODE TECHNOLOGY; Michael J. Patterson and Matthew T. Domonkos, National Aeronautics and Space Administration, Glenn Research Center, MS 301-3, 21000 Brookpark Road, Cleveland, Ohio 44135; Christian Carpenter and Scott d. Kovaleski, QSS Group, Inc., Cleveland, Ohio

2001-271: A REVIEW OF TESTING OF HOLLOW CATHODES FOR THE INTERNATIONAL SPACE STATION PLASMA CONTACTOR; S. D. Kovaleski, QSS Group, Inc., NASA Glenn Research Center Group, 21000 Brookpark Rd., Cleveland, OH 44135; M. J. Patterson, G. C. Soulas, and T. R. Sarver-Verhey, NASA Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH 44135

2001-272: THE RESULTS OF RESEARCHING OF LOW-CURRENT SELFHEATED HOLLOW CATHODES ON ELECTRIC CURRENT RANGE FROM 0,3 UP TO 0,5 A; Dr. Loyan A., Koshelev N., STC SPE “KhAI”, 17, Chkalova st., 310070, Kharkov, Ukraine

2001-273: HIGH-CURRENT SELF-HEATED HOLLOW CATHODES WITH OPERATION CURRENT MORE THAN 25 A. STATE AND DEVELOPMENT; Dr. Loyan A., Dr. Oransriy A., and Ichenko E., STC SPE “KhAI”, 17, Chkalova st. 310070, Kharkov, Ukraine

2001-274: HIGH-CURRENT HOLLOW CATHODE DEVELOPMENT; Christian B. Carpenter, QSS Group, Inc., MS 16-1, 21000 Brookpark Rd., Cleveland, OH 44135; Michael J. Patterson, NASA Glenn Research Center, MS 301-3, 21000 Brookpark Rd., Cleveland, OH 44135

2001-276: LIFE MODEL OF HOLLOW CATHODES USING A BARIUM CALCIUM ALUMINATE IMPREGNATED TUNGSTEN EMITTER; S. D. Kovaleski, QSS Group, Inc., NASA Glenn Research Center Group, 21000 Brookpark Rd., Cleveland, OH 44135

2001-277: ON THE HOLLOW CATHODE FOR AN OXYGEN DISCHARGE; Yoshihiro Nakamura and Teruaki Sue, Department of Mechanical Engineering, Hosei University, 3-7-2, Kajino-cho, Koganei, Tokyo 184-8584, Japan

2001-278: EXPERIMENTAL PERFORMANCE EVALUATIONS OF MO AND ZRC-COATED MO FIELD EMISSION ARRAY CAHTODES IN OXYGEN ENVIRONMENTS; Colleen Marrese-Reading and Jay Polk, Jet Propulsion Laboratory (JPL), California Institute of Technology, M/S 125-109, 4800 Oak Grove Drive, Pasadena, CA 91106; Kevin L. Jensen, Naval Research Laboratory, Code 6841, ESTD, Washington, DC 20375-5347

2001-279: DEVELOPMENT OF FIELD EMITTER ARRAY TECHNOLOGY FOR ED TETHER PROPULSION; Dave Morris and Brian Gilchrist, Space Physics Research Laboratory, University of Michigan, Ann Arbor, MI 48109; Alec Gallimore, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, MI 48109

2001-280: PRELIMINARY RESULTS OF FIELD EMISSION CATHODE TESTS; James S. Sovey, NASA Glenn Research Center; Scott D. Kovaleski, QSS Group at NASA Glenn Research Center, MS 301-3, 21000 Brookpark Road, Cleveland, OH 44135

2001-281: MICRO NEWTON COLLOID THRUSTER SYSTEM DEVELOPMENT; Vlad Hruby, Manuel Gamero-Castaño, Paul Falkos, and Suren Shenoy, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760-1023

2001-282: CHARACTERIZATION OF A COLLOID THRUSTER PERFORMING IN THE MICRO-NEWTON THRUST RANGE; Manuel Gamero-Castaño and Vladimir Hruby, Busek Co. Inc., 11 Tech Circle, Natick, Massachusetts 01760

2001-283: CHARACTERIZATION OF ELECTROSPRAYS AND ITS RELEVANCE TO COLLOID THRUSTERS; Manuel Gamero-Castaño and Vladimir Hruby, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760-1023

2001-284: PERFORMANCE STUDIES OF A COLLOID THRUSTER SYSTEM; Freddy M. Pranajaya and Mark A. Cappelli, Thermosciences Division, Mechanical Engineering Department, Stanford University, Building 520, Stanford, CA 94309-3032

2001-286: THE EFFECT OF USING FINITE-WIDTH ELECTROSTATIC GATES IN TIME-OF-FLIGHT MEASUREMENTS FOR COLLOID THRUSTERS; Paulo Lozano and Manuel Martinez-Sánchez, Massachusetts Institute of Technology, Room 37-438, 70 Vassar St., Cambridge, MA 02139

2001-288: FEEP-5 THRUST VALIDATION IN THE 10-100µN RANGE WITH A SIMPLE NULLED-PENDULUM THRUST STAND: INTEGRATION PROCEDURES; D. Nicolini, E. Chesta, J. Gonzalez del Amo, and G. Saccoccia, European Space Agency, ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands; E. B. Hughes and S. Oldfield, National Physical Laboratory, Dimensional Metrology Section, Queens Road, Teddington, TW11 0LW Middlesex, United Kingdom

2001-289: INDIUM FEEP ENDURANCE TEST: PRELIMINARY RESULTS; Angelo Genovese, Martin Tajmar, and Wolfgang Steiger, ARC Seibersdorf research GmbH, A-2444 Seibersdorf, Austria; Friedrich Rüdenauer, International Atomic Energy Agency, A-2444 Seibersdorf, Austria

2001-290: IN-FEEP THRUSTER ION BEAM NEUTRALIZATION WITH THERMIONIC AND FIELD EMISSION CATHODES; Colleen Marrese-Reading, Jay Polk, Juergen Mueller, and Al Owens, Jet Propulsion Laboratory (JPL), California Institute of Technology, M/S 125-109, 4800 Oak Grove Drive, Pasadena, CA 91106; Martin Tajmar, ARC Seibersdorf Research GmbH, A-2444 Seibersdorf, Austria; Capp Spindt, SRI International, Bldg. 320T, 333 Ravenswood Ave., Menlo Park, CA 94025; Richard Fink, Field Emission Picture Element Technology (FEPET) Inc., 3006 Longhorn Blvd. Suite 107, Austin, TX 78758-7631

2001-291: PLUME CHARACTERISTICS OF THE INDIUM NEEDLE EMITTER (InFEEP) THRUSTER; D. Nicolini, E. Chesta, and J. Gonzalez del amo, European Space Agency, ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands

2001-295: FEEP THRUSTER SURVIVABILITY IN THE LEO ATOMIC OXYGEN ENVIRONMENT; Fabioo Ceccanti, Salva Marcuccio, and Mariano Andrenucci, Centrospazio – Alta S.r.l., Via Gherardesca 5, 56014 Ospedaletto, Pisa, Italy

2001 FILE DIRECTORY

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2003 INDEX

2003-003: OPTIMIZATION OF GEOGYNCHRONOUS SATELLITE SYSTEM USING ELECTRIC PROPULSION BASED ON GENETIC ALGORITHM; Han Xianwei, He Hongqing, Tang Jinlan Mao, Genwang, and Yang Juan, College of Astronautics, Northwestern Polytechnical University, Xi’an, P. R. Chine, 710072

2003-005: COMBINING ELECTRIC AND SAIL PROPULSION FOR INTERPLANETARY SAMPLE RETURN; Robert J. Noble, Stanford Linear Accelerator Center, Stanford University, 2575 Sand Hill Road, Menlo Park, California 94025 USA

2003-007: ABOUT MODEL OF JET PROPULSION; Kolgotin O. V., Engineer, Postgraduate Student Moscow aviation institute, Russia, Pensa, ul.Stavskogo 12-125 440008

2003-008: SPACE TRANSPORTER; Kolgotin O., The Moscow aviation institute (Technical University)

2003-011: NUMERICAL INVESTIGATION OF A HALL THRUSTER PLASMA INCLUDING SPUTTER YIELD, Subrata Roy and B. P. Pandey, Computational Plasma Dynamics Laboratory, Kettering University, 1700 West Third Avenue, Flint, MI 48504

2003-014: MULTI-FLUID SHEATH MODEL FOR ELECTRIC PROPULSION DEVICES; Subrata Roy and B. P. Pandey, Computational Plasma Dynamics Laboratory, Kettering University, 1700 West Third Avenue, Flint, MI 48504

2003-015: OPTIMIZATION ON MAGNETIC FIELD AND ACCELERATION CHANNEL FOR LOW POWER HALL THRUSTERS; Hirokazu Tahara, Takashi Fujioka, Takahisa Kitano, Atsushi Shirasaki, and Takao Yoshikawa, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan; Kenji Fuchigami and Fumihiro Ueno, Fujio Iinoya, and,

2003-016: SIMPLE ONE-DIMENSIONAL CALCULATIONS OF HALL THRUSTER FLOWFIELDS; Hirokazu Tahara, Takashi Fujioka, Atsushi Shirasaki and Takao Yoshikawa, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan; Kenji Fuchigami and Fumihiro Ueno, Technical Research Laboratory, Ishikawajima-Harima Heavy Industries Co., Ltd., 1, Shinnakahara Ishogo, Yokohoma, Kanagawa 235-8501, Japan; Fujio Iinoya, Technologies Development Department, IHI Aerospace Co., Ltd., 1, Shinnakahara, Ishogo, Yokohama, Kanagawa 235-8501, Japan

2003-017: PLASMA CHARACTERISTICS OF QUASI-STEADY MPD ARCJETS FOR MATERIAL PROCESSING; Hirokazu Tahara, Tetsuji Shibata, Kazunori Mitsuo, Atsushi Shirasaki, Yoichi Kagaya, and Takao Yoshikawa, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

2003-019: TRACEABLE, HIGH-ACCURACY THRUST MEASUREMENT FOR ELECTRIC PROPULSION; E. B. Hughes and S. Oldfield, National Physical Laboratory, Queens Road, Teddington, Middlesex, TW11 0LW, UK

2003-021: THERMAL MODELING AND MEASUREMENTS OF AN ENGINEERING MODEL HALL THRUSTER; A. Warshavsky, Manor Division, Rafael, Haifa 31021, Israel; I. Zur, Mechanical CAD Division, Rafael, Haifa 31021, Israel; J. Ashkenazy and G. Appelbaum, Propulsion Physics Laboratory, Soreq NRC, Yavne 81800, Israel

2003-022: COMPARISON OF ORBIT TRANSFER VEHICLE CONCEPTS UTILIZING MID-TERM POWER AND PROPULSION OPTIONS; Frank S. Gulczinski III, AFRL Propulsion Directorate (AFRL/PRSS), 1 Ara Road, Edwards AFB, CA 93524-7013; John H. Schilling, W. E. Research, 4360 San Juan Ct., Rosamond, CA 93560

2003-024: THE GEAR OF A WORKING GAS FLOW IN THE SPT DISCHARGE CHAMBER; Sergey A. Oghienko and Anatoliy I. Oranskiy, Scientific and Technological Center of Space Power and Engines at Kharkov Aviation Institute, 17, Chkalova St., Kharkov, 61070, Ukraine

2003-027: NUMERICAL SIMULATION OF THE HOLLOW CATHODE PLASMA USING A PIC-DCMC CODE; Francis T. Crawford and Stephen B. Gabriel, School of Engineering Sciences, University of Southampton, UK

2003-028: MOMENTUM AND HEAT FLUX MEASUREMENTS IN THE EXHAUST OF VASIMR USING HELIUM PROPELLANT; D. Gregory Chavers, Research Scientist, Propulsion Research Center, MSFC/NASA, Huntsville, AL; Franklin R. Chang-Díaz, NASA Astronaut, ASPL Director, JSC/NASA, Houston, TX; Claude Irvine, Research Scientist, Propulsion Research Center, MSFC/NASA, Huntsville, AL; Jared P. Squire, Research Scientist, Advanced Space Propulsion Laboratory, Muniz Engineering, Houston, TX

2003-030: INTERACTIONS WITHIN A CLUSTER OF LOW POWER HALL THRUSTERS; W. A. Hargus, Jr., AFRL/PRSS, 1 Ara Road, Edwards AFB, CA, USA

2003-031: EFFECT OF APPLIED MAGNETIC NOZZLE IN A QUASI-STEADY MPD THRUSTER; Yoichi Kagaya, Hirokazu Tahara, and Takao Yoshikawa, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

2003-032: DEVELOPMENT AND TESTING FOR A HIGH-POWER HALL THRUSTER; Olivier Duchemin and Pierre  Dumazert, SNECMA Moteurs, Space Propulsion Division, Spacecraft Propulsion and Equipment, Villaroche Nord, 77550 Moissy-Cramayel, France; S. D. Clark and D. H. Mundy, Space Propulsion, QinetiQ, Farnborough, Hampshire, GU14 0LX, The United Kingdom

2003-033: NUMERICAL SIMULATION OF THE ARTUER-2 ARCJET; J. Heiermann and M. Auweter-Kurtz, Institut für Raumfahrtsysteme, Universität Stuttgart, Pfaffenwaldring 31, 70550 Stuttgart, Germany

2003-034: ANALYSIS OF HALL-EFFECT THRUSTERS AND ION ENGINES FOR EARTH-TO-MOON TRANSFER; A. Bober and M. Guelman, Asher Space Research Institute, Technion-Israel Institute of Technology, 32000 Haifa, Israel

2003-035: ENERGY ANALYSIS OF A HALL THRUSTER CLUSTER; Brian E. Beal and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, The University of Michigan, Ann Arbor, MI 48109

2003-036: END TO END OPTIMIZATION OF THREE DIMENSIONAL CHEMICAL-ELECTRIC ORBIT RAISING MISSIONS; David Y. Oh and Scott Kimbrel, Space Systems/Loral, 3825 Fabian Way M/S G-80, Palo Alto, CA 94303-4604; Manuel Martinez-Sanchez, Massachusetts Institute of Technology, 77 Massachusetts Avenue, Cambridge, MA 02139

2003-037: RECENT RESULTS FROM INTERNAL AND VERY-NEAR-FIELD PLASMA DIAGNOSTICS OF A HIGH SPECIFIC IMPULSE HALL THRUSTER; Richard R. Hofer, QSS Group, Inc., Cleveland, OH 44135, USA; Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, MI 48109, USA

2003-038: SENSITIVITY OF THE BEHAVIOR OF BACKFLOW CEX IONS TO ION ENGINE PLUME CHARACTERISTICS; M. Matsushiro and M. Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-8581, Japan; H. Kuninaka and K. Toki, Institute of Space and Astronautical Science, Sagamihara, Kanagawa 229-8510, Japan

2003-039: PROPELLANT ENERGY FLUX MEASUREMENTS IN PULSED PLASMA THRUSTER; Y. A. Alexeev, N. N. Kazeev, and V. F. Kozlov, Russian Research Centre “Kurchatov Institute”, 1, Kurchatov sq., Moscow, 123182, Russia

2003-040: PULSED PLASMA THRUSTER PROPULSION TECHNOLOGY FOR SMALL SATELLITE; Garry A. Popov and Nikolay N. Antropov, Research Institute of Applied Mechanics and Electrodynamics, 4, Volokolamskoye shosse, Moscow, 125810, Russia; Michael N. Kazeev, Russian Research Centre Kurchatov Institute, 1, Kurchatov sq., Moscow, 123182, Russia; Vladimir P. Khodnenko and Yakov V. Dubrovinskyi, All-Russian Research Institute of Electromechanics, 101000, P.O. Box 496, Moscow, Russia

2003-041: FUNCTIONALLY GRADED THERMAL BARRIER COMPOSITE COATINGS FORMED BY GAS TUNNEL TYPE PLASMA SPRAYING; Akira Kobayashi, JWRI, Osaka University, 11-1 Mihogaoka, Ibaraki, Osaka 567-0047, Japan

2003-043: PULSED PLASMA THRUSTERS FOR SPACE PROPULSION AND INDUSTRIAL PROCESSING; Henri P. Wagner and Monika Auweter-Kurtz, Institut für Raumfahrtsysteme, Universität Stuttgart

2003-048: STENTOR PLASMA PROPULSION SYSTEM EXPERIENCE; Pascal Garnero and Thierry Grassin, ALCATEL SPACE, 100 Bd du Midi, 06159 Cannes, France; F rank Darnon and Luc Petitjean, CNES, Centre Spatial de Toulouse, 18 av. E. Belin, 31401 Toulouse, France

2003-050: TRAJECTORY SIMULATION FOR THRUST-VECTORED ELECTRIC PROPULSION MISSIONS; N. Leveque, C. Welch, A. Ellery, and A. Curley, Kingston University, Astronautics and Space Systems Group, School of Engineering, Friars Avenue, London SW 15 3DW, UK

2003-051: OPERATIONAL CHARACTERISTICS OF CYLINDRICAL HALL THRUSTERS; Atsushi Shirasaki, Hirokazu Tahara, and Takao Yoshikawa, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

2003-052: ANGULAR DISTRIBUTION OF CERAMIC ISOLATOR SPUTTERED MATERIAL IN THE SPT JET; S. A. Khartov, A. B. Nadiradze, and Yu V. Zikeeva, Moscow Aviation Institute (State Technical University) MAI, Electric Propulsion and Space Power Plants Department, 4, Volokolamskoe sh., Moscow, 125971, Russia; V. K. Egorov, IPMT RAS, Chernogolovka, Moscow Region, Russia

2003-053: INTERACTION BETWEEN HIGH VOLTAGE SOLAR ARRAY AND ION THRUSTER PLASMA; Mengu Cho, Akiyo Saionji, and Kazuhiro Toyoda, Kyushu Institute of Technology; Yukishige Nozaki, NEC Toshiba Space Systems, Ltd., Tetsuo Sato, National Space Development Agency of Japan

2003-056: NOZZLE SHAPE EFFECTS ON VELOCITY DISTRIBUTION IN AN MPD ARCJET; Kiyoshi Kinefuchi and Kyoichiro Toki, Institute of Space and Astronautical Science, Kanagawa, Japan; Ikkoh Funaki, Institute of Engineering Mechanics and Systems, University of Tsukuba, Ibaraki, Japan

2003-057: MICROWAVE HALL THRUSTER DEVELOPMENT; Pedro Molina-Morales, Hitoshi Kuninaka, and Kyoichiro Toki, Institute of Space and Astronautical Science (ISAS), 3-1-1 Yoshinodai, Sagamihara, Kanagawa, 229-8510, Japan; Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

2003-058: INVESTIGATION OF DIFFERENT SCHEMES OF GAS DISTRIBUTION IN SPT CHANNEL; Sergey A. Khartov and Alexander B. Perfiliev, Moscow Aviation Institute (State Technical University) MAI, Electric Propulsion and Space Power Plants Department, 4, Volokolamskoe sh., Moscow, 125971, Russia

2003-059: SPT CERAMIC ISOLATOR SURFACED LAYER COMPOSITION CHANGE WITH LIFETIME; Sergey Khartov and Andrey Nadiradze, Moscow Aviation Institute (State Technical University) MAI, Electric Propulsion and Space Power Plants Department, 4, Volokolamskoe sh., Moscow, 125971, Russia; Olivier Duchemin and Snecma Moteurs, Villaroche Nord Plant, Arodrome de Melun-Villaroche 77550, Moissy-Cramayel-France

2003-060: THE RELIABILITY OF THE ELECTRIC PROPULSION PARAMETERS MEASUREMENT INCREASING; S. A. Khartov, L. A. Latyshev, and D. U. Silantiev, Moscow Aviation Institute (technical university) MAI, Electric Propulsion and Space Power Plants Department, 4, Volokolamskoe sh., Moscow, 125971, Russia

2003-061: DEVELOPMENT AND REFINEMENT OF HIGHLY EFFICIENT 150 J APPT; N. Antropov, G. Diakonov, M. Orlov, G. Popov, V. Tyutin, and V. Yakovlev, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), 5, Leningradskoye shosse, post box 43, Moscow, 125080, Russia

2003-062: 30MN-CLASS MICROWAVE DISCHARGE ION THRUSTER; Kazutaka Nishiyama, Hitoshi Kuninaka, Yukio Shimizu, and Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2003-063: ANALYSIS OF THE PLUME DIVERSION IN THE HALL THRUSTER IN THE NEAR AND FAR FIELDS; Avi Cohen-Zur and Alon Gany, Faculty of Aerospace Engineering, Technion – Israel Institute of Technology, Haifa 32000, Israel; Amnon Fruchtman, Holon Academic Institute of Technology, P. O. Box 305, Holon 58102, Israel

2003-064: A SIMILARITY PARAMETER FOR CAPILLARY FLOWS OF RELEVANCE TO MICROPROPULSION; Kurt A. Polzin and Edgar Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey 08544

2003-065: EFFECTS OF ION COLLISIONS ON ION ACCELERATION BY BEATING ELECTROSTATIC WAVES; R. Spektor and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey 08544

2003-067: HIGH POWER PROCESSING UNIT FOR STATIONARY PLASMA THRUSTER; E. Bourguignon and T. Scalais, Alcatel ETCA s.a., BP 4008, B-6000, Charleroi (Belgium)

2003-069: DISCHARGE PLASMA PARAMETERS OF A 30-cm ION THRUSTER MEASURED WITHOUT BEAM EXTRACTION USING A HIGH-SPEED PROBE POSITIONING SYSTEM; Daniel A. Herman, Daniel S. McFarlane, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, MI 48105, USA

2003-070: NUMERICAL SIMULATION OF TWO-DIMENSIONAL, NON-STEADY IDEAL MAGNETOGASDYNAMICS EQUATIONS; Livio S. Maglione, Facultad de Ingeniería, Universidad Nacional de Río Cuarto; Sergio A. Elaskar, Department de Aeronáutica, Universidad Nacional de Córdoba, Av. Velez Sarfield 1601, Córdoba (5000), Argentina, Centro de Investigaciones Aplicadas, Instituto Universitario Aeronáutico, Ruta 20, km. 5.5, Córdoba (5022), Argentina; Héctor H. Brito, Centro de Investigaciones Aplicadas, Instituto Universitario Aeronáutico, Ruta 20, km. 5.5, Córdoba (5022), Argentina

2003-071: COMPUTATIONAL MODEL OF AN SPT-100 THRUSTER; Justin W. Koo and Iain D. Boyd, Nonequilibrium Gas and Plasmadynamics Group, Department of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan 48109

2003-072: CHARACTERISTICS OF ENERGETIC IONS EMITTED FROM HOLLOW CATHODES; Casey C. Farnell, John D. Williams, and Paul J. Wilbur, Department of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523

2003-073: NUMERICAL SIMULATION OF ION THRUSTER OPTICS; Cody C. Farnell, John D. Williams, and Paul J. Wilbur, Department of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523

2003-075: DISCHARGE CHARACTERISITICS OF A LASER-ASSISTED PLASMA THRUSTER; Hideyuki Horisawa, Masatoshi Kawakami, Wun-Wei Lin, and Akira Igari, Department of Aeronautics and Astronautics, Tokai University, 1117 Kitakaname, Hiratsuka, Kanagawa, 259-1292, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo, 113-8856, Japan

2003-077: HOT FLOW PRESSURE MAP OF A VACUUM FACILITY AS A FUNCTION OF FLOW RATE TO STUDY FACILITY EFFECTS; Mitchell L. R. Walker and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, University of Michigan, College of Engineering, Ann Arbor, MI 48109, USA

2003-078: DISCHARGE CHARACTERISTICS OF A VERY LOW-POWER ARCJET; Hideyuki Horisawa and Hotaka Ashiya, Department of Aeronautics and Astronautics, Tokai University, 1117 Kitakaname, Hiratsuka, Kanagawa, 259-1292, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo, 113-8856, Japan

2003-079: HIGH ACCURACY MULTI-COLOR PYROMETRY FOR HIGH TEMPERATURE SURFACES; L. D. Cassady and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey, 08544

2003-082: CHARACTERIZATION OF A HIGH SPECIFIC IMPULSE HALL THRUSTER USING ELECTROSTATIC PROBES; Noah Z. Warner and Manuel Martinez-Sanchez, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, 77 Massachusetts Ave., Cambridge, MA 02139, USA; James J. Szabo, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760, USA

2003-083: ION THRUSTER THRUST VECTORING BY GRID TRANSLATION; Yasushi Okawa, Japan Society for the Promotion of Science, Yukío Hayakawa, Katsuhiro Miyazaki, and Shoji Kitamura, National Aerospace Laboratory of Japan

2003-084: ULTRA-LIGHT CONCENTRATORS FOR SOLAR THERMAL PROPULSION; Hironori Sahara, Japan Society for the Promotion of Science (JSPS), 7-44-1, Jindaiji-Higashi-Machi, Chofu, Tokyo 182-8522, Japan; Shinsuke Ezaki, Yasuhiro Matsui, and Yoshihiro Nakamura, Hosei University; Morio Shimizu, National Aerospace Laboratory of Japan (NAL)

2003-085: SOLAR THERMAL PROPULSION FOR MICROSATELLITES END-OF-LIFE DE-ORBITING; Hironori Sahara, Japan Society for the Promotion of Science (JSPS), NAL, 7-44-1, Jindaiji-Higashi-Machi, Chofu, Tokyo, 182-8522, Japan; Morio Shimizu, National Aerospace Laboratory of Japan (NAL); 7-44-1, Jindaiji-higashimachi, Chofu, Tokyo, 182-8584, Japan; Keitaro Osa, Kai Watanabe, and Yoshihiro Nakamura, Hosei University, 3-7-2, Kajino-Cho, Koganei, Tokyo, 184-8584, Japan

2003-086: CONDITION OF STABLE OPERATION IN A HALL THRUSTER; Naoji Yamamoto, Kimiya Komurasaki, and Yoshihiro Arakawa, University of Tokyo, Hongo 7-3-1, Bunkyo-ku, Tokyo, 113-8656, Japan

2003-087: LIQUID PROPELLANT PULSED PLASMA THRUSTER; H. Koizumi, A. Kakami, Y. Furuta, K. Komurasaki, and Y . Arakawa, The University of Tokyo, Department of Aeronautics and Astronautics, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

2003-088: EXPERIMENTAL INVESTIGATION OF THE THRUST PERFORMANCE OF ATTILA; Stefan Laure, Dr. Laure Plasmatechnologie GmbH, Stuttgart, Germany; Jörg Heiermann, Monika Auweter-Kurtz and Helmut Kurtz, Institut für Raumfahrtsysteme (IRS), Universität Stuttgart, Germany

2003-089: STUDY OF A PLASMA SAIL FOR FUTURE DEEP SPACE MISSIONS; I. Funaki, Institute of Engineering Mechanics and Systems, University of Tsukuba, Tsukuba, Ibaraki, 305-8573, Japan; H. Yamakawa, K. Fujita, H. Ogawa, S. Nonaka, S. Sawai, and H. Kuninaka, The Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan; H. Otsu, Faculty of Engineering, Shizuoka University, Hamamatsu, Shizuoka, 432-8561, Japan

2003-092: FEASIBILITY STUDY OF A LOW-POWER APPLIED-FIELD MPD ARCJET; Tetsuaki Nakano and Atsushi Ishiyama, Waseda University, 3-4-1 Ohkubo, Shinjuku, Tokyo, Japan; Yukio Shimizu and Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2003-093: SINGLE IMPULSE MEASUREMENT OF A COAXIAL PULSED PLASMA THRUSTER; Masahiko Kameoka and Haruki Takegahara, Tokyo Metropolitan Institute of Technology, Dept. of Aerospace Eng., 6-6, Asahigaoka, Hino, Tokyo 191-0065, Japan; Yukio Shimizu and Kyoichiro Toki, Institute of Space and Astronautical Science, Japan, 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2003-095: AN ANALYTICAL STUDY OF THE THRUST IN MPD THRUSTERS; Luigi Petrucci, Space Propulsion Laboratory, University of Rome “La Sapienza”, Via Eudossiana 18, 00184 Rome, Italy

2003-096: ARTEMIS ORBIT RAISING IN-FLIGHT EXPERIENCE WITH ION PROPULSION; Rainer Killinger and Ralk Kukies, Astrium GmbH, 74215 Lampoldshausen, Germany; Michael Surauer, Astrium GmbH, 81663 München, Germany; Howard Gray and Ray Dunster, Astrium Ltd., Portsmouth, United Kingdom; Giorgio Saccoccia, European Space Agency – ESTEC, Noordwijk, The Netherlands; Angelo Tomasetto, Alenia Spazio, Roma, Italy

2003-097: EVALUATIOIN OF NEW CARBON-CARBON COMPOSITE MATERIAL FOR A 20 CM ION ENGINE; Y. Shimizu, H. Kuninaka, K. Nishiyama, and K. Toki, The Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2003-098: FLIGHT READINESS OF THE MICROWAVE ION ENGINE SYSTEM FOR MUSES-C MISSION; Kyoichiro Toki, Hitoshi Kuninaka, Kazutaka Nishiyama, and Yukio Shimizu, The Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2003-100: ELECTRON INSTABILITIES IN HALL THRUSTERS: MODELING AND APPLICATION TO ELECTRIC FIELD DIAGNOSTICS; A. Kapulkin, A. Kogan, D. Alkalay, and M. Guelman, Asher Space Research Institute, Technion, I.I.T., Haifa, 32000, Israel; J. Ashkenazy and G. Appelbaum, Propulsion Physics Laboratory, Soreq, NRC, Yavne 81800, Israel

2003-103: STUDY OF THE HALL THRUSTER DISCHARGE WITH AN INTERMEDIATE ELECTRODE; B. Navazo and E. Ahedo, Univ. Politécnica de Madrid, Spain

2003-104: SCALING DOWN HALL THRUSTERS; E. Ahedo and J. M. Gallardo, E.T.S.I. Aeronáuticos, Universidad Politécnica de Madrid, Spain

2003-107: PLASMA PARAMETER DISTRIBUTION DETERMINATION IN SPT-70 PLUME; Vladimir Kim, Vyacheslav Kozlov, Garry Popov, and Alexander Skyrlnikov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), 5, Leningradskoye shosse, p.b. 43, Moscow, 125080, Russia

2003-110: NUMERICAL ANALYSIS OF NEXT ION THRUSTER OPTICS; Jerold W. Emhoff, Graduate Student Research Assistant; Iain D. Boyd, Professor; Steven P. Shepard, Undergraduate Student, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109

2003-112: INVESTIGATION OF A PPT UTILIZING WATER AS A COMPONENT PROPELLANT; Carsten A. Scharlemann and Thomas M. York, The Ohio State University, Aero/Astro Laboratory, 2300 West Case, Columbus, OH 43235; Peter J. Turchi, Los Alamos National Laboratory, Mail Stop D410. Los Alamos, NM 87545

2003-114: OPTIONS AND RISK FOR QUALIFICATION OF ELECTRIC PROPULSION SYSTEMS; Michelle Bailey, NASA/MSFC, Mail Code ED20, Marshall Space Flight Center, AL 35812, USA; Charles Daniel, 3418 Wildwood Drive, Huntsville, AL 35801, USA

2003-115: DEVELOPMENT AND PERFORMANCE OF THE ADVANCED RADIO FREQUENCY ION THRUSTER RIT-XT; Hans J. Leiter, Rainer Killinger, Helmut Bassner, Johann Müller, Ralf Kukies, and Thomas Fröhlich, Astrium GmbH, Space Infrastructure, Post Box 11 19, D-74215 Möckmühl, Germany

2003-116: PLASMA MODELING OF A HOLLOW ANODE FOR AN ANODE LAYER TYPE HALL THRUSTER; Ken Kumakura and Kimiya Komurasaki, Department of Advanced Energy, The University of Toyko; Shinsuke Yasui and Yoshihiro  Arakawa, Department of Aeronautics and Astronautics, The University of Tokyo, Hongo 7-3-1, Bunkyo, Tokyo 113-8656, Japan

2003-118: PROPELLANTS BEYOND XENON FOR RADIO FREQUENCY ION THRUSTER OPERATION; Hans J. Leiter, Astrium GmbH, IP 47, 81663 Munich, Germany

2003-120: PROBE MEASUREMENTS IN DISCHARGE CHAMBER OF LOW-POWER ION THRUSTER; M. V. Zikeyev and A. A. Shagayda, Keldysh Research Center, 125438, Russia, Moscow, Onezhskaya, 8/10

2003-121: OPERATION PRECULIARITIES OF HALL THRUSTER WITH POWER 1.5-2.0 KW AT HIGH DISCHARGE VOLTAGES; M. B. Belikov, N. V. Blinov, O. A. Gorshkov, R. N. Rizakhanov, and A. A. Shagayda, Keldysh Research Center, 125438, Moscow, Onezhskaya 8

2003-122: TWO KILOWATT BIPROPELLANT ARCJET DEVELOPMENTS; Kurt Hohman, Thomas Brogan, and Vladimir Hruby, Busek Company, Inc, 11 Tech Circle, Natick, MA 01760, USA; Kurt Annen and Robert Brown, Aerodyne Research Inc., 45 Manning Road, Billerica, MA 01821

2003-123: EXPENDING PLASMA JET FROM THE NOZZLE OF THE RF-PLASMA THRUSTER; Leonid A. Bazyma, National Aerospace University, “Kharkov Aviation Institute” 17 Chkalov Street, Kharkov, 61070, Ukraine; Vasyl M. Rashkovan, Instituto Politecnico Nacional de Mexico, ESIME-Culhuacan, Av. Santa Ana 1000

2003-124: INDUCTIVE PULSED THRUSTER WITH SUPERCONDUCTING ACCELRATING ELEMENTS; Vasyl Rashkovan, Iryna Ponomaryova and Omar J. Ramirez, Instituto Politécnico Nacional de México, ESIME-CULHUACAN, Av. Santa Ana, 1000, C.P.04430, México; Andrey Dashkov, National Aerospace University of Ukraine (KhAI), 17 Chkalov Street, Kharkov, 61070, Ukraine

2003-125: DEVELOPING SPACE STATION-BASED DEMONSTRATION FOR THE VASIMR PLASMA ROCKET; Andrew Petro, Franklin Change Díaz, Jared P. Squire, and Andrew Ilin, Advanced Space Propulsion Laboratory, NASA Johnson Space Center, Houston, Texas, USA

2003-126: FEASIBILITY STUDY OF AN ACTIVE PLASMA EXPERIMENTAL PLATFORM IN JAPANESE EXPERIMENTAL MODULE ONBOARD THE ISS; Ikkoh Funaki, Institute of Engineering Mechanics and Systems, University of Tsukuba, Tsukuba, Ibaraki, 305-8573, Japan; Hideyuki Usui and Hayato Tashima, Radio Science Center for Space and Atmosphere, Kyoto University, Uji, Kyoto, 611-0011, Japan; Hitoshi Kuninaka, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa, 229-8510, Japan; Masaki Okada, National Institute of Polar Research, 1-9-10 Kaga, Itabashi, Tokyo, 173-8512, Japan; and Yoshinori Nakayama, National Defense Academy, Yokoshuka, Kanagawa, 239-8686, Japan

2003-128: EXPERIMENTAL PERFORMANCE LIMITS ON HIGH SPECIFIC IMPULSE ION OPTICS; John D. Williams, D. Mark Laufer, and Paul J. Wilbur, Department of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523

2003-129: ELECTROMAGNETIC EMISSIONS TO 60 GHZ FROM A BPT-4000 EDM HALL THRUSTER; Edward j. Beiting and James E. Pollard, The Aerospace Corporation, Los Angeles, California; Vadim Khayms and Lance Werthman, Lockheed Martin Space Systems Company, Sunnyvale, Caifornia

2003-130: XENON SPUTTER YIELD MEASUREMENTS FOR ION THRUSTER MATERIALS; John D. Williams, Michael M. Gardner, Mark L. Johnson, and Paul J. Wilbur, Department of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523

2003-131: ALCATEL SPACE PLASMA PROPULSION SUBSYSTEM QUALIFICATION STATUS; Pascal Garnero and Olivier Dulau, ALCATEL SPACE, 100, Bd. Du Midi, BP 99, 06156 CANNES LA BOCCA Cedex, France

2003-132: FLIGHT TESTING OF VOLUME-IONIZATION ION THRUSTERS ON METEOR SATELLITE; Vladimir P. Khodnenko, NPP Russian Scientific and Research Institute of Electromechanics, Moscow 101000, P.O. Box 496, Russia

2003-133: EROISION ACTION OF THE SPT JET ONTON SOLAR BATTERIES OF METEOR-PRIDODA SPACECRAFT; Vladimir P. Khodnenko, NPP Russian Scientific and Research Institute of Electromechanics, Moscow 101000, P.O. Box 496, Moscow, Russia

2003-134: HYBRID-PIC SIMULATION OF HALL THRUSTERPLUME ON AN UNSTRUCTURED GRID WITH DSMC COLLISIOINS; Murat Celik, Mark Santi, Manuel Martinez-Sanchez, and Jamie Peraire, Massachusetts Institute of Technology, United States of America

2003-135: PULSED INDUCTIVE THRUSTER (PIT); MODELING AND VALIDATION USING THE MACH2 CODE; Pavlos G. Mikellides, Arizona State University, Tempe, AZ 85287-6106

2003-136: 3-D COMPUTATION OF SURFACE SPUTTERING AND REDEPOSITION DUE TO HALL THRUSTER PLUMES; J. M. Fife, M. R. Gibbons, and W. A. Hargus, U.S. Air Force Research laboratory, Edwards AFB, CA; D. B. VanGilder and D. E. Kirley, ERC, Inc., Edwards AFB, CA; L. K. Johnson, Jet Propulsion Laboratory, Pasadena, CA

2003-137: RADIOISOTOPE ELECTRIC PROPULSION FOR NEW FRONTIERS CLASS MISSIONS; Steven Oleson, Scott Benson, Michael Patterson, Jeffrey Schreiber, National Aeronautics and Space Administration, Glenn Research Center, MS 500-103, 21000 Brookpark Rd, Cleveland, Ohio 4413; Douglas Fiehler, QSS Group, Inc., Cleveland, Ohio

2003-138: DEVELOPMENT OF A MICRO-FABRICATED COLLOID THRUSTER ARRAY; Luis Fernando Velásquez García, PhD Candidate, Aeronautics and Astronautics, MIT; Manuel Martínez-Sánchez, Professor, Aeronautics and Astronautics, MIT; Akintunde I. Akinwande, Professor, Electrical Engineering and Computer Science, MIT

2003-139: PRELIMINARY RESULTS OF PLASMA FLOW MEASUREMENTS IN A 2 KW SEGMENTED HALL THRUSTER; Y. Raitses, D. Staack, A. Dunaevsky, L. Dorf, and N. J. Fisch, Princeton University Plasma Physics Laboratory, Princeton, NJ 08543

2003-140: INSTRUMENT DESIGN AND ANALYSIS FOR DIAGNOSIS OF A HALL THRUSTER PLUME FOR THE ETEEV SHUTTLE EXPERIMENT; Yassir Azziz and Manaul Martinez-Sanchez, Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 77 Massachusetts Avenue, Cambridge, MA 02139

2003-142: THE INFLUENCE OF CURRENT DENSITY AND MAGNETIC FIELD TOPOGRAPHY IN OPTIMIZING THE PERFORMANCE, DIVERGAENCE, AND PLASMA OSCILLATIONS OF HIGH SPECIFIC IMPULSE HALL THRUSTERS; Richard R. Hofer, QSS Group, Inc., Cleveland, OH 44135, USA; Robert S. Jankovsky, NASA Glenn Research Center, Cleveland, OH 44135, USA

2003-146: HIGH POWER MPD THRUSTER DEVELOPMENT AT THE NASA GLENN RESEARCH CENTER; Michael R. LaPointe, Ohio Aerospace Institute, 22800 Cedar Point Road, Cleveland, OH 44142

2003-150: HELICON WAVE PHYSICS IMPACTS ON ELECTRODELESS THRUSTER DESIGN; James Gilland, OAI, 22800 Cedar Point Rd., Brookpark, OH 44142

2003-154: THRUST MEASUREMENTS OF A MESO-SCALE HOLLOW CATHODE DISCHARGE; Andrew J. Jamison, Joseph Landon, Joshua A. Cripps, University of Southern California, Department of Aerospace and Mechanical Engineering, Los Angeles, CA 90089-1191; Andrew D. Ketsdever, Air Force Research Laboratory, Propulsion Directorate, Edwards AFB, CA 93524; Joseph Wang, Virginia Polytechnic Institute & State University, Dept. Aerospace and Ocean Engineering, Blacksburg, VA 24061-0203

2003-156: ENHANCED IONIZATION IN THE CYLINDRICAL HALL THRUSTER; A. Smirnov, Y. Raitses, and N. J. Fisch, Princeton University Plasma Physics Laboratory, P.O. Box 451, Princeton, New Jersey 08543

2003-157: DIAGNOSTIC SETUP FOR CHARACTERIZATION OF NEAR-ANODE PROCESSES IN HALL THRUSTERS; L. Dorf and Y. Raitses, Princeton Plasma Physics Laboratory (PPPL), Princeton, NJ, 08543

2003-158: NASA’S ELECTRIC PROPULSION PROGRAM; John W. Dunning Jr., Scott Benson, and Steven Oleson, National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field, Cleveland, Ohio, USA 44135

2003-159: NUMERICAL FEASIBILITY DESIGN CODE OF ION THRUSTER; Yoshinori Nakayama, Department of Aerospace Engineering, National Defense Academy, 1-10-20, Hashirimizu, Yokosuka, 239-8686, Japan

2003-160: STUDY ON PLUME CHARACTERISTICS OF PULSED PLASMA THRUSTER; Kentaro Kawahara, Naoki Kumagai, Kensuke Sato, Kohji Tamura, Takahiro Koide, Kenji Harima, Tadanori Fukushima, and Haruki Takegahara, Tokyo Metropolitan Institute of Technology, Department of Aerospace Engineering, Asahigaoka 6-6, Hino, Tokyo, 191-0065, Japan

2003-161: THREE-DIMENSIONAL IN-FEEP PLASMADIAGNOSTICS, M. Tajmar, K. Marhold, and S. Kropatschek, Space Propulsion, ARC Seibersdorf Reseach A-2444 Seibersdorf, Austria

2003-162: KINETIC MODEL OF THE ELECTRON AND ION TRANSPORT IN HALL THRUSTERS; I. Levchenko, National Aerospace University, Kharkov, Ukraine; M. Keidar, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109

2003-163: ENGINE DEVELOPMENT STATUS FOR NEXT: NASA’S EVOLUTIONARY XENON THRUSTER; Michael J. Patterson, John E. Foster, Thomas Haag, Vincent K. Rawlin, and George Soulas, NASA Glenn Research Center, 21000 Brookpark Rd. Cleveland, Ohio 44135; Robert F. Roman, QSS Group, Inc.

2003-164: YIELD OF SECONDARY ELECTRON EMISSION FROM CERAMIC MATERIALS OF HALL THRUSTER WITH SEGMENTED ELCTRODES; A. Dunaevsky, Y. Raitses, and N. J. Fisch, Plasma Physics Laboratory, Princeton University, P.O. Box 451, Princeton, NJ 09543, US

2003-165: RESEARCH AND DEVELOPMENT OF 150-MN XENON ION THRUSTER; Shoji Kitamura, Yukio Hayakawa, Katsuhiro Miyazaki, and Hideki Yoshida, National Aerospace Laboratory of Japan, Chofu, Tokyo 182-8522, Japan; Kenichi Kajiwara, National Space Development Agency of Japan, Tsukuba, Ibaraki 305-8505, Japan; Kouseki Akai, NEC Toshiba Space Systems, Yokohoma, Kanagawa 224-8555, Japan

2003-166: THE AZIMUTHAL BEAM-PLASMA INSTABILITIES IN STATIONARY PLASMA THRUSTERS; K. Makowski and S. Barral, Institute of Fundamental Technological Research – IPPT-PAN, Swietokrzyska 11/21, 00-049 Warsaw, Poland; Z. Peradzynski, Institute of Fundamental Technological Research – IPPT-PAN, Swietokrzyska 11/21, 00-049 Warsaw, Poland, Institute of Applied Mathematics & Mechanics, Warsaw University, Banacha 2, 02-697 Warsaw, Poland; M. Dudeck, Laboratoire d’ Aérothermique du CNRS, 1C av. de la Recherches Scientifiques, 45000 Orléans, France

2003-167: SOLUTIONS WITH SHOCKS FOR FLUID MODEL OF STATIONARY PLASMA THRUSTER; Zbigniew Peradzynski, Serge Barral, and Karol Makowski, Institute of Fundamental Technological Research – PAS, Swietokrzyska 21, 00-049 Warsaw, Poland, Institute of Applied Mathematics and Mechanics, Warsaw University, Banacha 2, 02-097 Warsaw, Poland; Michael Dudeck, CNRS Laboratoire d’ Aérothermique, 45071 Orléans, France

2003-168: PRELIMINARY INVESTIGATION OF HELICON PLASMA SOURCE FOR ELECTRIC PROPULSION APPLICATIONS; Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan; Shunjiro Shinohara, Interdisciplinary Graduate School of Engineering Sciences, Kyushu University, 6-1 Kasuga-Koen, Kausga, Fukuoka 816-8580, japan; Takao Tanikawa, Research Institute of Science and Technology, Tokai University, 2-28-4 Tomigaya, Shibuya-ku, Tokyo 151-0064, Japan; Ikkho Funaki, Institute of Engineering Mechanics and Systems, University of Tsukuba, 1-1-1, Ten-nodai, Tsukuba, Ibraki 305-8577, Japan; Konstantin P. Shamrai, Scientific Center Institute for Nuclear Research, National Academy of Sciences, 47 Prospeckt Nauki, Kiev 28, 03680 MSP, Ukraine

2003-169: AN OVERVIEW OF THE CNES ELECTRIC PROPULSION PROGRAM; Anne Cadiou, Franck Darnon, and Laurent Jolivet, CNES, 18 Avenue Edouard Belin, 31401 Toulouse Cedex 4

2003-170: ELECTRIC PROPULSION ON @BUS PLATFORM; Michel Lyszyk, @Bus Alcatel-Astrium JPT, Alcatel Space 100 Boulevard du Midi 06156, Cannes la Bocca Cedex, France; Vincent Jacod, @Bus Alcatel-Astrium JPT, Astrium Space 31 Rue des Cosmonautes 31402 Toulouse Cedex 4, France

2003-171: A COMPARISON OF SPUTTERING MODELS FOR PLASMA-SURFACE INTERACTIONS; D. B. VanGilder and D. E. Kirtley, ERC, Inc., Edwards AFB, CA; J. M. Fife and M. R. Gibbons, U. S. Air Force Research Laboratory, Edwards AFB, CA

2003-172: IMPROVED XENON LOADING EQUIPMENT WITH LOADING CAPACITY UP TO 1200 KG FOR ALPHABUS; Patrick Bravais, AIR LIQUIDE DTA; Roland Salome and Cécile Gelas, CNES Toulouse

2003-174: EFFECT OF PLASMA-WALL RECOMBINATION AND TURBULENT RESISTIVITY ON THE CONDUCTIVITY IN HALL THRUSTERS; A. A. Ivanov, RRC Kurhatov Institute, Kurchatov Square 1, 123182 Moscow, Russia; A. A. Ivanov Jr. and M. Bacal, Laboratoire de Physique et Technologie des Plasmas, Ecole Polytechnique, UMR 7648 du CNRS, 91128 Palaiseau, France

2003-176: STUDY OF EXTRACTION GRID EROSION IN A LONG-TIME ION THRUSTER OPERATIONAL TEST; M. Tartz, E. Harmann, and H. Neumann, Institut für Oberflächenmodifizierung e. V., Permoserstr. 15, D-04318 Leipzig, Germany; R. Deltschew, Solarion GmbH Leipzig

2003-180: A COLLOID ENGINE ACCELERATOR CONCEPT UPDATE; D. Kirtley, ERC, Inc., Edwards AFB, CA; J. M. Fife, U. S. Air Force Research Laboratory, Edwards AFB, CA

2003-181: MW-CLASS INDUCTIVE MPD THRUSTER USING NON-UNIFORM GAS-PLASMA FLOW; V. S. Slavin and A. A. Gavrilov, Krasnoyarsk State Technical University, 26 Kirensky Str, Krasnoyarsk, 660074, Russia

2003-183: PARAMETRIC STUDY OF HALL THRUSTER OPERATION BASED ON A 2D HYBRID MODEL: INFLUENCE OF THE MAGNETIC FIELD ON THE THRUSTER PERFORMANCE AND LIFETIME; L. Garrigues, C. Boniface, J. Bareilles, G. J. M. Hagelaar, and J. P. Boeuf, Centre de Physique des Plasmas et Applications, Université Paul Sabatier, 118 Route de Narbonne, 31062 Toulouse cedex, France

2003-184: CRITICAL ASSESSMENT OF A 2D MODEL OF HALL THRUSTERS-COMPARISONS WITH EXPERIMENTS; J. Bareilles, G. J. M. Hagelaar, L. Garrigues, C. Boniface, and J. P. Boeuf, Centre de Physique des Plasmas et Applications, Université Paul Sabatier 118 Route de Narbonne, 31062 Toulouse cedex, France; N. Gascon, Laboratoire d’ Aérothermique, 1C Avenue de la Recherche Scientifique, 45071 Orléans cedex 2, France

2003-185: MODELING OF ION CYCLOTRON WAVES ABSORPTION IN VASIMR; Andrew V. Ilin, Muñiz Engineering, Inc., Advanced Space Propulsion Laboratory, NASA Johnson Space Center, Houston, Texas, 77059, USA; Franklin R. Chang Díaz, Advanced Space Propulsion Laboratory, NASA Johnson Space Center, Houston, Texas, USA; Boris N. Breizman, University of Texas at Austin, Austin, Texas, USA; Mark D. Carter, Oak Ridge National Laboratory, Oak Ridge, Tennessee, USA

2003-186: ACCELERATOR SYSTEMS FOR LONG-LIFE ION THRUSTER OPERATION AT SPECIFIC IMPULSES GREATER THAN 4000 S; John Brophy, Ira Katz, and James Polk, Jet Propulsion Laboratory, California Institute of Technology, MS 125-109, 4800 Oak Grove Drive, Pasadena, CA 91109

2003-187: MODELING A MESO-SCALE HOLLOW CATHODE THRUSTER; Joseph J. Wang, Virginia Polytechnic Institute & State University, Dept. Aerospace and Ocean Engineering, Blacksburg, VA 24061-0203; Andrew D. Ketsdever, Air Force Research Laboratory, Propulsion Directorate, Edwards, AFB, CA 93524; and Andrew J. Jamison, University of Southern California, Department of Aerospace and Mechanical Engineering, Los Angeles, CA 90089-1191

2003-188: CHARGED PARTICLES TRANSPORT IN THE HALL EFFECT THRUSTER; Oleg Batishchev and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, MIT NW 16-232, 167 Albany St. Cambridge, MA 02139, USA

2003-191: VASIMR THRUSTER OPERATION WITH HYDROGEN AND HELIUM GAS PROPELLANTS; Oleg Batishchev and Kim Molvig, Massachusetts Institute of Technology, MIT NW 16-232, 167 Albany St. Cambridge, MA 02139, USA

2003-192: THE DEVELOPMENT OF ION PROPULSION IN THE UK: A HISTORICAL PERSPECTIVE; David G. Fearn, EP Solutions, 23 Bowenhurst Road, Church Crookham, Fleet, Hants, GU52 6HS, UK

2003-193: THE POTENTIAL APPLICATION OF SMALL ELECTRICALLY-PROPELLED SPACECRAFT TO LOW-COST INTERPLANETARY MISSIONA; David G. Fearn, EP Solutions, 23 Bowenhurst Road, Church Crookham, Fleet, Hants, GU52 6HS, UK; Stephen D. Clark, Space Department, Y72 Building, QinetiQ, Farnborough, Hants GU14 OLX, UK

2003-198: STUDY OF ENERGY CONVERSION PROCESS IN CW LASER PROPULSION; Satoshi Hosoda, Kimiya Komurasaki, and Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

2003-202: RESEARCH AND DEVELOPMENT STATUS OF LOW POWER PULSED PLASMA THRUSTER SYSTEM FOR µ-LAB SAT II; Naoki Kumagai, Kensuke Sato, Kohji Tamura, Kentaro Kawahara, Takahiro Koide, and Haruki Takegahara, Tokyo Metropolitan Institute of Technology, Dept. of Aerospace Eng., Asahigaoka 6-6, Hino, Tokyo 191-0065, Japan; Mitsuteru Sugiki, Astro Research Corporation, Kugenuma Tachibana, 1-1-4, Fujisawa, Kanagawa, 251-0024, Japan; Takashi Wakizono, HI-SERVE Corporation, Totohara 780-7, Akiruno, Tokyo, 190-0152, Japan; Hidekazu Hashimoto, National Space Development Agency of Japan, Advanced Mission Research Center, Micro Space Systems Laboratory, Sengen, 2-1-1, Tsukuba, Ibaraki 305-0047, Japan

2003-204: STUDY OF DISCHARGE CHANNEL EROSION IN MULTI MODE ANODE LAYER THRUSTER; A. E. Solodukhin and A. V. Semenkin, Central Research Institute of Machine Building (TSNIIMASH(, Pionerskaya 4, Korolev, Moscow region, Russia 141070

2003-205: SMART-1 PRIMARY ELECTRIC PROPULSION SUB-SYSTEM THE FLIGHT MODEL; Christophe R. Koppel, Snecma Moteurs, Division Moteurs-Spatiaux, Site de Villaroche Nord, Direction Propulsion et Equipements Satellites, Aérodrome de Melun Villaroche; Denis Estublier, ESA/ESTEC, Keplerlaan, 1, Noordwijk, The Netherlands

2003-206: COMPARISON OF MATHEMATICAL MODEL OF A PLASMA PLUME WITH OUTCOMES OF SPACE EXPERIMENTS; A. G. Korsun, F. F. Gabdullin, E. M. Tverdokhlebova, and V. I. Garkusha, Central Research Institute of Machine Building (TSNIIMASH), 141070 Korolev, Moscow region, Russia; V. P. Khodnenko, NPP All-Russian Research Institute of Electromechanics, 101000, P. O. Box 496, Moscow, Russia

2003-207: EXPERIMENTAL AND NUMERICAL COMPARISON OF HIGH POWER STEADY STATE MPD-THRUSTERS WITH RADIATION-AND-WATER-COOLED ANODES; Michael W. Winter, Jörg Heiermann, and Monika Auweter-Kurtz; Institut für Raumfahrtsysteme (IRS), Universität Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Germany

2003-210: A SUMMARY THE QINETIQ HOLLOW CATHODE PROGRAMME IN SUPPORT OF THE ARTEMIS MISSION; N. C. Wallace and H. B. Simpson, Electric Propulsion, Space Department, QinetiQ, Farnborough, Hampshire, United Kingdom, GU14 0LX

2003-211: INVESTIGATION OF THE SPT OPERATION UNDER HIGH DISCHARGE VOLTAGES; Andre Bouchoule, Alexey Lazurenko and Vanessa Vial, GREMI Laboratory, Orleans University, 45067, Orléans cedex 2, France; Vladimir Kim, Vyacheslav Kozlov, and Alexander Skrylnikov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute, 5 Leningradskoye shosse, p/b 43, Moscow, 125080, Russia

2003-212: FIRST TEST RESULTS OF THE HEMP THRUSTER CONCEPT; Günter Kornfeld, Norbert Koch, and Grégory Coustou, Thales Electron Devices GmbH, Söflinger Straße 100, D-89077 Ulm, Germany

2003-213: A DESCRIPTION OF THE NEW 3.8M DIAMETER HIGH POWER ELECTRIC PROPULSION TEST FACILITY AT QINETIQ FARNBOROUGH, UK, H. B. Simpson, N. C. Wallace, S. D. Clark, and D. H. Mundy, QinetiQ, Farnborough, Hampshire, GU14 0LX, The United Kingdom

2003-214: A SUMMARY OF THE QINETIQ HOLLOW CATHODE DEVELOPMENT PROGRAMME IN SUPPORT OF EUROPEAN HIGH POWER HALL EFFECT AND GRIDDED THRUSTERS; H. B. Simpson, N. C. Wallace, D. G. Fearn, and M. K. Kelly, QinetiQ, Farnborough, Hampshire, GU14 0LX, The United Kingdom

2003-216: A STUDY INTO THE TECHNIQUES FOR MINIATURISED ELECTRIC PROPULSION SYSTEMS, AND MISSION CATEGORIES, FOR SMALL SPACECRAFT; Stephen D. Clark, Space Department, Y72 Building, QinetiQ, Farnborough, Hants, GU14 0LX, UK; David G. Fearn, EP Solutions, 23 Bowenhurst Road, Church Crookham, Fleet, Hants, GU52 6HS, UK; Frederic Marchandise, Rocket Engine Division, Satellites Propulsion & Equipment, Aerodrome de Melun, Villaroche, 77550 Moissy-Cramayel, France

2003-218: CHARACTERIZATION OF MICROINST ABILITIES IN HALL THRUSTER PLASMA: EXPERIMENTAL AND PIC CODE SIMULATION RESULTS, PHYSICAL INTERPRETATION AND IMPACT ON TRANSVERSE ELECTRON TRANSPORT; A. Lazurenko, V. Vial, and A. Bouchoule, GREMI, Université d’Orléans, BP 6744, 45067 Orléans, France; M. Prioul, SNECMA, Villaroche Nord, B.P. n°93, F-77552 Moissy-Cramayel Cédex; J. C. Adam, A. Heron, and G. Laval, CPHT, Ecole Polytechnique, route de Saclay, 91128 Palaiseau, France

2003-219: OPTICAL PROBE MEASUREMENTS ON THE INTERNAL PLASMA OF A T6 TYPE HOLLOW CATHODE; S. J. Pottinger and S. B. Gabriel, Astronautics Research Group, University of Southampton SO17 1BJ, United Kingdom

2003-220: PHYSICAL INSIGHTS ON SPT THRUSTERS THROUGH ULTA-FAST, EXTERNALLY DRIVEN CURRENT INTERRUPTIONS; Vanessa Vial, Alexey Lazurenko, and André Bouchoule, GREMI Laboratory, Orléans university, 45067 Orléans Cedex 2; Mathieu Prioul, SNECMA, Direction Propulsion et Equipements Satellites, 77-550, Moissy Cramayel

2003-221: XENON GAS INJECTION IN SPT THRUSTERS; Vanessa  Vial, Alexey Lazurenko, Claude Laure, and André Bouchoule, GREMI, Orléans University, 45067 Orléans Cedex 2, France; Daniel Pagnon, LPGP, Orsay University, 91405 Orsay Cedex, France

2003-222: AUTOMATIC INTERPLANETARY MISSIONS. OPTIMISATION OF A MISSION WITH LOW THRUST STRATEGY; Nicolas Pillet, Sophie Geffroy, and Régis Bertrand, CNES Toulouse, Space Technic’s Directory, Denis Moura, CNES Toulouse, Orbital System Directory; Christophe Talbot, CNES Evry, Launcher Directory; Mikhail  Stepanov, ENSMA, Ecole Nationale Supérieure de Méchanique et d’Aérotechnique

2003-225: PROPULSION INSTRUMENT ELECTRONICS AND SENSOR PACKAGE; Paul B. Adkison, Sverdrup Inc., Edwards AFB, CA 93524; Michael J. Dulligan, ERC, Inc., Edwards AFB, CA 93524; Greg Spanjers and Daron Bromaghim, USAF, Edwards AFB, CA 93524; Rick Harrison and Dale McGehee, Naval Post Graduate School, Monterey, CA 93940; Dave White, W.E. Research, Rosamond, CA 93560; David Conroy and Lee Johnson, Jet Propulsion Laboratory, Pasadena, CA 91109

2003-226: MICRO NEWTON COLLOID THRUSTER SYSTEM DEVELOPMENT FOR ST7; Manuel Gamero-Castaño, Vlad Hruby, Douglas Spence, Charles Gasdaska, and Bill Connolly, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760-1023

2003-227: LOW POWER HALL THRUSTER DEVELOPMENT FOR TECHSAT 21; B. Pote, V. Hruby, M. Gamero-Castaño, G. Kolencik, L. Byrne, R. Tedrake, and W. Connolly, Buseck Co. Inc., 11 Tech Circle, Natick, MA 01760-1023; D. Bromaghim and G. Spanjers, Air Force Research Laboratory, Propulsion Directorate, 1 Ara Road, Edwards AFB, CA 93524-7013

2003-228: DESIGN AND PRELIMINARY CHARACTERIZATION OF A 5 KW HALL THRUSTER PROTOTYPE; L. Biagioni, M. Saverdi, M. Berti, and M. Andrenucci, Centrospazio-CPR, Pisa (Italy); U. Cesari, Alta S.p.A., Via A. della Gherardesca 5, I-56121, Pisa (Italy)

2003-229: THE NEW EP TEST FACILITIES AT CENTROSPAZIO AND ALTA; M. Andrenucci, M. Berti, Centrospazio-CPR, Pisa (Italy); L. Biagioni, U. Cesari, R. Falorni, L. Milaneschi, and M. Saverdi, Alta S.p.a., 56121 Ospedaletto, Pisa (Italy)

2003-230: BASIC ISSUES IN ELECTRIC PROPULSION TESTING AND THE NEED FOR INTERNATIONAL STANDARDS; L. Biagioni, Alta S.p.A. Pisa (Italy); V. Kim, Moscow Aviation Institute, RIAME, Moscow (Russia); D. Nicolini, European Space Agency, ESTEC, TOS-MPE, Noordwijk (The Netherlands); A. V. Semenkin, Central Institute of Machine Building (TsNIIMash), Korolev (Russia; N. C. Wallace, Qinetiq Ltd., Space Dept., Farnborough (United Kingdom)

2003-231: ONE AND TWO DIMENSIONAL MODELING OF THE BHT-1000; James J. Szabo, Peter S. Rostler, Seth A. McElhinney, and Noah Z. Warner; Busek Co. Inc., 11 Tech Circle, Natick, MA 01760, The United States of America

2003-234: EXPERIMENTAL PERFORMANCE OF 1 MN-CLASS FEEP THRUSTERS; Salvo Marcuccio, Marco Saviozzi, Leonardo Priami, and Mariano Andrenucci, Alta S.r.l., Via Gherardesca 5, 56121 Ospedaletto, Pisa, Italy

2003-236: ELECTRIC PROPULSION IN ITALY: STATUS AND PERSPECTIVES; Mariano Andrenucci, Alta S.p.A. / Centrospazio, Via A. Gherardesca 5, 56121 Ospedaletto, Pisa, Italy; Giovanni Matticari, LABEN – Proel Tecnologie Division, Viale Machiavelli 31, 50125 Firenze, Italy

2003-237: PERFORMANCE CHARACTERIZATION OF THE VAPORIZING LIQUID MICRO THRUSTER (VLM); Juergen Mueller, John Ziemer, Amanda Green, and David Bame, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2003-240: PRELIMINARY RESULTS FROM A PERMANENT MAGNET HALL THRUSTER EVALUATION; José Leonardo Ferreira and Ivan Soares Ferreira, Plasma Laboratory of Institute of Physics at University of Brasilia (UnB), ICC- Centro, Campus Universitário Darcy Ribeiro – Asa Norte, 70910-900 Brasília – DF, Brasil

2003-241: THE DESIGN OF MICRONEWTON FEEP THRUSTERS FOR DISTURBANCE REDUCTION SYSTEMS; Salvo Marcuccio, Alta / Centrospazio, Via Gherardesca 5, 56121 Ospedaletto, Pisa, Italy

2003-242: ELECTRIC PROPULSION SYSTEM FOR A MANEUVERABLE ORBITAL VEHICLE; Fabio Ceccanti and Salva Marcuccio, Alta S.p.A / Centrospazio, Via A. Gherardesca 5, 56121 Ospedaletto, Pisa, Italy

2003-243: MODEL OF HOLLOW CATHODE OPERATION AND LIFE LIMITING MECHANISMA; Ira Katz, John R. Anderson, James E. Polk, and Dan M. Goebel, Jet Propulsion Laboratory, Pasadena, CA 91109, USA

2003-244: END-OF-MISSION CHARACTERIZATION OF THE ION THRUSTER ON DS1; John Brophy, Dave Brinza, James Polk, and Mike Henry, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

2003-245: 3-DIMENSIONAL ION OPTICS SIMULATIONS USING AN IFE-PIC CODE; J. Wang, R. Kafafy, and T. Lin, Virginia Polytechnic Institute & State University, Blacksburg, VA 24061-0203

2003-246: APPLICATIONS OF MICROTHRUST SYSTEMS FOR MICROSPACECRAFT, DRAG-FREE, AND PRECISION CONSTELLATION STATIONKEEPING MISSIONS; John K. Ziemer, Juergen Mueller, Colleen M. Marrese, James E. Polk, and Robert F. Shotwell, Jet Propulsion Laboratory, M/S 125-109, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109

2003-247: A NEW ULTA-HIGH VACUUM FACILITY FOR PLUME CHARACTERIZATION AND NEUTRALIZATION STUDIES OF FEEP AND COLLOID THRUSTERS; John K. Ziemer, Colleen M. Marrese, Juergen Mueller and James E. Polk, Jet Propulsion Laboratory, M/S 125-109, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109

2003-250: CONDENSABLE PROPELLANTS AS AN OPTION FOR MULTI KILOWATT SPACE PROPULSION; S. O. Tverdokhlebov, A. V. Semenkin, B. S. Borisov, and F. F. Gabdullin, Central Research Insitute of Machine Building (TsNIIMASH), Russia; C. M. Marrese and J. E. Polk, Jet Propulsion Laboratory, USA

2003-251: DEVELOPMENT OF MICROWAVE ENGINE; S-W. Kim, Y. Aoki, A. Nagata, and T. Kizaki, Advanced Technology Institute, Sapporo, Hokkaido 006-0814, Japan; S. Satori, Hokkaido Institute of Technology, Sapporo, Hokkaido 006-8585, Japan; Y. Itoh, H. Okamoto, and T. M. Sugiki, Astro Research Corporation, Fujisawa, Kanagawa 251-0024, Japan

2003-253: HOLLOW CATHODE THRUST MEASUREMENTS USING A TARGET: INITIAL RESULTS AND SOME ISSUES; Paolo Gessini and Stephen B. Gabriel, Astronautics Research Group, School of Engineering Sciences, University of Southampton, Highfield, Southampton, Hants, SO17 1BJ, United Kingdom; David G. Fearn, EP Solutions, Fleet, Hants, GU14 0LX, United Kingdom

2003-257: EROSION OF MATERIALS USED ON A SATELLITE EXTERNAL SKIN BY ELECTRIC PROPULSION; T. Tondu and V. Viel-Inguimbert, ONERA/DESP 2, Avenue Edouard Belin, 31 055 Toulouse Cédex, France; F. Darnon, CNES 18, Avenue Edouard Belin 31 401 Toulouse Cédex, France

2003-258: SECONDARY ELECTRON EMISSION OF CERAMICS USED IN THE CHANNEL OF SPT; V. Viel-Inguimbert, ONERA/DESP 2, Avenue Edouard Belin, 31 055 Toulouse Cédex France

2003-259: FUNDAMENTAL SCALING LAWS FOR ELECTRIC PROPULSION CONCEPTS; PART 1: HALL EFFECT THRUSTERS; Mariano Andrenucci, Leonardo Biagioni, Salvo Marcuccio, and Fabrizio Paganucci, Alta S.p.A/Centrospazio, Via A. Gherardesca 5, 56121 Ospedaletto, Pisa, Italy

2003-262: DEVELOPMENT OF A CLUSTER OF LOW POWER HALL THRUSTERS; Lawrence Byrne, Bruce Pote, George Kolencik, Rachel Tedrake, and Vlad Hruby, Busek Co. Inc. 11 Tech Circle, Natick, MA 01760-1023

2003-263: AN IMPROVED SMALL CLOSED DRIFT THRUSTER WITH BOTH CONDUCTING AND DIELECT RIC CHANNELS; A. I. Burgrova, A. D. Desiatskov, and V. K. Kharchevnikov, Moscow Institute of Radioelectronics, Moscow, Russia; H. R. Kaufman, Kaufman & Robinson Inc., Fort Collins, CO, U.S.A.; A. I. Morozov, Kurchatov_s Russian Research Center, Moscow, Russia; V. V. Zhurin, Front Range Fakel Inc., Fort Collins, CO, U.S.A.

2003-265: MODELING DEVELOPMENTS ON COLLOID THRUSTERS; Jorge A. Carretero, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139; Francisco J. Higuera, E.T.S. Ingenieros Aeronautics, Madrid Spain; Manuel Martinez-Sanchez, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139

2003-266: OVERVIEW OF ASTRIUM EROSION / CONTAMINATION MODELLING TOOL AND VALIDATION ON ONERA EXPERIMENTAL RESULTS; S. Provost, C. Theroude, and P. Chéoux-Damas, ASTRIUM SAS, 31 avenue des Cosmonautes, 31402 Toulouse Cedex 4 (France)

2003-267: OVERVIEW OF ASTRIUM MODELLING TOOL FOR PLASMIC THRUSTER FLOW FIELD SIMULATION; C. Theroude, S. Provost, and P. Chéoux-Damas, Astrium SASM 31 avenue des Cosmonautes, 31402 Toulouse Cedex 4 (France)

2003-270: PPS -1350-G QUALIFICATION STATUS MARCH 2003; Pierre Dumazert, Sophie Eagardére-Verdier, Frédéric Marchandise, and Christophe R. Koppel, Snecma Moteurs, Division Moteurs-Spatiaux; Pascal Garnero and Francois Balme, Alcatel Space Industries

2003-272: MAGNETIC NOZZLE PLASMA EXHAUST SIMULATION FOR THE VASIMR ADVANCED PROPULSION CONCEPT; A. G. Tarditi and J. V. Shebalin, Advanced Space Propulsion Laboratory, NASA Johnson Space Center, Houston, TX (USA)

2003-273: CONTROL OF THE ACCELERATION REGION IN HALL THRUSTERS; David Staack, Yevgeny Raitses and Nathaniel J. Fisch, Princeton Plasma Physics Laboratory, Princeton, NJ 08543

2003-276: VACUUM ARC THRUSTER FOR CUBESAT PROPULSION; Jochen Schein, Andrew Gerhan, and Mahadevan Krishnan, Alameda Applied Sciences Corporation, San Leandro, CA, USA; Filip Rysanek, University of Illinois Urbana-Champaign, IL, USA

2003-277: MEDIUM AND HIGH CURRENT CATHODES FOR ELECTRIC PROPULSION: REVIEW OF RECENT DEVELOPMENTS AT LABEN/PROEL; J. Bussotti, M. Capacci, G. Matticari, G. E. Noci, A. Severi, and P, Siciliano, LABEN Proel Tecnologie Division, Viale Machiavelli, 31-50125 Firenze (Italy); R. Grill, PLANSEE AG A-6600, Reutte, Tyrol – Austria; D. Estublier, ESA/ESTEC Keplerlaan 1, 2200 AG Noordwijk – The Netherlands

2003-278: A COMPUTATIONAL STUDY OF SINGLE AND DOUBLE STAGE HALL THRUSTERS; Kay  Sullivan, Manuel Martínez-Sánchez, Oleg Batishchev, and James Szabo, Massachusetts Institute of Technology, 77 Massachusetts Avenue, Cambridge, MA 02139

2003-279:  FEEP SYSTEM FOR THE MICROSCOPE MISSION; Salvo Marcuccio and Lorenzo Serafini, Alta S.p.A. / Centrospazio, Via Gherardesca 5, 56121 Ospedaletto, Pisa, Italy; David Nicolini, ESA-ESTEC, Noordwijk, The Netherlands; Laurent Jolivet and Olivier Vandermarcq, CNES, Toulouse, France; Pierre Touboul, ONERA, Chatillon, France

2003-284: MAGNETIC CIRCUITS FOR HALL THRUSTERS; USE OF PERMANENT MAGNETS; P. Renaudin, V. Cagan, and M. Guyot, Laboratoire de Magnétisme et d’Opitque de Versailes, 45 avenue des Etats-Unis, 78035 Versailles, France; A. Cadiou, CNES, 18 avenue Edouard Belin, 31401 Toulouse cedex 4, France; P. Lasgorceix and M. Dudeck; Laboratoire d’ Aéothermique, 1C avenue de la Recherche Scientifique, 45071 Orléans cedex, France; V. Vial, Groupe de Recherche sur l’Energétique des Milieux Ionisés, 12 rue de Blois, 45067 Orléans cedex 2, France; P. Dumazert, SNECMA, Aérodrome de Melun-Villaroche, 77550 Moissy-Cramayel, France

2003-285: CORONAL TYPE AND COLLISIONAL-RADIATIVE MODELLING OF RARE GASES PLASMA; K. Katsonis, A. Siskos, and M. Touzeau, Laboratoire de Physique des Gaz et des Plasmas, UMR 8578, Université Paris-sud 91405 Orsay, France

2003-286: EXPERIMENTAL RESEARCH PROGRESS TOWARD THE VASIMR ENGINE; Jared P. Squire and Verlin T. Jacobson, Muñiz Engineering, Inc., Advanced Space Propulsion Laboratory, NASA Johnson Space Center, Houston, Texas, 77059, USA; Franklin R. Chang Díaz, Advanced Space Propulsion Laboratory, NASA Johnson Space Center, Houston, Texas, USA; Tim W. Glover, Rice University, Advanced Space Propulsion Laboratory, Houston, Texas, USA; F. Wally, and Richard H. Goulding, Oak Ridge National Laboratory, Oak Ridge, Tennessee, USA; Roger Bentson, University of Texas at Austin, Austin, Texas, USA; Edgar A. Bering III, University of Houston, Houston, Texas, USA; Kristy A. Stokke, Massachusetts Institute of Technology, Cambridge, Massachusetts, USA

2003-287: FLOW CHARACTERISTICS OF SUPERSONIC LASER-SPIKE ENGINE; In-Seuck Jeung and Sung-Don Kim, Seoul National University, Seoul 151-744, Korea; Jeong-Yeol Choi, Pusan National University, Pusan 609-735, Korea

2003-288: DEVELOPMENT STATUS OF NEXT: NASA’S EVOLUTIONARY XENON THRUSTER; Scott W. Benson and Michael J. Patterson, NASA Glenn Research Center

2003-289: RADIOFREQUENCY WITH MAGNETIC FIELD ION THRUSTER (RMT): REVIEW OF THE ENGINEERING PHASE ACCOMPLISHED UNDER ASI CONTRACT; M. Capacci, G. Matticari, G. E. Noci, and A. Severi, LABEN Proel Tecnologie Division, Viale Machiavelli, 31-50125, Firenze (Italy); A. Ricciardi and F. Svelto, Italian Space Agency (ASI), Viale Liegi 26-00198 Roma (Italy)

2003-290: RESEARCH ON TWO-STAGE ENGINE SPT-MAG; A. I. Morozov, Kurchatov’s Russia Research Center, Moscow, Russia 123098; A. I. Bugrova, A. D. Desiatskov, and V. K. Kharchevnikov, Moscow Institute of Radioelectronics, Moscow Russia 129110; M. Prioul, SNECMA MOTEURS, Site de Villaroche Nord, BP N°93, 77552 Moissy-Cramayel Cedex, France; L. Jolivet, CNES, 18 avenue Edouard Belin, 31401 Toulouse Cedex 4, France

2003-291: FIELD EMISSION ELECTRIC PROPULSION PLUME EFFECTS ON MICROSCOPE SATELLITE; L. Jolivet and B. Debray, CNES, 18-avenue Edouard Belin, 31401 Toulouse Cedex 4 (France)

2003-292: TIME-RESOLVED SURFACE TEMPERATURE MEASURMENT FOR PULSED ABLATIVE THRUSTERS; Erik L. Antonsen and Rodney L. Burton, University of Illinois at Urbana-Champaign, IL 61801; Gregory G. Spanjers and Ronald A. Spores, AFRL Propulsion Directorate, Edwards AFB CA 93524

2003-293: PHENOMENOLOGICAL MODEL OF CURRENT SHEET CANTING IN PULSED ELECTROMAGNETIC ACCELERATORS; T. E. Markusic, Propulsion Research Center, NASA Marshall Space Flight Center, Huntsville, AL 35812; E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey 08544

2003-294: THEME: ELECTRICAL PROPULSION ON SPACE VEHICLES: ELECTRICAL MOOVING

2003-295: THE DEVELOPMENT AND QUALIFICATION OF A 4.5 KW HALL THRUSTER PROPULSION SYSTEM FOR GEO SATELLITE APPLICATIONS-STATUS UPDATE; J. Fisher, A. Wilson, D. King, S. Meyer, and K. de Grys, Aerojet, P. O. Box 97009, Redmond, VA 98073-9709; L. Werthman, Lockheed Martin Space Systems Company, 1111 Lockheed Martin Way, Sunnyvale, CA 94089

2003-296: CONVERGENCE AND DEFLECTION OF A HALL THRUSTER PLUME; I. Viera, L. Gargaté and J. T. Mendonca, GoLP – Centro de Fisica de Plasmas, Instituto Superior Técnico, Av. Rovisco Pais, 1049-001, Lisboa-Portugal

2003-297: LOW POWER HALL THRUSTER FOR THE ESEO SATELLITE; L. Gargaté and I. Vieira, Instituto Superior Técnico, 1049-001 Lisbon, Protugal; N. Adams, University of Strathclyde – Glasgow, United Kingdom

2003-298: RESONANT OPERATION OF A MICRO-NEWTON THRUST STAND; Capt. James P. Lake, Lt. Greg Cavallaro and Greg Spanjers, AFRL Propulsion Directorate, Edwards AFB, CA 93524; Paul B. Adkison, Sverdrup Inc., Edwards AFB, CA 93524; Michael J. Dulligan, ERC, Inc., Edwards AFB, CA 93524

2003-299: PLASMA FLUCTUATIONS IN A MPD THRUSTER WITH AND WITHOUT THE APPLICATION OF AN EXTERNAL MAGNETIC FIELD; M. Zuin, V. Antoni, G. Regnoli, N. Vianello and M. Bagatin, Consorzio RFX, Associazione Euratom-Enea sulla Fusione, Corso Stati Uniti, 4, I-35127 Padova (Italy), INFM, Unitá di Padova, sez. A, (Italy); F. Paganucci, P. Rossetti, and M. Andrenucci, Centrospazio, Via A. Gherardesca 5, 56014 Pisa (Italy); R. Cavazzana, G. Serianni, and M. Spolaore, Consorzio RFX, Associazione Euratom-Enea sulla Fusione, Corso Stati Uniti, 4, I-35127 Padova (Italy)

2003-301: DIAGNOSTICS OF AN APPLIED FIELD MPD THRUSTER; M. Andrenucci, F. Paganucci, and P. Rossetti, Department of Aerospace Engineering, Univ. of Pisa / Centrospazio, Via A. Gherardesca 5, 56014 Pisa; V. Antoni, M. Bagatin, R. Cavazzana, G. Serianni, and M. Zuin, RFX Consortium, Association Euratom-ENEA on Fusion, Corso Stati Uniti 4, 35127 Padova; M. R. Carraro, A. Cristofolini, and R. Ghidini, Department of Electrical Engineering, University of Bologna, Viale Risorgimento 2, 40136 Bologna

2003-302: PERFORMANCE OF AN APPLIED FIELD MPD THRUSTER WITH A PRE-IONIZATION CHAMBER; Fabrizio Paganucci, Paola Rossetti, and Mariano Andrenucci, CENTROSPAZIO, Via Gherardesca, 5, 56121, Pisa, Italy; Victor B. Tikhonov and Vladimir A. Obukhov, RIAME MAI, 125080 Moscow, PB 43, Russia

2003-303: SMART-1 EPS END-TO-END TEST: FINAL RESULTS & LESSONS LEARNT; Denis Estublier, ESA/ESTEC, Keplerlaan 1, Postbus 299, 2200 AG Noordwijk ZH, The Netherlands; Christophe Koppel, SNECMA Mouteurs, Division Moteurs-Spatiaux, DPES, Propulsion et Equipements Satellites, Aérodrome de Melun-Villaroche

2003-304: EXPERIMENTAL STUDIES RELATED TO FIELD EMISSION THRUSTER OPERATION: EMISSION IMPACT ON SOLAR CELL PERFORMANCES AND NEUTRALIZATION ELECTRON BACKSTREMING PHENOMENA; E. Chesta, D. Nicolini, D. Robertson, and G. Saccoccia, European Space Agency, Electric and Advanced Propulsion Section, ESTEC, TOS-MPE, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands

2003-305: XENON RESISTOJETS AS SECONDARY PROPULSION ON EP SPACECRAFTS AND PERFORMANCE RESULTS OF RESISTOJETS USING XENON; D. Nicolini, D. Robertson, E. Chesta, and G. Saccoccia, European Space Agency, ESTEC, Noordwijk, The Netherlands; D. Gibbon and A. Baker, Surrey Satellite Technology Ltd., University of Surrey, Guildford, England

2003-306: COUPLED ELECTRODYNAMIC TETHER/ELECTROSTATIC PROPULSION SYSTEM; D. Nicolini, European Space Agency, ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands

2003-307: CHARACTERIZATION OF CURRENT SHEET EVOLUTION IN A PULSED ELECTROMAGNETIC ACCELERATOR; J. W. Berkery and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Princeton, New Jersey 08540

2003-308: ADVANCES IN THE PULSED INDUCTIVE THRUSTER DRIVE SYSTEM; M. Franklin Rose, Radiance Technologies, Inc., 500 Wynn Dr. Suite 504, Huntsville, AL 35816; Henry W. Brandhorst Jr., Space Research Institute, 231 Leach Center, Auburn University, AL 36849-5320

2003-311: STUDY OF MULTI THRUSTER ASSEMBLY OPERATION; L. E. Zakharenkov, A. V. Semenkin, A. V. Rusakov, N. A. Urchenko, S. O. Tverdokhlebov, and V. I. Garkusha, Central Research Institute of Machine Building (TSNIIMASH), Pionerskaya 4, Korolev, Moscow region, Russia 141070; U. V. Lebedev and S. N. Podkolsin, Institute of Space Research, Moscow, Russia; J. M. Five, U.S. Air Force Laboratory Edwards, AFB, CA

2003-312: ANALYSIS OF PROSEDS BARE-TETHER PERFORMANCE; J. R. Sanmartín, Universidad Politécnica de Madrid, Spain; E. C. Lorenzini and M. L. Cosmo, Harvard-Smithsonian Center for Astrophysics, Cambridge, MA, USA; R. D. Estes, OnScreen Science, Inc. Cambridge, MA, USA

2003-313: NEXT GENERATION ION ENGINES: MISSION PERFORMANCES; Muriel Noca, Jet Propulsion Laboratory, California Institute of Technology, MS 301-180, 4800 Oak Grove Drive, Pasadena, CA 91109

2003-316: ELECTRON CURRENTS IN HALL THRUSTER; Igor Levchenko, National Aerospace University, Kharkov, Ukraine; Michael Keidar, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109

2003-319: ELECTRIC PROPULSION SYSTEMS WITH FAST NON-INCANDESCENT START; Mykola V. Bilan, Volodymyr I. Bilokon, Mykola M. Koshelev, Andriy V. Loyan, Sergiy Yu. Nesterenko, Anatoliy I. Oranskiy, and Mykola P. Stepanushkin, Scientific & Technological Center of Space Power & Engines at National Aerospace University, “Kharkov Aviation Institute”, 17, Chkalov St., Kharkov, 61070, Ukraine

2003-320: THE INFLUENCE OF STATIONARY PLASMA THRUSTER FACTORS ON FUNCTIONAL PARAMETERS OF NEUTRALIZER CATHODE; Mykola V. Bilan, Volodymyr I. Bilokon, Sergey V. Veryutin, Volodymyr D. Olendarev, and Anatoliy I. Oranskiy, Scientific & Technological Center of Space Power & Engines at National Aerospace University “Kharkov Aviation Institute”, 17, Chkalov St. Kharkov, 61070, Ukraine

2003-321: TWO DIMENSION EFFECTS IN ION FLOW INSIDE INTER-ELECTRODE GAP OF PLASMA-ION THRUSTER ION OPTICAL SYSTEM; Sergey Yu. Nesterenko and Anatoily I. Oranskiy, Scientific & Technological Center of Space Power & Engines at National Aerospace University “Kharkov Aviation Institute”, 17, Chkalov St. Kharkov, 61070, Ukraine

2003-327: FURTHER INVESTIGATIONS OF AN OPEN DRIFT HALL THRUSTER WITH BORON NITRIDE AND DIAMOND WALL; N. Gascon, C. Thomas, W. Hermann, and M. A. Cappelli, Stanford University, Mechanical Engineering Department, Thermosciences Division, Stanford, CA 94305-3032

2003-328: WALL EFFECTS ON THE EXCITATION AND PROPAGATION OF INSTABILITIES IN HALL THRUSTERS; N. Gascon and M. A. Cappelli, Stanford University, Mechanical Engineering Department, Thermosciences Division, Stanford, CA 94305-3032

2003-329: A NEW LARGE VACUUM TEST FACILITY FOR HIGH POWER ELECTRIC PROPULSION TESTING; Fabrizo Scortecci, AEROSPAZIO Tecnologie s.r.l., I-53040 Rapolano Terme, Siena, Italy

2003-330: IN-SPACE PROPULSION PROGRAM OVERVIEW AND STATUS; Paul F. Wercinski, ISP Program Executive, Solar System Exploration Division, NASA Headquarters, Office of Space Science, Washington, D.C. 20546; Les Johnson, In Space Transportation Investment Area Manager, Advanced Space Transportation Program/TD15, NASA Marshall Space Flight Center, Marshall Space Flight Center, Alabama 35812; Randy M. Baggett, Project Manager, Next Generation Ion, Advanced Space Transportation Program/TD15, NASA Marshall Space Flight Center, Marshall Space Flight Center, Alabama 35812

2003-331: RECENT RESULTS FROM A MODEL OF THE HALL THRUSTER DISCHARGE; E. Ahedo, J. M. Gallardo, F. I. Parra, and C. Pérez Trigo, E.T.S.I. Aeronáuticos, Universidad Politécnica de Madrid, Spain

2003-332: THE HELICON DOUBLE LAYER THRUSTER; Rod Boswell and Christine Charles, Space Plasma and Plasma Processing, PRL/RSPhySE, Australian National University, Canberra ACT 0200

2003-333: INTERACTION OF A HOLLOW CATHODE STREAM WITH A HALL THRUSTER; L. Albaréde, V. Largo, P. Lasgorceix, and M. Dudeck, Laboratoire d’ Aérothermique, 1C avenue de la Recherche Scientifique, 45071 Orléans cedex, France; A. I. Bugrova, Moscow State Institute of Radio-Engineering Electronics and Automation, MIREA, Laboratory of Plasmotics, 78, 117454, Moscow, Russia; K. Malik, Imperial College, London, Great-Britain

2003-334: MODELING AND OPTICAL DIAGNOSTICS OF AN AR PLASMA UNDER PLASMA THRUSTER CONDITIONS; K. Katsonis, S. Bliman, and A. Siskos, Laboratoire de Physique des Gaz et des Plasmas (LPGP), UMR 8578, Université Paris-sud 91405, Orsay cedex, France; S. Pellerin, Ch. De Izarra, and J. Chapele, Laboratoire d’Analyse Spectroscopique et d’Energétique des Plasmas (LASEP), Université d’Orléans-Site de Bourges, rue Gaston Berger, BP 4043, 18028 Bourges cedex, France; K. Dzierzega, M. Smoluchowski Institute of Physics, Jagiellonian University, ul. Reymonta 4 30-059 Kraków, Poland; M. Tanguy, Laboratoire de Physique et Technologie des Plasmas (LPTP), Ecole Polytechnique 91128 Palaiseau, France

2003-335: AN ALTERNATIVE THEORY OF TRANSIT-TIME OSCILLATIONS IN HALL THRUSTERS; Serge Barral, Zbigniew Peradzynski, and Karol Makowski, Institute of Fundamental Technological Research – PAS; Swietokrzyska 21, 00049 Warsaw, Poland; Michael Dudeck, CNRS Laboratoire d’ Aéothermique, 45071 Orléans, France

2003-336: TAL RELATIVE EROSION RATE REAL-TIME MEASUREMENTS THROUGH ANALYSIS OF ITS EMISSION SPECTRA; O. S. Tverdokhlebov, TsNIIMASH, Pionerskaya 4, Korolev, Moscow region, Russia 141070; G. F. Karabadzhak, TsNIIMASH, Pionerskaya 4, Korolev, Moscow region, Russia 141070

2003-339: AN OVERVIEW OF ELECTRIC PROPULSION ACTIVITIES IN JAPAN; Hirokazu Tahara, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

2003-340: STATE OF THE ART AND PROSPECTS OF ELECTRIC PROPULSION IN RUSSIA; Vyacheslav Murashko, Alexander Koryakin, and Arkadij Nyatin, Design Bureau Fakel, 181 Moskovsky prospect, Kaliningrad, 236000, Russia; Vladimir Kim and Garry Popov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), Moscow, Russia; Anatoly Romashko, Yuri Yermoshkin, and Victor Petrusevich, Reshetnev Scientific and Production Association of Applied Mechanics (NPO PM), Zheleznogorsk, Krasnoyarsk Region, Russia; Oleg Gorshkov and Anatoly Koroteyev, Keldysh Research Center (KeRC), Moscow, Russia; Valrey Garkusha and Alexander Semenkin, Sergei Tverdokhlebov Central Institute of Machine-building (TsNIIMASH), Korolev of Moscow Region, Russia

2003-341: INTRODUCTION TO THE EUROPEAN ACTIVITIES IN ELECTRIC PROPULSION; G. Saccoccia, Head of Propulsion and Aerothermodynamics Division, European Space Agency, ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands

2003-366: INTEGRAL AND SPECTRAL CHARACTERISTICS OF ATON STATIONARY PLASMA THRUSTER OPERATING ON KRYPTON AND XENON; A. I. Bugrova, A. S. Lipatov, A. M. Bishaev, V. K. Kharchevnikov, and M. V. Kozintseva, Moscow Institute of Radio Engineering, Electronics and Automation (Technical University), Laboratory of Plasmaoptics, prosp. Vernadskogo, 78, Moscow, Russia, 119454; A. I. Morozov, Russian Scientific Center “Kurchatov Institute”, Kurchatov sq., 1, Moscow, Russia 123182

2003-367: HYBRID PARTICLE-FLUID MODEL OF A HALL THRUSTER PLUME; Francesco Taccogna, Savino Longo, and Mario Capitelli, IMIP-CNR sect. Bari, Italy, Department of Chemistry, University of Bari, Italy

2003-368: A PARALLEL PIC CODE FOR A HALL THRUSTER SIMULATION; I. Vieira, L. Gargaté, R. Fonseca, L. Silva, and J. T. Mendoca, GoLP – Centro de Fisica de Plasmas, Instituto Superior Técnico, Av. Rovisco Pais, 1049-001, Lisboa-Portugal

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0097-0303iepc-full.pdf 09-Jun-2008 13:17  449K

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2005 INDEX

2005-001: ELECTRIC PROPULSION THRUSTER POINTING MECHANISM (TPM) FOR EUROSTAR 3000: DESIGN & DEVELOPMENT TEST RESULTS; Manfred Falkner, Theodor Nitschko, Josef Zemann, Gerhard Mitterbauer, and Gerhard Traxler, Austrian Aerospace GmbH (AAE), Vienna, A-1120, Austria; Alain Demaire, EADS-Astrium, 31402 Toulouse, France

2005-002: EFFECT OF MAGNETIC FIELD PROFILE ON THE ANODE FALL IN A HALL THRUSTER; Leonid A. Dorf, Yevgeny F. Raitses, and Nathaniel J. Fisch, Princeton Plasma Laboratory (PPPL), Princeton, NJ 08543, USA

2005-003: SPACECRAFT/THRUSTERS INTERACTION ANALYSIS FOR SMART-1; J. Gonzalez del Amo and D. Estublier, ESA Technical and Operational Support Directorate ESTEC, Noordwijk, The Netherlands; C. Koppel, Snecma; M. Capacci, M. Tajmar, and A. Passaro, Alenia-Laben, ARC, Alta Spa

2005-004: INVESTIGATION OF THE LOCAL PLASMA PARAMETER DISTRIBUTIONS IN THE SPT ACCELERATING CHANNEL UNDER INCREASED DISCHARGE VOLTAGES; Vladimir Kim, Vycheslav I. Kozlov, Alexander I. Skrylnikov, Lev N. Umnitsin, and Victoria V. Svotina, Research Institute of Applied Mechanics and Electrodynamics (RIAME), 4 Volokolamskye shosse, Moscow, 125871, Russia; Andre Bouchoule, Orleans University, France; Mathieu Prioul, Snecma Moteurs, France

2005-005: RESEARCH AND DEVELOPMENT STATUS OF JAXA NEXT-GENERATION ION ENGINE; Shoji Kitamura, Yukio Hayakawa, Hideki Yoshida and Yasushi Okawa, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan; Ken-ichi Kajiwara, Japan Aerospace Exploration Agency, Tsukuba, Ibaraki, 305-8505, Japan

2005-006: IMPLEMENTATION OF EXTERNALLY-APPLIED MAGNETIC FIELDS TO A NON-IDEAL MHD SOLVER FOR MPD THRUSTER SIMULATION; P.C. Norgaard and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Princeton University, Princeton, NJ, 08544, USA; S. C. Jardin, Princeton Plasma Physics Laboratory (PPPL), Princeton, NJ 08643, USA

2005-007: RESONANT CAVITY HOLLOW CATHODE PROGRESS; Kevin D. Diamant, The Aerospace Corporation, Los Angeles, CA 90009

2005-008: COMPARISON OF EXPERIMENTAL AND COMPUTATIONAL SIMULATIONS RESULTS OF A PULSED PLASMA ACCELERATOR; T. Moeller, D. Keefer, R. Rhodes, and D. Rooney, University of Tennessee Space Institute, Tullahoma, TN 37388, USA; D. Li and C. Merkle, Purdue University, West Lafayette, IN 47907, USA

2005-009: THE CHARGED PARTICLE BEAM SYSTEM OF AN ELECTROSTATIC ION THRUSTER AS AN ANTENNA BEACON ABOARD A SATELLITE; K. Malik, Imperial College, London, SW7 2BZ, UK; J. Gonzalez del Amo, European Space Agency, ESTEC, TOS-MPE, Noordwijk aan Zee (NL)

2005-010: ASTEROID RENDEZVOUS OF HAYABUSA EXPLORER USING MICROWAVE DISCHARGE ION ENGINES; Hitoshi Kuninaka, Kazutaka Nishiyama, Ikko Funakai, Tetsuya, Yukio Shimizu and Jun’ichiro Kawaguchi, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Yoshinodai, Sagamihara, Kanagawa 229, Japan

2005-011: PERFORMANCE OF A LOW-POWER CYLINDRICAL HALL THRUSTER; Kurt A. Polzin, Thomas E. Markusic, Boris J. Stanojev and Amado Dehoyos, Propulsion Research Center, NASA – Marshall Space Flight Center, Huntsville, Alabama 35812; Yevgeny Raitses, Artem Smirnov, and Nathaniel J. Fisch, Princeton University Plasma Physics Laboratory (PPPL), P. O. Box 451, Princeton, New Jersey 08543

2005-012: NUMERICAL MODEL OF PLASMA SHEATHS IN HALL THRUSTER; F. Taccogna, Max-Planck Instittue für Plasmaphysik, EURATOM Association, Wendelsteinstr. 1, Greifswald, D-17491, Germany; S. Longo and M. Capitelli, Dip. Di Chimica, Universitá degli Studi di Bari, Via Orabona 4, Bari, I-70126, Italy

2005-013: A HYDRODYNAMIC-BASED EROSION MODEL FOR HALL THRUSTERS; John T. Yim, Michael Keidar, and Iain D. Boyd, University of Michigan, Ann Arbor, MI 48109, USA

2005-014: ANALYSIS OF PLUME BACKFLOW FROM A LITHIUM MAGNETOPLASMADYNAMIC THRUSTER; Ian D. Boyd, Kevin Scavezze, and Chunpei Cai, University of Michigan, Ann Arbor, Michigan, 48109, USA; James E. Polk, NASA Jet Propulsion Laboratory, Pasadena, California, 91109, USA; Edgar Y. Choueiri, Princeton University, Princeton, New Jersey, 08544, USA

2005-015: EFFECTS OF CHANNEL WALL MATERIAL ON PERFORMANCE AND PLASMA CHARACTERISTICS OF HALL THRUSTERS; Hirokazu Tahara, Katsumi Imanaka, and Seiro Yuge, Graduate School of Engineering Science, Osaka University, Toyonaka, Osaka 560-8531, Japan

2005-016: DEVELOPMENT OF THE TOP HAT ELECTRIC PROPULSION PLUME ANALYZER (TOPAZ): MASS ANALYZER DESIGN AND PRELIMINARY CALIBRATION DATA; Allen L. Victor , Thomas Zurbuchen, and Alec D. Gallimore, University of Michigan, Ann Arbor, Michigan, 48109, USA

2005-017: PERFORMANCE CHARACTERISTICS OF LASER ABLATIVE THRUSTERS FOR SMALL SATELLITES; Hirokazu Tahara, Elichiro Koizumi, and Shin-ichiro Kitagawa, Graduate School of Engineering Science, Osaka Universi04, Toyonaka, Osaka 560-8531

2005-018: SILICON NITRIDE SPRAYING USING QUASI-STEADY MPD ARCJETS; Hirokazu Tahara and Toshiaki Edamitsu, Graduate School of Engineering Science, Osaka University, Toyonaka, Osaka 560-8531, Japan

2005-019: LEVEL SET SIMULATIONS OF CHARGED DROPLETS USING A BOUNDARY ELEMENT METHOD; Anton VanderWyst, University of Michigan, Ann Arbor, MI 8109-210, USA; Andrew Christlieb, University of Michigan, Ann Arbor, MI 8109-103, USA; Mark Sussman, Florida State University, Tallahassee, FL 32306-510, USA; Ian D. Boyd, University of Michigan, Ann Arbor, MI 8109-210, USA

2005-020: PERFORMANCE ENHANCEMENT OF A 1-KW ANODE-LAYER HALL THRUSTER; Seiro Yuge and Hirokazu Tahara, Graduate School of Engineering Science, Osaka University, Toyonaka, Osaka, 560-8531, Japan

2005-021: THEORETICAL ANALYSIS OF ANOMALOUS CONDUCTIVITY IN HALL EECT THRUSTERS; A. Ducrocq, J. C. Adamy, A. Heronzand, and G. Lavalx, Centre de Physique Theorique, Ecole Polytechnique, CNRS UMR, 7644 Palaiseau, 91128, France

2005-022: POTENTIAL STRUCTURE AND PROPELLANT FLOW RATE THEORY FOR ION THRUSTER DISCHARGE CATHODE EROSION; Joshua L. Rovey and Alec D. Gallimore, The University of Michigan, Ann Arbor, MI, 48109, USA; Daniel A. Herman, QSS Group, Inc., Cleveland, OH 44135, USA

2005-023: NEW GENERATION PROPELLANT FLOW CONTROL COMPONENTS FOR ELECTRIC PROPULSIOIN SYSTEMS: STATUS OF ACHIEVEMENTS AT ALCATEL ALENIA SPACE ITALIA/LABEN-PROEL; G. Matticari, G. E. Noci, and P. Siciliano, Alcatel Alenia Space Italia, BU Pro. El, via A. Enstain 35, 50013, Campi Bisenzio, Firenze; G. Martini and A. Rivetti, Istituto Metrologia Guido Colonnetti (IMGC) CNR Torino; N. Kutufa, AOES – BV Leiden – ESA/ESTEC, TOS-MPE, Keplerlaan I, Noordwijk (NL)

2005-024: INTERNAL PLASMA STRUCTURE MEASUREMENTS OF A HALL THRUSTER USING XENON AND KRYPTON PROPELLANT; Jesse A. Linnell and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109, USA

2005-026: DESTRUCTIVE PHYSICAL ANALYSIS OF HOLLOW CATHODES FROM THE DEEP SPACE 1 FLIGHT SPARE ION ENGINE 30,000 HR LIFE TEST; Anita Sengupta, Jet Propulsion Laboratory, Pasadena, CA 91109, US

2005-028: NON-LOCAL ELECTRIC FIELD EFFECTS IN MAGNETIZED PLASMAS; Cliff A. Thomas, Nicolas Gascon, Michelle Allis, Emmanuelle Sommier, and Mark A. Cappelli, Stanford University, Stanford, CA, 94305-3032

2005-029: DEMONSTRATION OF ION HEATING AND ACCELERATION IN A FAST-FLOWING PLASMA FOR THE VASIMR THRUSTER; A. Ando, M. Inutake, K. Hattori, H. Tobari, M. Hatanaka, and M. Shibata, Department of Electrical Engineering, Graduate School of Engineering, Tohoku University, 6-6-05, Aoba-yama, Sendai, 980-8579, Japan

2005-031: FORTY YEARS OF GIESSEN EP-ACTIVITIES AND THE RECENT RIT-MICROTHRUSTER DEVELOPMENT; H. W. Loeb, K. – H. Schartner, B. K. Meyer, D. Feili, St. Weis, and D. Kirmse, 1st Institute of Physics, Giessen University, Giessen D 35392, Germany

2005-033: EXPERIMENTAL INVESTIGATION OF MAGNETIC FIELD TOPOLOGY INFLUENCE ON STRUCTURE OF ACCELERATING LAYER AND PERFORMANCE OF HALL THRUSTER; Nikolay V. Blinov, Oleg A. Gorshkov, and Andrey A. Shagayda, Keldysh Research Center, Moscow, Russia

2005-035: FULLY KINETIC MODELING OF LOW-POWER HALL THRUSTERS; Sergey V. Irishkov, Oleg A. Gorshkov, and Andrey A. Shagayda, Keldysh Research Center, Moscow, Russia

2005-036: EFFECT OF ANTENNA CONFIGURATION ON THRUST PERFORMANCE IN A MINIATURE MICROWAVE DISCHARGE ION ENGINE; Naoji Yamamoto, Hiroshi Kataharada Takayuki Chikaoka, Hirokazu Masui, and Hideki Nakashima, Graduate School of Engineering Sciences, Kyushu University, Kasuga, Fukuoka 816-8580, Japan; Yoshiyuki Takao, Oita National College of Technology, Maki, Oita, 870-0152, Japan

2005-037: ESTIMATION OF EROSION RATE BY ABSORPTION SPECTROSCOPY IN A HALL THRUSTER; Naoji Yamamoto, Graduate School of Engineering Sciences, Kyushu University, Kasuga, Fukuoka 816-8580, Japan; Shirgeru Yokota, Makoto Matsui, Kimiya Komurasaki, and Yoshihiro Arakawa, The University of Tokyo, City, Bunkyo-ku, Tokyo, 113-8656, Japan

2005-038: NON-DIMENSIONAL PERFORMANCE TRENDS OF A PULSED PLASMA ACCELERATOR; John W. Berkery and Edgar Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey 08544

2005-040: SIMULATION OF HIGH-SPECIFIC-IMPULSE AND DOUBLE-STAGE HALL THRUSTERS; D. Escobar, A. Ant, and E. Ahedo, Universidad Politdcnica de Madrid, Spain

2005-041: ON CONDITIONS AT THE SHEATH BOUNDARIES OF A QUASINEUTRAL CODE FOR HALL THRUSTERS; D. Escobar and E. Ahedo, E.T.S.L Aeronduticos, Universidad Politdcnica de Madrid, Madrid 28050, Spain

2005-043: MODELING OF A MICRO-MACHINED PULSED PLASMA THRUSTER; Michael Keidar and Iain D. Boyd, University of Michigan, Ann Arbor, MI; Daniel Simon and Bohdan   Cybyk, The Johns Hopkins University Applied Physics Laboratory, Laurel, MD

2005-044: PROGRESS IN HYDRODYNAMIC MODELING OF HALL THRUSTERS; Michael Keidar and Iain D. Boyd, University of Michigan, Ann Arbor, MI

2005-045: MODELING A TWO-STAGE HIGH-POWER BISMUTH ANODE LAYER THRUSTER AND ITS PLUME; Michael Keidar, Yongiun Choi, and Iain D. Boyd, University of Michigan, Ann Arbor, MI

2005-046: CHARACTERIZATION OF HALL EFFECT THRUSTER PLASMA OSCILLATIONS BASED ON THE HILBERT-HUANG TRANSFORM; Gerard Bonhomme and Cedric Enjolras, LPMI, UMR 7040 CNRS-Université Henri Poincaré, BP 239, F-55506 Vandoeuvre-Iés-Nancy Cedex, France; Jacek Kurzyna, Institute of Fundamental Technological Research, Polish Academy of Sciences, Swietokrzyska 21, 00049 Warsaw, Poland; Stéhane Mazouffre, Luc Albaréde, and Michael Dudeck II, Laboratoire d’ Aérothermique, CNRS, 1C Avenue de la Recherche Scientifique, 45071 Orléans Cedex 2, France

2005-047: HOLLOW CATHODE WITHOUT LOW-WORK-FUNCTION INSERT; H. R. Kaufman and J. R. Kahn, Kaugman & Robinson, Inc., Fort Collins, Colorado 80524, USA

2005-048: THREE-DIMENSIONAL PARTICLE SIUMLATION OF PLUME FLOWS FROM HALL THRUSTERS; Chunpei Cai, Iain D. Boydy and Quanhua Sunz, University of Michigan, Ann Arbor, Michigan, 48109, U.S.A.

2005-049: ADVANCED ELECTRIC PROPULSION CONCEPTS BASED ON MAGNETIC FLUX COMPRESSION AND EXPANSION; P. J. Turchi, Los Alamos National Laboratory, Los Alamos, NM 87545, USA

2005-051: PLUME MEASUREMENTS AND MINIATURIZATION OF THE HALL THRUSTERS WITH CIRCULAR CROSS-SECTIONAL DISCHARGE CHAMBERS; Atsushi Shirasaki and Hirokazu Tahara, Department of Mechanical Science and Bioengineering, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

2005-052: THE DEPENDENCE OF THE ELECTRON TEMPERATURE ON THE DISCHARGE VOLTAGE FOR DIFFERENT HALL THRUSTER CONFIGURATIONS; Yevgeny Raitses, Artem Smirnov, David Staack, and Nathaniel J. Fisch, Princeton University Plasma Physics Laboratory, Princeton, NJ, 08543

2005-053: CONTROLLING ION ACCELERATION REGION IN HALL THRUSTERS; Yevgeny Raitses, David Staack, Leonid Dorf, and Nathaniel J. Fisch, Princeton University Plasma Physics Laboratory, Princeton, NJ, 08543; Michael Keidar, University of Michigan, Ann Arbor, MI 48109

2005-054: SWIRL ACCELERATION IN A QUASI-STEADY MPD THRUSTER BY APPLIED MAGNETIC NOZZLE; Yoichi Kagaya and Hirokazu Tahara, Osaka University, Toyonaka, Osaka, 560-8531, Japan

2005-055: RESEARCH AND DEVELOPMENT STATUS OF MICROWAVE DISCHARGE ION THRUSTER µ20, Kazutaka Nishiyama, Yukio Shimizu, and Hitoshi Kuninaka, Japan Aerospace Exploration Agency / Institute of Space and Astronautical Science, Sagamihara, Kanagawa, 229-8510, Japan; Takashi Miyamoto, Kyushu University, Koganei, Tokyo, 184-8584, Japan; Tatsuya Nakai, The University of Tokyo, Bunkyo-ku, Tokyo, 113-8656, Japan

2005-056: DEVELOPMENT OF A MICROWAVE-EXCITED MICROPLASMA THRUSTER; Yoshinori Takao, Kouichi Ono Kazuo Takahashi, and Koji Eriguchi, Department of  Aeronautics and Astronautics, Kyoto University, Kyoto, 606-8501, Japan

2005-057: EFFECT OF CHARGE EXCHANGE ON 2D HALL THRUSTER SIMULATION; Michelle K. Allis, Nicolas Gascon, and Mark A. Cappelli, Stanford University, Stanford, CA 94305; Eduardo Fernandez, Eckerd College, St. Petersburg, FL, 33711

2005-058: STATIONARY REFERENCE BI DISCHARGE CELL FOR OPTICAL DIAGNOSTICS OF A BISMUTH HALL THRUSTER; David B. Scharfe and Mark A. Cappelli, Stanford University, Stanford, CA, 94305, USA

2005-059: DEVELOPMENT OF AN APPLIED FIELD MAGNETOPLASMADYNAMIC THRUSTER DESIGN SUPPORTED BY NUMERICAL SIMULATIONS AT IRS; Daniel Haag, Monika Auweter-Kurz, Markus Fertig and Helmut Kurtz, Universität Stuttgart, Institut Für Raumfahrtsysteme (IRS), Pfaffenwaldring 31, 70550 Stuttgart, Germany

2005-060: TESTING OF A DIGITAL COLLOID THRUSTER FOR PRECISE THRUST THROTTLING; Mark D. Paine, Queen Mary, University of London, London, E1 4NS, United Kingdom

2005-061: PLASMA PARAMETERS INVESTIGATION IN THE NEAR CATHODE ZONE OF THE SPT DISCHARGE; A. A. Pereslavtsev and S. A. Khartov, Moscow Aviation Institute (State University of Aerospace Technologies) MAI, 4, Volokolamskoe sh., Moscow, 125971, Russia

2005-062: SPT’S HIGH LIFETIME-SOME PROBLEMS OF SOLUTION; S. A. Khartov, A. B. Nadiradze, I. I. Shkarban, and Y. V. Zikeeva, Moscow Aviation Institute (State University of Aerospace Technologies) MAI, 4, Volokolamskoe sh., Moscow, 125971, Russia

2005-063: AN INFRARED THERMOGRAPHY STUDY ON THE THERMAL LOAD EXPERIENCED BY A HIGH POWER HALL THRUSTER; S. Mazouffre, J. Pérez Luna, D. Gawron, and M. Dudeck, Laboratoire d’Aérothermique, CNRS, 1C Avenue de la Recherche Scientifique, Orléans, 45071, France

2005-064: DEVELOPMENT STATUS OF 200MN CLASS XENON HALL THRUSTER OF MELCO; Toshiyuki Ozaki, Mitsubishi Electric Corporation, Kamakura, Kanagawa, 247-8520, Japan; Yasutaka Inanaga, Mitsubishi Electric Corporation, Amagasaki, Hyogo, 661-8661, Japan; Takafumi Nakagawa and Hiroyuki Osuga, Mitsubishi Electric Corporation, Kamakura, Kanagawa, 247-8520, Japan

2005-065: DIRECT MEASUREMENT OF LORENTZ FORCES IN AN APPLIED-FIELD MPD THRUSTER; H. Tobari, A. Ando, M. Inutake and K. Hattori, Department of Electrical Engineering, Graduate School of Engineering, Tohoku University, 6-6-05, Aoba-yama, Sendai, 980-8759, Japan

2005-066: THE XENON REGULATOR AND FEED SYSTEM FOR ELECTRIC PROPULSION SYSTEMS; Ray Thompson and Howard Gray, EADS Astrium Ltd, Portsmouth, PO3 5PU, UK

2005-067: HEAT FLUX MEASUREMENTS IN THE HALL THRUSTER PLUME; G. Makrinich and A. Fruchtman, Holon Academic Institute of Technology, Holon 58102, Israel; S. Shitrit, G. Appelbaum and J. Ashkenazy, Soreq NRC, Yavne 81800, Israel

2005-068: THE EFFECT OF THE MAGNETIC FIELD PROFILE OIN THE PLUME AND ON THE PLASMA FLOW IN THE HALL THRUSTER; A. Fruchtman, Holon Academic Institute of Technology, 52 Golomb St., Holon 58102, Israel

2005-069: PERFORMANCE IMPROVEMENT OF A LIQUID PROPELLANT PULSED PLASMA THRUSTER; Hiroyuki Koizumi, Yoko Kawazoe, Kimiya Komurasaki, and Yoshihiro Arakawa, University to Tokyo, Tokyo, 113-8656, Japan

2005-071: DEVELOPMENT OF HYBRID PIC/DSMC CODE; Monika Auweter-Kurtz, Markus Fertig, Dejan Petkow and Torsten Stindl, Institut für Raumfahrtsysteme, Universität Stuttgart, D-70550 Stuttgart, Germany; Martin Quandt and Claus-Dieter Munz, Institut für Aerodynamik und Gasdynamik, Universität Stuttgart, D-70550 Stuttgart, Germany; Panos Adamidis, Michael Resch and Sabine Roller, Höchstleistungsrechenzentrum Stuttgart, D-70550 Stuttgart, Germany; Danilo D’Andrea and Rudolf Schneider, Institut für Hochleistungsimpuls and Mikrowellentechnik, Forschungszentrum Karlsruhe, D-76133 Karlsruche, Germany

2005-073: THE DISTINCTION BETWEEN THE EP PLUME EXPANSION IN SPACE AND IN VACUUM CHAMBER; Anatoly G. Korsun, Ekaterina M. Tverdokhlebova, Flur R. Gabdullin, Central Research Institute of Machine Building (TsNIIMASH), Pionerskaya str., 4, Korolev, Moscow region, 141070, Russia

2005-074: NUMERICAL PROCEDURE PERMITTING CALCULATION OF HOW A VACUUM CHAMBER INFLUENCES ELECTRIC PROPULSION THRUSTER JET EXPANSION; Toropov G. P., Student, Moscow Aviation Institute (State Technical University) MAI Engineering Plasma Computational Laboratory (EPCLab) 24b, Zalineynaya str., Vologda, 160010, Russia

2005-075: 1 KW AMMONIA ARCJET SYSTEM DEVELOPMENT FOR A SCIENCE MISSION TO THE MOON; Dagmar Bock, Monika Auweter-Kurtz, and Helmut L. Kurtz, Universität Stuttgart, Institut für Raumfahrtsysteme. Pfaffenwaldring 31, D-0569 Stuttgart, Germany

2005-077: A 3D MODEL CALCULATING SPUTTERING AND DEPOSITING PROCESSES UNDER ELECTRIC PROPULSION THRUSTER TESTING IN A VACUUM CHAMBER; G. P. Toropov, Student, Moscow Aviation Institute (State Technical University) MAI Engineering Plasma Computational Laboratory (EPCLab), 24b, Zalineynaya str., Vologda, 160010, Russia; A. B. Nadiradze and S. A. Khartov, Moscow Aviation Institute (State Technical University) MAI Electric Propulsioin and Space Power Plants Department 4, Volokolamskoe sh., Moscow, 125971, Russia

2005-078: KINETIC SIMULATION OF EFFECTS OF SECONDARY ELECTRON EMISSION ON ELECTRON TEMPERATURE IN HALL THRUSTERS; D. Sydorenko and A. Smolyakov, University of Saskatchewan, Saskatoon, SK, S7H3E6, Canada; I. Kaganovich and Y. Raitses, Princeton University, Princeton, NJ, 08543, USA

2005-079: PLASMA DIAGNOSTICS ON XENON FOR APPLICATION TO ION THRUSTERS; Michael W. Winter, Monika Auweter-Kurtz, Thomas Pfrommer and Nataliya Semenova, Universität Stuttgart, Institut für Raumfahrtsysteme (IRS), Pfaffenwaldring 31, 70550 Stuttgart, Germany

2005-080: HALL THRUSTER MODIFICATIONS FOR REDUCED POWER OPERATION; J. Ashkenazy, S. Shitrit, and G. Appelbaum, Propulsion Physics Laboratory, Soreq NRC, Yavne 81800, Israel

2005-081: THE EFFECT OF MOLAR CONDUCTIVITY UPON CURRENT AND THRUST IN A COLLOID ELECTROSPRAY THRUSTER SYSTEM; Katharine L. Smith, Matthew S. Alexander, and John P. W. Stark, Queen Mary University of London, London, E1 4NS, UK

2005-082: INMARSAT 4F1 PLASMA PROPULSION SYSTEM INITIAL FLIGHT OPERATIONS; Howard Gray, EADS Astrium Ltd, Portsmouth, PO3 5PU, UK; Severin Provost, EADS Astrium SAS, 31402 Toulouse Cedex 4, France; Michael Glogowski, Inmarsat Global Ltd, London, EC1Y 1AX, UK; Alain Demaire, EADS Astrium SAS, 31402 Toulouse Cedex 4, France

2005-083: IMPROVEMENT OF AN MPD THRUSTER PERFORMANCE WITH A LAVAL-TYPE MAGNETIC NOZZLE; M. Inutake, A. Ando, K. Hattori, H. Tobari, K. Harata and T. Komagome, Department of Electrical Engineering, Graduate School of Engineering, Tohoku University, 6-6-05, Aoba-yama, Sendai, 980-8579, Japan

2005-084: THE ONSET OF VOLTAGE HASH AND ITS RELATIONSHIP TO ANODE SPOTS IN MAGNETOPLASMADYNAMIC THRUSTERS; Luke Uribarri and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory, Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, New Jersey, 08544

2005-085: NUMERICAL SIMULATION OF FARADAY PROBE MEASUREMENTS IN A MULTI-COMPONENT NON-EQUILIBRIUM PLASMA; Jeremiah J. Boemer and Iain D. Boyd, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI, 48109

2005-086: DEVELOPMENT OF A CAPACITIVELY COUPLED INSERT-FREE RF-NEUTRALIZER; St. Weis, K. H. Schartner, H. Löb, and D. Feili, University of Gießen, 1. Physikalisches Institut, Heinrich-Buff-Ring 16, 35392 Gießen

2005-087: VOLTAGE EFFECTS ON THE VOLUMETRIC FLOW RATE AND THRUST PRODUCED IN ELECTROSPRAY PROPULSION SYSTEMS; Matthew S. Alexander, Katharine L. Smith, and John P. W. Stark, Queen Mary, University of London, London, E1 4NS, UK

2005-088: LOWER-HYBRID INSTABILITY IN HALL THRUSTER; Alexander Kapulkin and Moshe Guelman, Asher Space Research Institute Technion, I.I.T., Haifa, 32000, Israel

2005-089: NUMERICAL INVESTIGATION OF IONIZATION AND ACCELERATION PROCESSED IN A SELF-FIELD MPD THRUSTER; K. Kubota, Tokyo Institute of Technology, Yokohama, Kanagawa, 226-8503, Japan; I. Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan; Y. Okuno, Tokyo Institute of Technology, Yokohama, Kanagawa 226-8503, Japan

2005-092: SPACE CHARGE NEUTRALIZATION USING NEGATIVE IONS AND DUST PARTICLES IN THE ION AND HALL THRUSTERS; Artem Smimov, Yevgeny Raitses, and Nathaniel J. Fisch, Princeton University Plasma Physics Laboratory, P.O. Box 451, Princeton, New Jersey 08543

2005-093: ION ACCELERATION BY SINGLE PASS ION CYCLOTRON HEATING IN THE VASIMR ENGINE; Edgar A. Bering, III and Michael Brukardt, University of Houston, Houston, TX, 77204-5005, USA; Franklin R. Chang-Diaz, Jared P. Squire, Timothy W. Glover, Verlin Jacobson, Alfonso Tarditi, and Gred McKaskill, AdAstra Rocket Company, Houston, TX, 77058, USA; Roger D. Bengtson, University of Texas at Austin, Austin, TX 78712

2005-094: EXPERIMENTAL AND THEORETICAL STUDIES OF THE LITHIUM-FED MULTICHANNEL AND SINGLE-CHANNEL HOLLOW CATHODE; Leonard D. Cassady and Edgar Y. Choueiriy, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey, 08544

2005-095: ION THRUSTER OPTICAL PERFORMANCE ENHANCEMENT VIA ION-EMISSIVE-SURFACE SHAPING; Paul J. Wilbur, Cody Farnell, and John D. Williams, Colorado State University, Fort Collins, Colorado, 80523, USA

2005-096: MODELING OF COLLISIONLESS AND KINETIC EFFECTS IN THRUSTER PLASMAS; Igor D. Kaganovich, Plasma Physics Laboratory, Princeton University, Princeton, NJ, 08543, USA

2005-098: ELECTRON CROSS-FIELD TRANSPORT IN A 100 W CYLINDRICAL HALL THRUSTER; Artem Smimov, Yevgeny Raitses, and Nathaniel J. Fisch, Princeton University Plasma Physics Laboratory, P. O. Box 451, Princeton, New Jersey 08543

2005-099: THE EFFECT OF MAGNETIC FIELD ON THE PERFORMANCE OF LOW-POWER CYLINDRICAL HALL THRUSTERS; Artem Smimov, Yevgeny Raitses, and Nathaniel J. Fisch, Princeton University Plasma Physics Laboratory, P.O. Box 451, Princeton, New Jersey, 08543

2005-100: THE COAXIAL HIGH ENERGY THRUSTER; Flavio Poehlmann, Nicolas Gascon, Cliff Thomas, Mark Cappelli, Stanford University, Stanford, CA 94305, USA

2005-101: MECHANICAL ASSEMBLY OF ELECTROSPRAY THRUSTER GRID; B. Gassend, L. F. Velasques-Garc, A. I. Akinwandez, and M. Martnez-Sanchez, Massachusetts Institute of Technology, Cambridge, Massachusetts, 02139, USA

2005-104: AN EXPERIMENTAL STUDY OF CARBON NANOTUBE FIELD EMISSION CATHODES FOR ELECTRODYNAMIC TETHERS; Yasushi Okawa, Shoji Kitamura, and Satomi Kawamoto, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan; Yasushi Iseki, Kiyoshi Hashimoto, and Etsuo Noda, Toshiba Corporation, Fuchu, Tokyo, 183-8511, Japan

2005-105: PERFORMANCE MEASUREMENT AND FLOWFIELD CALCULATION OF AN ELECTROTHERMAL PULSED PLASMA THRUSTER WITH A PROPELLANT FEEDING MECHANISM; Toshiaki Edamitsu and Hirokazu Tahara, Graduate School of Engineering Science, Osaka University, Toyonaka, Osaka 560-8531, Japan

2005-106: RESEARCH AND DEVELOPMENT OF A PULSED PLASMA THRUSTER IN OSAKA UNIVERSITY; Toshiaki Edamitsu, Hirofumi Asakura, Akinori Matsumoto, and Hirokazu Tahara, Graduate School of Engineering Science, Osaka University, Toyonaka, Osaka 560-8531, Japan

2005-107: EXPERIMENTAL SIMULATION OF A PLASMA FLOW AROUND MAGNETIC SAIL; H. Kojima, University of Tsukuba, Tsukuba, Ibaraki, 2305-8577, Japan; I. Funaki, Y. Shimizu, H. Yamakawa, S. Shinohara, Institute of Space and Astronautical Science (ISAS) of Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan; Y. Nakayama, National Defense Academy, Yokosuka, Kanagawa, 239-8686, Japan

2005-108: VHITAL-160 THERMAL MODEL BUILDING AND 3D THERMAL MODELING CARRYING-OUT; Svetlana A. Tverdokhlebova, TsNIIMASH, Pionerskaya 4, Korolev, Moscow region, Russia, 141070; Oleg S. Tverdokhlebov, TsNIIMASH, Pionerskaya 4, Korolev, Moscow region, Russia, 141070

2005-111: APPT PROPULSION SYSTEM FOR SMALL SATELLITES; Nikolay N. Antropov and Garry A. Popv, Research Institute of Applied Mechanics and Electrodynamics, 4, Volokolamskoye shosse, Moscow, 125810, Russia; Michael N. Kazeev, Russian Research Centre Kurchatov Institute, 1, Kurchatov sq., Moscow, 123182, Russia; Vladimir P. Khodnenko, All-Russian Research Institute of Electromechanics, 101000, P.O. Box 496, Moscow, Russia; Yuri I. Pugachev and Nikolay P. Shelkov, Russian Research Institute of Electromechanics, 143500, ul. Panfilova, Istra-2 Moscow region, Russia

2005-114: DEVELOPMENT STATUS OF POWER PROCESSING UNIT FOR 200MN-CLASS HALL THRUSTER; Hiroyuki Osuga, Kentarou Suzuk, Toshiyuki Ozaki, and Takafumi Nakagawa, Space System Department, Kamakura Works, Mitsubishi Electric Corporation, 325 Kamimachiya, Kamakura, Kanagawa, 247-8520, Japan; Ikuro Suga, Tomoyuki Kawakam, and Takuya Sakai, Advanced Technology R&D  Center, Mitsubishi Electric Corporation, 8-1-1 Tukaguchi-ho nmachi, Amagasaki, Hyogo, 661-8661, Japan; Yoshiyuki Akuzawa, Fumitoshi Soga, and Teppei Furuich, Engineering Department, Kamakura Engineering Office, Mitsubishi Electric Engineering Company Limited, 730 Kamimachiya, Kamakura, Kanagawa, 247-0065, Japan

2005-115: FEASIBLITY STUDY OF MAGNETOPLASMA SAIL; Ikkoh Funaki, Hiroshi Yamakawa, Hiroyuki Ogawa, Hiroyuki Nishida, and Iku Shinohara, Institute of Space and Astronautical Science, JAXA, Sagamihara, Kanagawa, 229-8510, Japan; Kazuhisa Fujita, Institute of Space Technology and Aeronautics, JAXA, Chofu, Tokyo, 182-8522, Japan; Yoshinori Nakayama, National Defense Academy, Yokosuka, Kanagawa, 239-8686, Japan; Hirotaka Otsu, Shizuoka University, Hamamatsu, Shizuoka, 432-8561, Japan

2005-117: ON THE ANOMALOUS DIFFUSION MECHANISM IN HALL-EFFECT THRUSTERS; J. M. Gallardo and E. Ahedo, Universidad Politdcnica de Madrid, Spain

2005-118: EFFECTS OF PARTIAL THERMALIZATION AND SECONDARY EMISSION ON THE ELECTRON DISTRIBUTION FUNCTION IN HALL THRUSTERS; E. Ahedo and V. de Pablo, Universidad Politécnica de Madrid, Madrid 28040, Spain; M. Martínez-Sánchez, Massachusetts Institute of Technology, Cambridge, MA 02139, USA

2005-119: THE SMART-1 HALL EFFECT THRUSTER AROUND THE MOON: IN FLIGHT EXPERIENCE; Christophe R. Koppel, Snecma, Safran Group, Division Moteurs Spatiaux, 77552 Moissy-Cramayel, France; Denis Estublier, ESA Technical and Operational Support Directorate ESTEC, Noordwijk, The Netherlands

2005-020: NUMERICAL INVESTIGATION OF LOW-FREQUENCY LONGITUDINAL OSCILLATIONS IN HALL THRUSTERS; S. Barral, Institute of Fundamental Technological Research, PAS, 0009, Warsaw, Poland; V. Lapuerta, A. Sancho and E. Ahedo, Universidad Politécnica de Madrid, 2800 Madrid, Spain

2005-022: ON THE POSSIBILITIES OF RF ION THRUSTERS OPTIMIZATION; A. F. Alexandrov, E. A. Kralkina, V. B. Pavlov, and A. A. Rukhadze, Physical Department of Moscow State University, Vorobjevy gory, Moscow, Russia 119992; A. I. Bugrova, G. E. Bugrov, and K. V. Vavilin, Moscow Institute of Radiotechniks, Electronics and Automatics, (Technical University), Vemadskogo pr., 78, Moscow, Russia 117454

2005-023: MICRO-ARCJET: MICROFABRICATION WITH UV LASERS AND THRUST CHARACTERISTICS; Hideyuki Horisawa and Tsuyoshi Noda, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Kosuke Onodera, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo, Bunkyo-ku, Tokyo, 113-8856, Japan

2005-124: SPACE POTENTIAL FLUCTUATION IN AN ANODE-LAYER HALL THRUSTER; Shigeru Yokota, Kimiya Komurasaki, and Yoshihiro Arakawa, The University of Tokyo, Department of Aeronautics and Astronautics, Hongo 7-3-1, Bunkyo, Tokyo 113-8656, Japan

2005-125: MEASUREMENT OF PLASMA BEAM ENERGY EFECTED FROM MICROWAVE DISCHARGE HALL THRUSTER; Hirohisa Kuwano, Kyushu University, 6-1, Kasuga-Kouen, Kasuga 816-8580, Japan; Hitoshi Kuninaka, Institute of Space and Astronautical Science (ISAS), Japan, Aerospace Exploration Agency (JAXA), 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan; Hideki Nakashima, Kyushu University, 6-1, Kasuga-Kouen, Kasuga 816-8580, Japan

2005-126: MICRO-THRUST BALANCE TESTING AND CHARACTERIZATION; Simone Rocca, University of Padova, Padova, 35131, Italy; Davide Nicolini, European Space Agency, Noordwijk, 2201 AZ, The Netherlands

2005-128: MODELING OF THE PULSED INDUCTIVE THRUSTER, (PIT) OPERATING WITH AMMONIA PROPELLANT; Pavlos G. Mikellides and Darcy L. Allison, Arizona State University, Tempe, AZ 85287, USA; Nalin Ratnayake, Arizona State University, Tempe, AZ 85287, USA; Deborah Booze, Arizona State University, Tempe, AZ 85287, USA

2005-129: PROBE DIAGNOSTICS IN A BISMUTH HALL THRUSTER; Alex Kieckhafer, Dean Massey, and Lyon B. King, Michigan Technological University, 815 R. L. Smith Bldg., Houghton, MI 49931

2005-130: ELECTRIC PROPULSION IN GERMANY: CURRENT PROGRAM AND PROSPECTIVES; Hans Meusemann, German Aerospace Center (DLR), 53227 Bonn, Germany; Michael Winter, Institute of Space Systems at Stuttgart University, 50550 Stuttgart, Germany; Contributions of members of the “German Working Group on Electric Propulsion (EP WG)”; Horst W. Loeb, Karl-Heinz Schartner, Monika Auweter-Kurtz, Rainer Killinger, Guenter Kornfeld, Harry Adirim, Michael Tartz, Holger Kersten, Ulrich Schwab, Michael Boss, and Hartmut Henkel

2005-132: THE “NEW GRID SYSTEMS FOR ION ENGINES” TECHNOLOGY PROJECT – RESULTS AND CONCLUSION; Hans J. Leiter and Rainer Kiillinger, EADS Space Transporation GmbH, Möckmühl, D-74215, Germany; Elisa Bonelli, Simone Scaranzin and Fabrizio Scortecci, Aerospazio S.r.l. Zona Industriale “SENTINO”, 53040 Rapolano Terme, Siena, Italy; Marco Capacci and Maurizio Materassi, ALENIA LABEN Proel Via A. Einstein 35, 50013 Campi Bisenzio (Firenze), Italy; Leonardo Biagioni, ALTA Via A. Gherardesca 5, Ospedaletto, Pisa, Italy; Niccola Kutufa, AOES-BV Leiden and European Space Research and Technology Centre, ESTEC/ESA, P.O. 299, 2200 Noordwijk, The Netherlands; Horst Neumann and Michael Tartz, IOM Leipzig, Permoserstaße 15, 04318 Leipzig, Germany; Davar Feili, University of Giessen, Heinrich Buff Ring 16, 35539 Giessen, Germany

2005-136: CHARACTERISTICS OF PPS-1350 TYPE THRUSTERS UNDER INCREASED DISCHARGE VOLTAGES AND COMPARISON WITH HYBRID CODES SIMULATION RESULTS; L. Albaréde and A. Bouchoule, Laboratoire GREMI, université d’Orléans France; A. Lazurenko, Laboratoire d’Aérothermique CNRS 45071 Orléans France; V. Kim, V. Kozlov, and A. Skrylnikov, RIAME Moscow Russia

2005-137: NUMERICAL STUDY OF A DOUBLE STAGE HALL EFFECT THRUSTER; C. Boniface, G.J.M. Hagelaar, L. Garrigues and J. P. Boeuf, CPAT, UMR 5002, Université Pau Sbatier, 118 Route de Narbonne, 31062 Toulouse Cedex 4, France; M. Prioul Snecma Moteurs DPES Site de Villaroche Nord BP93F 77552, Moissy-Cramayel, France

2005-138: PARTICLE SIMULATION OF HALL THRUSTER PLUMES IN THE 12V VACUUM CHAMBER; Iain D. Boyd, Quanhua Sun, and Cai Chunpei, University of Michigan, Ann Arbor, MI, 48109, USA; Kenneth E. Tatum, Aerospace Testing Alliance, Arnold Air Force Base, TN, 37389, USA

2005-139: GRID PERFORMANCE MODELS USING DESGIN OF EXPERIMENTS (DoE) METHODS; Michael Tartz, Jan H. Peters, and Horst Neumann, Leibniz-Institute for Surface Modification, Leipzig, Germany

2005-140: RESEARCH ON OPTIMIZATION OF ONBOARD MAGNETIC DIAGNOSTICS SYSTEM OF HALL THRUSTER PLASMA; Binyamin Rubin, Faculty of Aerospace Engineering, Technion, I.I.T., Haifa, 32000, Israel; Alexander Kapulkin and Moshe Guelman, Asher Space Research Institute Technion, I.I.T., Haifa, 32000, Israel

2005-141: AN OVERVIEW OF THE TsNIIMASH/ TsE EFFORTS UNDER VHITAL PROGRAM; Oleg S. Tverdokhlebov, TsNIIMASH, Pionerskaya 4, Korolev, Moscow region, Russia, 141070; Sergey O. Tverdokhlebov, TsNIIMASH-EXPORT, Pionerskaya 4, Korolev, Moscow region, Russia 141070; Alexander V. Semenkin, TsNIIMASH, Pionerskaya 4, Korolev, Moscow region, Russia, 141070

2005-142: HIGH-FREQUENCY INSTABILITIES IN HALL-EFFECT THRUSTERS: CORRELATION WITH THE DISCHARGE CURRENT AND THRUSTER SCALE IMPACT; A. Lazurenko, Aerothernique Laboratory, CNRS, Orleans, France; L. Albaréde, and A. Bouchoule, GREMI Laboratory, Orleans University, France

2005-143: PYROLYTIC GRAPHITE AND CARBON-CARBON SPUTTER BEHAVIOUR UNDER XENON ION INCIDENCE; Michael Tartz and Horst Neumann, Leibniz-Institute for Surface Modification, Leipzig, Germany; Hans Leiter, EADS Space Technology, Möckmühl, Germany; Joachim Esch, Schunk Kohlenstofftechnik, Heuchelheim, Germany

2005-144: PARAMETIC STUDY OF THE ACCELERATION LAYER IN A HIGH POWER HALL EFFECT THRUSTER BY FABRY-PEROT SPECTROSCOPY; D. Gawron and s. Mazouffre,Laboratoire d’Aérothermique, CNRS, 1c Avenue de la recherché scientific, 45071 Orléans, France; C. Boniface, CPAT, CNRS, Université Paul Sabatier, 118 route de Narbonne, 31062 Toulouse, France

2005-145: OPERATION OF TWO-STAGE THRUSTER WITH ANODE LAYER IN “FLOATING ELECTRODE” SCHEME; Alexander E. Solodukhin and Alexander V. Semenkin, Central Research Institute of Machine Building (TSNIIMASH), Pionerskaya 4, Korolev, Moscow region, 141070, Russia

2005-146: INVESTIGATION OF PHYSICAL PROCESSES IN SPT MAG; A. I. Bugrova, A. V. Desyatskov, and V. K. Kharchevnikov, Moscow Institute of Radioengineering, Electronics and Automatics, Moscow, Russia; A. I.  Morozov, RSC, Kurchatov Institute, Moscow, Russia; M. Priol, Snecma Moteurs, Satellite Propulsion and Equipment, Villaroche, France

2005-147: EVALUATION OF IMPURITY COMPOSITION AND CONTENT IN THE TAL AT VARIOUS OPERATING REGIMES; G. F. Karabadzhak, A. V. Semenkin, A. e. Solodukhin and O. S. Tverdokhlebov, Central Research Institute of Machine-Building (TSNIIMASH), Korolev, Moscow region, 141070, Russia

2005-149: A MINIATURIZED MICROWAVE DISCHARGE ION THRUSTER WITH HIGH HOLE NUMBER DENSITY GRID SYSTEM; Yoshinori Nakayama, National Defense Academy, Yokosuka, Kanagawa, 239-8686, Japan; Ikkoh Funaki and Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2005-152: HALL EFFECT THRUSTER WITH AN A1N DISCHARGE CHANNEL; S. Barral, Institute of Fundamental Technological Research – PAS, 0009, Warsaw, Poland; Y. Jayet, S. Mazouffre, and M. Dudeck, Laboratoire d’Aérothermique – CNRS, 5071 Orléans, France; E. Vron and P. Echegut, Centre de Recherche sur les Matdriaux Haute Température – CNRS, 5071 Orléans, France

2005-153: FUNDAMENTALS OF DISCHARGE INITIATION IN GAS-FED PULSED PLASMA THRUSTERS; James E. Cooley and Edgar Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Princeton University, Princeton, New Jersey 08544

2005-155: PERVEANCE AND BEAMLET EXPANSION MODELING OF THE NEXT ION ENGINE; Jerold W. Emhoff, Johns Hopkins University Applied Physics Laboratory, Laurel, Maryland, 20723; Iain D. Boyd, University of Michigan, Ann Arbor, Michigan, 48109; Cody C. Farnelland and John D. Williams, Colorado State University, Fort Collins, Colorado, 80523

2005-156: DEVELOPMENT OF A HIGH POWER ELECTRODELESS THRUSTER; Gregory D. emsellem, The Elwing Company, Wilmington, DE, 19801, USA

2005-158: ATON-TYPE SPT OPERATION AT HIGH VOLTAGES; A. I. Bugrova, A. S. Lipatov, and S. V. Baranov, Moscow Institute of Radio-engineering, Electronics and Automatics, Moscow, Russia; A. I. Morozov, RSC Kurchatov Institute, Moscow, Russia

2005-160: EXPERIMENTAL AND ANALYTICAL INVESTIGATION OF A MODIFIED RING CUSP NSTAR ENGINE; Anita Sengupta, Jet Propulsion Laboratory, Pasadena, CA, 91109, US

2005-161: SPT OPERATION IN “MACHINE-GUN” MODE; A. I. Bugrova, A. S. Lipatov, and S. V. Baranov, Moscow Institute of Radio-engineering, Electronics and Automatics, Moscow, Russia; A. I. Morozov, RSC, Kurchatov Institute, Moscow, Russia; Yu Daren, Harbin Institute of Technology, Harbin, Chinese People’s Republic

2005-162: OVERVIEW OF ELECTRIC PROPULSION ACTIVITIES IN FRANCE; Franck Darnon, Denis Arrat, Enrico Chesta, Stéphane d’Escrivan, and Nicolas Pillet; Centre National d’Etudes Spatiales, 18 av. E. Belin, 31401, Toulouse, France

2005-163: EXPERIMENTAL VERIFICATION OF THE NOZZLE SHAPE OPTIMIZATION FOR SELF-FIELD MPD THRUSTER; Daisuke Nakata and Yoshihiro Arakawall, University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan; Kyoichiro Toki, Tokyo University of Agriculture and Technology, 2-24-16, Nakaeho, Koganei-shi, Tokyo 184-8588, Japan; Ikkoh Funaki, Yukio Shimizu, and Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara-shi, Kanagawa 229-8510, Japan

2005-164: THE EMISSIVE MEMBRANE ION THRUSTER CONCEPT; Paul J. Wilbur, Colorado State University, Fort Collins, Colorado, 80523, USA; Merrill Wilson and Kent Hutchings, Ceramatec, Inc., Salt Lake City, Utah, 84119, USA; John D. Williams, Colorado State University, Fort Collins, Colorado, 80523, USA

2005-167: SPECTRAL INVESTIGATION OF SPT MAG INSULATOR EROSION; A. I. Bugrova, A. M. Bishaev, A. V. Desyatskov and M. V. Kozintseva, Moscow Institute of Radio-engineering, Electronics and Automatics, Moscow, Russia; M. Prioul, Snecma Moteurs, Satellite Propulsion and Equipment, Villaroche, France

2005-168: DIAGNOSTICS FOR IN-SPACE TESTING OF HIGH POWER ELECTRIC THRUSTERS ON THE INTERNATIONAL SPACE STATION; D. Gregory Chavers, Chris Dobson, Jonathan Jones, and Jason Vaughn, NASA Marshall Space Flight Center, Huntsville, AL 35812, USA; Andrew Petro, NASA Johnson Space Center, Houston, Texas, 77058, USA; Franklin Chang-Diaz, Ad Astra Rocket Companny, Houston, Texas 77058, USA; Edgar Bering, University of Houston, Houston, Texas, 77204-5005, USA

2005-169: FROM THE PAST TO THE FUTURE; A. I. Morozov, RSC Kurchatov Institute, Moscow, Russia

2005-170: CHARACTERIZATION OF HIGH-DENSITY FLOWING PLASMAS USING A DIRECTIONAL MICRO-RETARDING POTENTIAL ANALYZER; James Partridge and Nikolaos A. Gatsonis, Worcester Polytechnic Institute, Worcester, MA 01609, USA

2005-171: DETAILS OF AN ANNULAR FIELD REVERSED CONFIGURATION PLASMA DEVICE FOR SPACECRAFT PROPULSION; David Kirtley, Daniel L. Brown, and Alec D. Gallimore, University of Michigan, Ann Arbor, MI 48109

2005-173: TRAJECTORY OPTIMIZATION USING GLOBAL METHODS; Michael A. Paluszek and Stephanie J. Thomas, Princeton Satellite S ystems, Princeton, NJ

2005-174: NUMERICAL REBUIDLING OF SMART-1 PLASMA PLUME-SPACERAFT INTERACTION; A Passaro, A. Vicini, F. Nania, and L. Biagioni, Alta SpA, Pisa, I-56121, Italy

2005-175: ELECTRIC THRUSTER PLUME SIMULATION: APPLICATION TO MPD AND FEED THRUSTERS; A. Passaro, F. Nania, F. Paganucci, L. Biagioni, and L. Priami, Alta S.p.A. Pisa, Italy, 56121

2005-176: SCALABLE FLAT-PANEL NANO-PARTICLE MEMS/NEMS THRUSTER; L. Musinski, T. Liu, B. Gilchrist, A. Gallimore, and M. Keidar, University of Michigan, Ann Arbor, MI 48109, USA

2005-177: RESPONSE OF A CYLINDRICAL PLASMA TO TIME-VARYING EXTERNAL ELECTROMAGNETIC FIELD: NUMERICAL SIMULATION STUDIES; Yasushi Ikeda, Tohru Hada, Syuichi Matsukiyo, and Shunjiro Shinohara, Kyushu University, 6-1 Kasuga-Kohen, Kasuga, Fukuoka 816-8580, Japan; Kyoichiro Toki, Tokyo University of Agriculture and Technology, 2-24-16 Naka-cho, Koganei-shi, Tokyo 184-8588, Japan

2005-181: EVALUATION OF RADIOSOTOPE ELECTRIC PROPULSION FOR SELECTED INTERPLANETARY SCIENCE MISSIONS; David Oh and Eugen Bonfiglio, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109-8099; Mike Cupples and Jeremy Belcher, Science Applications International Corporation, Huntsville, Alabama, 35806

2005-183: ENDURANCE TESTS OF 150 µ FEEP MICROTHRUSTERS; M. Andrenucci, L. Biagioni, F. Ceccanti, and M. Saviozzi, Alta S.p.A., Pisa, 56121, Italy; D. Nicolini, European Space Technology Centre – ESA, Noordwijk, AG2200, The Netherlands

2005-184: MEASUREMENT FEATURES AND RESULTS OF TAL D-55 PLUME; Leonid E. Zakharenkov and Alexander V. Semenkin, Central Research Institute of Machine Building (TSNIIMASH), Pionerskaya 4, Korolev, Moscow region, 141070, Russia; Yuri V. Lebedev, Institute of Space Research, Moscow, Russia

2005-185: STUDY OF THE 3-TAL THRUSTER ASSEMBLY OPERATION; Leonid E. Zakharenkov, Alexander V. Semenkin and Valeri I. Garkusha, Central Research Institute of Machine Building (TSNIIMASH), Pionerskaya 4, Korolev, Moscow region, 141070, Russia; Yurii V. Lebedev, Institute of Space Research, Moscow, Russia

2005-186: HELICON MAGNETOPLASMADYNAMIC (HMPD) THRUSTER CONCEPT; Lachlan Blackhall, University of Sydney, Sydney, NSW, 2999, Australia

2005-187: HALL THRUSTER SCALING METHODOLOGY; Mariano Andrenucci, Alta S.p.A., 56121 Ospedaletto, Pisa, Italy; Francesco Battista and Pietro Piliero, Centrospazio, 56121 Ospedaletto, Pisa, Italy

2005-189: WALL EROSION IN 2D HALL THRUSTER SIMULATIONS; Emmanuelle Sommier, Michelle K. Allis, and Mark A. Cappelli, Stanford University, Stanford, CA, 94305

2005-191: PRELIMINARY TESTING OF A COAXIAL HALL THRUSTER WITH A DIAMOND NOSE CONE; Nicolas Gascon, W. Scott Crawford, Ronald L. Corey, and Mark A. Cappelli, Stanford University, Stanford, CA, 94305, USA; David White, WE Research, LLC, Rosamond, CA 93560, USA

2005-192: PERFORMANCE CHARACTERISITCS OF A LINEAR IONIC LIQUID ELECTROSPRAY THRUSTER; Paulo Lozano, Benajmin Glass and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, MA 02139, USA

2005-193: PLUME EFFECTS ON RADIATION DETECTION BY SPACECRAFT; Murat Celik and Manuel Martinez-Sanchezy, Massachusetts Institute of Technology, Cambridge, MA, 02139, USA

2005-194: XE+-SPUTTERED MOLYBDENUM PROPERTIES OF LOW IMPINGEMENT ENERGY; Mark W. Crofton, The Aerospace Corporation, El Segundo, CA 90245, USA; Johnathan C. Murray, The University of Michigan, Ann Arbor, MI 48109-2140, USA; James E. Pollard, The Aerospace Corporation, El Segundo, CA, 90245, USA

2005-195: THE CHARACTERIZATION OF SILICON WETTABILITY AND PROPERTIES OF EXTERNALLY WETTED MICROFABRICATED ELECTROSPRAY THRUSTER ARRAYS; Tanya Cruz Garza, Paulo Lozano, Luis F. Velásquez-Garc ía, and Manuel Martinez Sanchez, Massachusetts Institute of Technology, Cambridge, MA, 02139, USA

2005-196: HALL THRUSTER WITH AN EXTERNAL ACCELERATION ZONE; Nicolas Gascon, Ronald L. Corey, and Mark A. Cappelli, Stanford University, Stanford, CA, 94305, USA; William A. Hargus, Jr., Air Force Research Laboratory, Edwards AFB, 93524, USA

2005-197: A TWO-DIMENSIONAL (Z-0( FLUID/PIC SIMULATION OF COAXIAL HALL THRUSTERS; Eduardo Fernandez, Eckerd College, St. Petersburg, FL 33711; Aaron Knoll and Marck Cappelli, Stanford University, Stanford, CA 94035; Tarik Kaya, Carleton University, Ottawa, ON K1S 5B6, Canada

2005-198: ULTRA-LOW POWER STATIONARY PLASMA THRUSTER; Tsuyohito Ito, Nicolas Gascon, W. Scott Crawford, and Mark A. Cappelli, Stanford University, Stanford, California, 94305-3032, USA

2005-200: NUMERICAL SIMULATION OF THE HOLLOW CATHODE DISCHARGE PLASMA DYNAMICS; Ioannis G. Mikellides, Ira Katz, and Dan M. Goebel, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109

2005-201: DEVELOPMENT OF MAGNETOPLASMADYNAMIC SOLAR WIND SIMULATOR FOR MAGSAIL EXPERIMENT; Yukio Shimizu, Institute of Space and Astronautical Science (ISAS) of Japan Aerospace Exploration Agency (JAXA), Sagamihara 229-8510, Japan; Kyoichiro Toki, Tokyo University of Agriculture and Technology, Koganei 184-8588, Japan; Ikkoh  Funaki, Institute of Space and Astronautical Science (ISAS) of Japan Aerospace Exploration Agency (JAXA), Sagamihara 229-8510, Japan; Hidenori Kojima, Graduate School of Systems and Information Engineering, University of Tsukuba, Ibaraki, Japan; Hiroshi Yamakawa, Institute of Space and Astronautical Science (ISAS) of Japan Aerospace Exploration Agency (JAXA), Sagamihara 229-8510, Japan

2005-203: ELECTROSTATIC AND ELECTROMAGNETIC ACCELERATION IN A LASER-ELECTRIC HYBRID THRUSTER; Hideyuki Horisawa and Koki Sasaki, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Akira Igari, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo, Bunkyo-ku, Tokyo, 113-8856, Japan

2005-205: FAST ION EMISSION CHARACTERISTICS OF A FORWARD LASER PLASMA ACCELERATOR FOR SPACE PROPULSION APPLICATIONS; Hideyuki Horisawa and Masaya Izumi, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Takehito Takeda, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo, Bunkyo-ku, Tokyo, 113-8856, Japan

2005-206: NUMERICAL SIMULATION OF A MW-CLASS SELF FIELD MAGNETOPLASMADYNAMIC THRUSTER USING THE MACH 2 CODE; Brian L. England and Pavlos G. Mikellides, Arizona State University, Tempe, AZ, 85283, United States of America

2005-207: DESIGN RULES FOR HIGH-PERFORMANCE FARAD THRUSTERS; Kurt A. Polzin and Edgar Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey 08544

2005-208: INVESTIGATION AND OPTIMIZATION OF AN INSTATIONARY MPD THRUSTER IN IRS; Anuscheh Nawaz, Monika Auweter-Kurtz, Georg Herdrich and Helmut L. Kurtz, University of Stuttgart, Institut für Raumfahrtsysteme, 70550 Stuttgart, Germany

2005-209: THE PPS 1350 QUALIFICATION DEMONSTRATION 7500H ON GROUND, ABOUT 5000H IN FLIGHT; Frédéric R. Marchandise, Joel Biron, Marc Gambon, and Nicolas Cornu, Snecma, Division Moteurs Spatiaux, Site de Villaroche Nord, 77552 Moissy-Cramayel, France; Frank Darnon, CNES, Avenue Edouard Belin, 31000 Toulouse, France; Denis Estublier, ESTEC, Keplerlaan 1, 22000 Noordwijk ZH, The Netherlands

2005-211: MISSION DESIGN FOR THE INNOVATIVE INTERSTELLAR EXPLORER VISION MISSION; Douglas I. Fiehler, QSS Group, Inc., - NASA Glenn Research Center, Cleveland, OH, 44135, USA; Ralph L. McNutt, Jr., Johns Hopkins University Applied Physics Laboratory, Laurel, MD, 20723, USA

2005-212: A 3.000 HOURS ENDURANCE TESTING OF RIT-22 THRUSTER IN THE NEW AEROSPAZIO TEST FACILITY; E. Bonelli, S. Scaranzin, F. Scortecci and F. Saito, AEROSPAZIO Tecnologie s.r.l., Rapolano Terne, Siena, 53040, Italy; R. Killinger, R. Kukies and H. Leiter, EADS Space Transportation, Möchmühl, 74215, Germany

2005-213: THE THRUSTER MODULE ASSEMBLY (HALL EFFECT THRUSTER) DESIGN, QUALIFICATION AND FLIGHT; Joel Biron, Nicolas Cornu, Hubert Illand, and Marc Serrau, SNECMA, Division Moteurs Spatiaux, Site de Villaroche Nord, Direction Propulsion et Equipements Satellites, Aérodrome de Melun-Villaroche, 77552 Moissy-Cramayel, France; Richard Rigollet, EADS ASTRIUM SAS, 31, rue des cosmonauts, 31402 Toulouse Cedex 4, France; Howard L. Gray, EADS ASTRIUM Ltd., Anchorage Road, Portsmouth, PO3 5PU, UK

2005-214: NUMERICAL SIMULATION OF THE INTERACTIONS BETWEEN SOLAR ARRAYS AND THE SURROUNDING PLASMA ENVIRONMENT; R. Sedmik, C. Scharlemanny, and M. Tajmarz, ARC Seibersdorf research Gmbh., Seibersdorf, A-2444, Austria; J. Gonzalez del Amox, A. Hilgers and D. Estublierk, ESA-ESTEC, Keplerlaan 1, 2200 AG Noordwijk, The Netherlands; G. Noci and M. Capacciyy, LABEN, Proel, Firenze, Italy; C. Koppelzz, Snecma Safran Group, Site de Villaroche Nord, BP No 93, 77552, Moissy Cramayel Cedex, France

2005-215: THRUST STAND FOR APPLIED-FIELD MPD THRUSTERS; James H. Gilland, Ohio Aerospace Institute, Brookpark, OH, 44142, USA; Mitchell L. R. Walker, Georgia Institute of Technology, Atlanta, GA, 30332, USA; Eric J. Pencil, NASA Glenn Research Center, Cleveland, OH 44135, USA

2005-219: ADEQUATE ELECTRIC PROPULSION SYSTEM PARAMETERS FOR PILOTED MARS MISSIONS; Tanja D. Schmidt, German Aerospace Center (DLR), Cologne, 51147, Germany; Monika Auweter-Kurtz, Institut für Raumfahrtsysteme (IRS), Universität Stuttgart, Stuttgart 70550, Germany

2005-221: SPECTRAL CHARACTERISTICS OF RADIATED EMISSION FROM SPT-100 HALL THRUSTERS; Edward J. Beiting, Michael L. Garrett, and James E. Pollard, The Aerospace Corporation, Los Angeles, CA 90009, USA; Bernard Pezet and Patrice Gouvermayre, 31, rue des Cosmonautes, 31402 Toulouse Cedex 4, France

2005-222: TEMPORAL CHARACTERISTICS OF RADIATED EMISSION FROM SPT-100 HALL THRUSTERS IN THE L, S, AND C BANDS; Edward J. Beiting, Michael L. Garrett, and James E. Pollard, The Aerospace Corporation, Los Angeles, CA 90009, USA; Bernard Pezet and Patrice Gouvernayre, 31, rue des Cosmonautes, 31402 Toulouse Cedex 4, France

2005-224: IN-FEEP CLUSTER FOR LISA PATHFINDER; N. Buldrini, A. Genovese, and M. Tajmal, ARC Seibersdorf Research, Seibersdorf A-2444, Austria

2005-226: MISSION ANALYSIS, SPACECRAFT CONCEPT AND ION THRUSTER DESIGN FOR A LOW-COST RENDEZVOUS WITH AND ASTEROID; David G. Fearn, EP Solutions, Fleet, Hampshire, GU52 6HS, UK

2005-227: ORBIT-RAISING, PAST AND PRESENT – THE X-SERIES OF SPACECRAFT AND ARTEMIS; David G. Fearn, EP Solutions, Fleet, Hampshire, GU52 6HS, UK

2005-228: COMBINED PLASMA AND THERMAL HOLLOW CATHODE INSERT MODEL; Ira Katz, James E. Polk, Ioannis G. Mikellides, Dan M. Goebel and Sarah E. Hornbeck, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109

2005-230: MAGNETIC NOZZLE DESIGN FOR HIGH-POWER MPD THRUSTERS; Robert P. Hoyt, Tethers Unlimited, Inc., Bothell, WA, 98011, USA

2005-231: PERFORMANCE IMPROVEMENT DUE TO KINK INSTABILITY SUPPRESSION IN MPD THRUSTERS; E. Martines, M. Zuin, M. Bagatin, r. Cavazzana, G. Serianni, and V. Antoni, Consorzio RFX, Associazione Euratom-Enea sulla Fusione, corso Stati Uniti 4, 35127 Padova, Italy; P. Rossetti and M. Signori, Alta/Centrospazio, via A. Gherardesca 5, 56014 Pisa, Italy; F. Paganucci and M. Andrenucci, Department of Aerospace Engineering, University of Pisa, via Caruso, 56122 Pisa, Italy

2005-232: MAGNETICALLY GUIDED LASER ABLATION FOR HIGH SPECIFIC IMPLUSE THRUSTERS; Sohail H. Zaidi, Thomas W. Smith, Robert Murray, and Richard B. Miles, Princeton University, Princeton, NJ 08540, USA

2005-233: FEASIBILITY STUDY ON HIGH SPECIFIC IMPULSE ION THRUSTER WITH C/C GRID SYSTEM; Yoshinori Nakayama, National Defense Academy, Yokosuka, Kanagawa, 329-8686, Japan; Ikkoh Funaki and Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2005-234: STUDY ON PULSED PLASMA THRUSTER CONFIGURATION TO EXPAND IMPULSE BIT RANGE; Junji Uezu and Junpei Lio, Tokyo Metropolitan Institute of Technology (presently, Tokyo Metropolitan Univeristy), Asahigaoka 6-6, Hino, Tokyo, 191-0065, Japan; Yukiya Kamishima and Haruki Takegahara, Tokyo Metropolitan University, Asahigaoka 6-6, Hino, Tokyo, 191-0065, Japan; Takashi Wakizono, HI-SERVE Corporation, Totohara 780-7, Akiruno, Tokyo, 190-0152, Japan; Mitsuteru Sugiki, Astro Research Corporation, Godo-cho 134, Hodogaya-ku, Yokohama, Kanagawa, 240-0005, Japan

2005-235: DIRECT THRUST MEASUREMENT OF IN-FEEP CLUSTERS; K. Marhold and M. Tajmar, ARC Seibersdorf research GmbH, A-2444 Seibersdorf, Austria

2005-236: EVALUATION ON IMPULSE BIT CHARACTERISTICS OF PULSED PLASMA THRUSTER BY SINGLE IMPULSE MEASUREMENT; Junpei Lio, Junji Uezu, and Tadanori Fukushima, Tokyo Metropolitan Institute of Technology (presently Tokyo Metropolitan University), Japan; Yukiya Kamishima and Haruki Takegahara, Toyko Metropolitan University, Japan

2005-238: AN OVERVIEW OF THE VHITAL PROGRAM: A TWO-STAGE BISMUTH FED VERY HIGH SPECIFIC IMPULSE THRUSTER WITH ANODE LAYER; Anita Sengupta and Colleen Marrese-Reading, Jet Propulsion Laboratory, Pasadena, CA, 91109, US; Mark Cappelli and David Scharfe, Stanford University, Stanford, CA, 94305, US; Sergey Tverdokhlebov, Sasha Semenkin, and Oleg Tverdokhlebov, TsNIIMASH Export, Moscow, Russia; Ian Boyd and Michael Keidar, University of Michigan, Ann Arbor, MI, 48109, US; Azer Yalin and Vijaya Surla, Colorado State University, Fort Collins, CO, 80523, US; Tom Markusic and Kurt Polzin, NASA Marshall Space Flight Center, Huntsville, AL, US

2005-244: GRID GAP MEASUREMENT FOR AN NSTAR ION THRUSTER; Esther M. Diaz and George C. Soulas, National Aeronautics and Space Administration, Cleveland, OH, 44135, United States

2005-245: SMART-1 ELECTRIC PROPULSION OPERATIONAL EXPERIENCE; D. Milligan, D. Gestal, O. Camino, and P. Pardo-Voss, European Space Operations Centre, Robert Bosch Str. 5, 64293, Darmstadt, Germany; D. Estublier, ESA/ESTEC, Kepleraan 1, Noordwijk, The Netherlands; C. Koppel, Snecma Moteurs, Division Moteurs-Spatiaux, Villaroche Nord, France

2005-246: OPERATIONALLY ENHANCED ELECTRIC PROPULSION PERFORMANCE ON ELECTRICALLY PROPELLED SPACECRAFT; D. Milligan, D. Gestal, O. Camino, and P. Bearman, European Space Operations Centre, Robert Bosch Str. 5, 64293, Darnstadt, Germany; C. Koppel, Snecma Moteurs, Division Moteurs-Spatiaux, Villaroche Nord, France

2005-248: CALCULATION OF THERMALLY-INDUCED DISPLACEMENTS IN SPHERICALLY DOMED ION ENGINE GRIDS; George C. Soulas, NASA Glenn Research Center, Cleveland, OH 44135, USA

2005-252: PERFORMANCE MAPPING OF NEW GN-RITS AT GIESSEN, D. Feili, H. W. Loeb, K. H. Schartner, St. Weis, D. Kirmse, and B. K. Meyer, Electric Propulsion, Giessen University, Giessen, D-35390, Germany; R. Kilinger and H. Mueller, EADS-ST, Moekuehl, D-74215, Germany; Davina Mafia Di Cara, ESA/ESTEC – Electric Propulsion Section, Keplerlaan 1, 2200 AG Noordwijk ZH, The Netherlands

2005-256: PROGRESS ON THE DEVELOPMENT OF A DIRECT EVAPORATION BISMUTH HALL THRUSTER; Dean R. Massey and Lyon B. King, Michigan Technological University Ion Space Propulsion Lab Houghton, MI 49931, United States of America

2005-257: THRUST CHARACTERIZATION OF A T6 HOLLOW CATHODE; Paolo Gessini and Stephen B. Gabriel, University of Southampton, Southampton, Hants, SO17 1BJ, United Kingdom; David G. Fearn, EP Solutions, Fleet, Hants, GU14 0LX, United Kingdom

2005-258: A (RE-) EXAMINATION OF ELECTRON MOTION IN HALL THRUSTER FIELDS; Lyon B. King, Michigan Technological University, Houghton, Michigan, 49931, USA

2005-260: PRELININARY WEAR ANALYSIS FOLLOWING A 2000 H WEAR TEST OF THE HIPEP ION THRUSTER; George J. Williams Jr., The Ohio Aerospace Institute, Cleveland, OH, 44135, USA; Tyler A. Hickman, Thomas W. Haag, John E. Foster, and Michael J. Patterson, NASA Glenn Research Center, Cleveland, OH, 44135, USA

2005-265: VACUUM TESTING OF THE MINIATURE RADIO-FREQUENCY ION THRUSTER; Valerie F. Mistoco, Thomas A. Trudel, Sven G. Bilen and Michael M. Micci, The Pennsylvania State University, University Park, PA, 16802 USA

2005-266: ENERGETIC ION PRODUCTION AND KEEPER EROSION IN HOLLOW CATHODE DISCHARGES; Dan M. Goebel, Kristina Jameson, Ira Katz, and Ioannis G. Mikellides, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2005-269: HOLLOW CATHODE AND THRUSTER DISCHARGE CHAMBER PLASMA MEASUREMENTS USING HIGH-SPEED SCANNING PROBES; Kristina K. Jameson, Dan M. Goebel, and Ron M. Watkins, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2005-270: MODELING ION BEAM NEUTRALIZATION AND NEAR-THRUSTER PLUME INTERACTIONS; Lubos Brieda and Douglas VanGilder, Air Force Research Laboratory, Edwards AFB, CA 93524; Joseph Wang, Virginia Polytechnic Institute and State University, Blacksburg, VA, 24061-0203

2005-271: ION PROPULSION SIMULATIONS USING PARALLEL SUPERCOMPUTER; J. Wang, Y. Cao, R. Kafafy, and J. Pierru, Virginia Polytechnic Institute and State University, Blacksburg, VA, 24061, USA; V. Decyk, University of California, Los Angles, CA 90095, USA

2005-272: HIGH POWER ECR ION THRUSTER DISCHARGE CHARACTERIZATION; John E. Foster, Hani Kamhawi, Tom Haag, Christian Carpenter, and George Williams, NASA Glenn Research Center, Cleveland, OH, 44135

2005-274: ELETRON DYNAMICS OF A NON-NEUTRAL ELECTRON PLASMA IN THE DEFINING FIELDS OF A HALL-EFFECT THRUSTER; Emily C. Fossum, Lyon B. King, and Jerry L. Ross, Michigan Technological University, Houghton, MI, 49931, U.S.A.

2005-275: ARCJET STAGE INVESTIGATION AND INDUCTIVE HYDROGEN HEATING IN THE TIHTUS ENGINE; Hannah Böhrk, Dejan Petkow, Georg Herdrich, Monika Auweter-Kurtz, and Helmut Kurtz, Institut für Raumfahrtsysteme, Universität Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Germany

2005-276: COMPACT HIGH VOLTAGE POWER PROCESSING FOR FIELD EMISSION ELECTRIC PROPULSION (FEEP); Matthias Gollor, EADS Astrium, Electronics Division, 88039 Friedrichshafen, Germany and Fachhochschule Konstanz – University of Applied Science – Dept. of Electrical Engineering, 78462 Konstanz, Brauneggerstr. 55D, Germany; Klaus Breier, EADS Astrium, Electronics Division, 88039 Friedrichshafen, Germany

2005-277: HOLLOW CATHODES STUDY AT ALTA-CENTROSPAZIO; P. Rossetti and M. Signori, Alta SpA-Centrospazio, Pisa, I-56121, Italy; M. Andrenucci and F. Paganucci, University of Pisa, Pisa, I-56100 Italy

2005-278: GENERIC HIGH VOLTAGE POWER MODULE FOR ELECTRICAL PROPULSION; Michael Boss, Frank Herty, and Kurt Rogalla, EADS Astrium, Electronics Division, 88039 Friedrichshafen, Germany; Matthias Gollo, EADS Astrium, Electronics Division, 88039 Friedrichshafen, Germany and Fachhochschule Konstanz – University of Applied Science – Dept. of Electrical Engineering, 78462 Konstanz, Brauneggerstr. 55D, Germany

2005-281: RESULTS OF A 2000-HOUR WEAR TEST OF THE NEXIS ION ENGINE; John Steven Snyder, Dan M. Goebel, James E. Polk, Analyn C. Schneider, and Anita Sengupta, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109

2005-282: PERFORMANCE EVALUATION OF A HIGH ENERGY PULSED PLASMA THRUSTER II; Hani Kamhawi, NASA Glenn Research Center at Lewis Field, Cleveland, Ohio, 44135; Lynn Arrington, QSS Group, Cleveland, Ohio, 44135; Eric Pencil and Thomas Haag, NASA Glenn Research Center at Lewis Field, Cleveland, Ohio, 44135

2005-283: INVESTIGATION OF VARIOUS MICROWAVE ELECTRON CYCLOTRON RESONANCE CATHODE CONFIGURATIONS; Hani Kamkawi, and John E. Foster, NASA Glenn Research Center, Cleveland, Ohio 44135

2005-284: INVESTIGATION OF VARIOUS MICROWAVE ELECTRON CYCLOTRON RESONANCE CATHODE CONFIGURATIONS; Hani Kamhawi and John E. Foster, NASA Glenn Research Center, Cleveland, Ohio 44135

2005-285: NEXT MULTI ION ENGINE TEST: PLUME MODELING AND TEST PLANS; Myron J. Mandell, Science Applications International Corporation, San Diego, CA

2005-287: SPECTROSCOPIC INVESTIGATION OF THE STEADY STATE CHARACTERISTICS OF HOLLOW CATHODE INTERNAL PLASMAS; S. J. Pottinger and S. B. Gabriely, University of Southampton, Higheld, Hampshire, SO17 1BJ, United Kingdom

2005-289: MEASUREMENTS OF ION ENERGIZATION BY A PAIR OF BEATING ELECTROSTATIC ION CYCLOTRON WAVES; R. Spektorand and Edgar Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Princeton University, Princeton, New Jersey 08544

2005-290: HELICON DOUBLE LAYER THRUSTERS; C. Charles, P. Alexander, C. Costa, O. Sutherland, R. W. Boswell, Plasma Research Laboratory, RSPHYSSE, The Australian National University, Canberra, ACT 0200, Australia; L. Pfitzner and R. Franzen, AUSPACE, Canberra, Australia; J. Kingwell and A. Parfitt, Cooperative Research Centre (CRC) for Satellites Systems, Canberra, Australia; P.E. Frigot, J. Gonzalez del Amo, E. Gengembre, and G. Saccoccia, Propulsion and Aerothermodynamics Division, European Space Agency, ESTEC, The European Space Agency, The Netherlands

2005-292: NUMERICAL SIMULATIONS DEVELOPED AT ALCATEL ALENIA SPACE FOR ELECTRIC PROPULSION EFFECTS ON SATELLITE; Sylvie Brosse, Sébastien Clerc, and Véronique Perrin, Alcatel Alenia Space, 100 Bd Du MIDI, 06156 Cannes La Bocca, France

2005-293: DIFFERENTIAL SPUTTERING YIELDS OF REFRACTORY METALS BY XENON, KRYPTON, AND ARGON ION BOMBARDMENT AT NORMAL AND OBLIQUE INCIDENCES; Kirk A. Zoerb, John D. Williams, Desiree D. Williams, and Azer P. Yalin, Colorado State University, Fort Collins, CO, 80523, USA

2005-294: DIRECT AND REMOTE MEASUREMENTS OF PLASMA PROPERTIES NEARBY HOLLOW CATHODES; Russell H. Martin, Casey C. Farnell, and John Williams, Dept. of Mechanical Engineering, Colorado State University, Fort Collins, Colorado 80523

2005-295: ELECTROMAGNETIC PUMPS FOR CONDUCTIVE-PROPELLANT FEED SYSTEMS; Thomas E. Markusic, Kurt A. Polzin, and Amado Dehoyos, Propulsion Research Center, NASA – Marshall Space Flight Center, Huntsville, Alabama 35812

2005-296: MULTI-MEGAWATT PROPULSION BASED ON A COMPACT TOROID THRUSTER; John Slough, University of Washington, Seattle, WA, 98195, USA

2005-297: DEVELOPMENT & TEST STATUS OF THE THALES HIGH EFFICIENCY MULTISTAGE PLASMA (HEMP) THRUSTER FAMILY; N. Koch, H.-P. Harmann and G. Kornfeld, THALES Electron Devices GmbH, Söflingerstr. 100, 89073 Ulm, Germany

2005-298: DEVELOPMENT & TEST STATUS OF THE THALES W/OS MIXED METAL METRIX HOLLOW CATHODE NEUTRALISER HKN5000 G. Kornfeld, N. Koch, and H. –P. Harmann, THALES Electron Devices GmbH, Söflingerstr. 100, 89077 Ulm, Germany

2005-299: EROSION MEASUREMENTS BY CAVITY RING-DOWN SPECTROSCOPY FOR THE VHITAL PROGRAM; Azer P. Yalin Vijaya Surla, and John D. Williams, Colorado State University, Fort Collins, Colorado, 80523

2005-300: DETERMINATION OF NUMBER DENSITY AND VELOCITY OF SPUTTERED PARTICLES BY CAVITY RING-DOWN SPECTROSCOPY; Azer P. Yalin and Vijaya Surla, Colorado State University, Fort Collins, Colorado, 80523

2005-301: NONAMBIPOLAR ELECTRON SOURCE FOR NEUTRALIZATION OF ION AND HALL THRUSTERS; Ben W. Longmier and Noah Hershkowitz, University of Wisconsin – Madison, Madison, WI 53706, US

2005-302: CHARACTERIZATION OF COLLOID THRUSTER BEAMS; M. Gamero-Castaño and J. Ziemer, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91108, USA

2005-303: ESTIMATION OF HALL THRUSTER EROSION USING HPHALL; M. Gamero-Castaño and I. Katz, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91108, USA

2005-304: THRUUST IMPROVEMENT OF THE MAGNETICALLY ENHANCED VACUUM ARC THRUSTER (MVAT); Benjamin Tang, Luke Idzkowski, Michael Au, Don Parks, and Mahadevan Krishnan, Alameda Applied Sciences Corporation, San Leandro, CA, 94577, USA; John Ziemer, NASA Jet Propulsion Laboratory, Pasadena, CA, 91109, USA

2005-306: TESTING OF THE NASA GSFC MEMS COLLOIDAL THRUSTER; Eric H. Cardiff, Brad Degen, Abraham Grindle, Brian Jamieson, Loral O’Hara, Kevin Pearce, and Patrick Roman, NASA Goddard Space Flight Center, Greenbelt, MD, 20771, USA

2005-309: TEMPORAL BEHAVIOR OF THE ION VELOCITY DISTRIBUTION FUNCTIONS IN PULSED HELICON PLASMA SOURCES; Costel Biloiu, Xuan Sun, and Earl Scimej, West Virginia University, Morgantown, West Virginia 26506, USA; Edgar Choueiri and Rostislav Spektor, Department of Mechanical and Aerospace Engineering, Princeton University Princeton, New Jersey, 08544, USA

2005-310: LASER PROPULSION FOR GROUND TO ORBIT LAUNCH; David P. Resendes, Sérgio Mota and José T. Mendonca, Instituto Superior Técnico, Lisboa, Portugal; Berry Sanders, TNO Prins Maurits Laboratory Rijswijk, The Netherlands; Joäo Encarnocäo, T. U. Delft, Delft, The Netherlands; Jose Gonzalez del Amo, European Space Agency, ESTEC

2005-314: HOLLOW CATHODE IGNITION STUDIES AND MODEL DEVELOPMENT; William G. Tighe and Kuei-Ru Chien, L-3 Communications Electron Technologies, Inc., Torrance, CA, 90505; Dan M. Goebel, Jet Propulsion Laboratory, Pasadena, CA, 91109; Robert T. Longo, Private Consultant, Arcadia, CA 91007

2005-315: L-C COMMUNICATIONS ETI ELECTRIC PROPULSION OVERVIEW; Kuei-Ru Chien, Stephen L. Hart, William G. Tighe, Michael K De Pano, Thomas A. Bond, and Rafael Spears, L-3 Commmunications Electron Technologies, Inc., 3100 W. Lomita Blvd.,  Torrance, California 90509, USA

2005-316: INVESTIGATION AND DEVELOPMENT OF A HIGH VOLTAGE PROPELLANT ISOLATOR FOR ION THRUSTERS; Stephen L. Hart, William Tighe, and Charles Pearce, L-3 Communications Electron Technologies, Inc., Torrance, CA, 90505; Dan M. Goebel, Jet Propulsion Laboratory, Pasadena, CA, 91109

2005-318: A 25NH LOW-NOISE THRUST STAND FOR MICROTHRUSTERS; Claude R. Phipps and James R. Luke, Photonic Associates, LLC, Santa Fe, NM 87508; Wesley D. Helgeson, NMT/IERA, Albuquerque, NM 87106

2005-320: A SOLAR ELECTRIC PROPULSION CARGO VEHICLE TO SUPPORT NASA LUNAR EXPLORATION PROGRAM; Ronald Spores and Jeff Monheiser, Aerojet Corporation, Redmond, WA 98073; Brian P. Dempsey, Darren Wade, and Kenneth Creel, Lockheed Martin, Denver, CO 80201; David Jacobson, NASA Glenn Research Center, Cleveland, OH 44135; Geoff Drummond, Colorado Power Electronics, Inc. Fort Collins, CO 80524

2005-321: CHARATERIZATION OF A HIGH CURRENT, LONG LIFE HOLLOW CATHODE; Jonathan L. Van Noord, Hani Kamhawi and Heather K. McEwen, NASA Glenn Research Center, Cleveland, OH, 44135

2005-323: AMBITIOUS CHALLENGES OF JAPANESE ELECTRIC PROPULSION; Hitoshi Kuninaka, ISAS/JAXA, Yoshinodai, Sagamihara, Kanagawa, Japan

2005-324: CHARACTERIZATION OF A HIGH SPECIFIC IMPULSE XENON HALL EFFECT THRUSTER; James J. Szabo, Busek Co. Inc., Natick, MA, 01760, USA; Yassir Azziz, MIT, Cambridge, MA, 02139, USA

2005 FILE DIRECTORY

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2007 INDEX

2007-001: CALCULATING SPUTTER RATE ANGULAR DEPENDENCE USING OPTICAL PROFILOMETRY; Alexander C. Barrie and Bryan S. Taylor, Advatech Pacific, Inc., Palmdale, CA, 93550, United States; Jared M. Ekholm and William H. Hargus, Air Force Research Laboratory, 1 Ara Rd., Edwards AFB, CA, United States

2007-002: NUMERICAL PROCEDURE PERMITTING CALCULATION OF HOW A VACUUM CHAMBER INFLUENCES ELECTRIC PROPULSION THRUSTER JET EXPANSION; Grigory Toropov, Moscow Aviation Institute (State Technical University) MAI, Electric Propulsion and Space Power Plants Department, 4, Volokolamskoe sh., Moscow, 125971, Russia; Vladimir Chervakov, Moscow Aviation Institute (State Technical University) MAI, Electric Propulsion and Space Power Plants Department, 4, Volokolamskoe sh., Moscow, 125971, Russia

2007-004: A 3D BOUNDARY SHEATH ANALYSIS ON FARADAY PROBE MEASUREMENTS IN A NON-EQUILIBRIUM PLASMA; Grigory Toropov, Moscow Aviation Institute  (State Technical University) MAI, Engineering Plasma Computational Laboratory (EPCLab), 24b-I20, Zalineynaya str., Vologda, 160010, Russia

2007-005: SUMMARY OF THE VHITAL THRUSTER TECHNOLOGY DEMONSTRATION PROGRAM: A TWO-STAGE BISMUTH-FED VERY HIGH SPECIFIC IMPULSE TAL; Anita Sengupta and Colleen Marrese-Reading; Jet Propulsion Laboratory, Pasadena, CA, 91109, US; Alexander Semenkin, Leonid Zakharenkov, Sergey Tverdokhlebov, and Oleg Tverdokhlebov, TsNIIMASH Export, Moscow-Region, Russia; Kurt Polzin and Tom Markusic, NASA Marshall Space Flight Center, Huntsville, AL, US; Marck Cappelli and David Scharfe, Stanford University, Stanford, CA, 94305, US; Ian Boyd and Michael Keidar, University of Michigan, Ann Arbor, MI, 48109, US; Azer Yalin and Vijaya Surla, Colorado State University, Fort Collins, CO, 80523, US

2007-006: PLASMA PARAMETERS INVESTIGATION IN THE NEAR CATHODE ZONE OF THE SPT DISCHARGE; Sergey A. Khartov and Igor P. Nazarenko, Moscow Aviation Institute (State University of Aerospace Technologies) MAI, Moscow, Russia; Andrey A. Pereslavtsev, Moscow Aviation Institute (State University of Aerospace Technologies) MAI, Moscow, Russia

2007-007: SPUTTERING PROCESS OF BN BASED CERAMIC BY THE FLOWS OF NONCOMPENSATIED CHARGE PLASMA; Elvira N. Nikiporetz and Alexander A. Semenov, Moscow Aviation Institute (State University of Aerospace Technologies) MAI, Moscow, Russia; Igor I. Shkarban, Moscow Aviation Institute (State University of Aerospace Technologies) MAI, Moscow, Russia; Elena S. Khartova, Moscow Aviation Institute (State University of Aerospace Technologies) MAI, Moscow, Russia

2007-008: ELECTRON-ENHANCED DESORPTION INFLUENCE ON THE SPT ISOLATOR WALL EROISION PROCESSES; Sergey S. Elovikov, Moscow State University, (MGU) Moscow, Russia; Sergey A. Khartov, Moscow Aviation Institute (State University of Aerospace Technologies) MAI, Moscow, Russia

2007-009: RE-IGNITION OF MICROWAVE DISCHARGE ION ENGINES ON HAYABUSA FOR HOMEWARD JOURNEY; Hitoshi Kuninaka, Kazutaka Nishiyama, Yukio Shimizu, Tetsuya Yamada, Ikko Funaki, Satoshi Hosoda, and Hiroyuki Koizumi, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Yoshinodai, Sagamihara, Kanagawa 229, Japan

2007-010: SENSITIVITY TESTING OF THE NSTAR ION THRUSTER; Anita Sengupta, John Anderson, and John Brophy, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109, US

2007-011: A STUDY OF SOME PHYSICAL PROCESSES IN HALL THRUSTER OPERATED IN THE DISCHARGE VOLTAGE UP TO 1000 V; Oghienko (Ogiienko) Sergii, Bilokon Volodymyr, and Oransky Anatoliy, Zhukovski National airspace university “Kharkov Aviation institute”, Ukraine; Bober Alexander, Asher Space Research Institute, TECHNION-Israeli Institute of technology, Israel

2007-012: SEVEN YEARS OF HALL THRUSTER MODELING: AN EUROPEAN COLLABORATION BETWEEN BARI AND GREIFSWALD; F. Taccogna, S. Longo, and M. Capitelli, Dip, Di Chimica, Universitá degli Studi di Bari & IMIP-CNR, Sect. Bari, via Orabona 4, Bari, I-70126, Italy; R. Schneider, Max-Planck Institute für Plasmaphysik, EURATOME Association, Wendelsteinstr. 1, Greifswald, D-17491, Germany

2007-014: INITIATION OF THE NUMERICAL INVESTIGATION OF THE HYBRID PLASMA THRUSTER TIHTUS; Uwe Bauder, Markus Fertig, Hannah Böhrk, Georg Herdrich, and Dejan Petkow, Institut für Raumfahrtsysteme, Universität Stuttgart, 70550 Stuttgart, Germany; Monika Auweter-Kurtz, Universität Hamburg, 20146 Hamburg, Germany

2007-015: PLASMA SAIL PROPULSION BASED ON THE PLASMA MAGNET; John Slough, University of Washington, Seattle, WA, 98195, USA

2007-016: MAGNETICALLY ACCELERATED PLASMOID (MAP) THRUSTER – INITIAL RESULTS AND FUTURE PLANS; John Slough, Arthur Blair, Chris Pihl, and George Votroubek, MSNW, Redmond, WA 98052, USA

2007-017: PLASMA HEATING OF INERT GAS HOLLOW CATHODE INSERTS; Ira Katz, Ioannis G. Mikellides, Dan M. Goebel, and James E. Polk, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109

2007-018: NUMERICAL SIMULATIONS OF A HALL THRUSTER HOLLOW CATHODE PLASMA; Ioannis G. Mikellides, Ira Katz, Kristina K. Jameson, and Dan M. Goebel, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109

2007-019: MICRO-NEWTON RIT POWER CONTROL UNIT DEVELOPMENT; Matthias Gollor, Professor, University of Applied Science Konstanz – Electrical Engineering; Michael Boss, Rafael Braeg, Andreas Franke, Frank Herty, and Bernhard Kiewe, Astrium GmbH – Friedrichshafen – Germany, Dept. Electronics Equipment Germany – ASE2

2007-020: ELECTRIC PROPULSION ELECTRONICS ACTIVITIES IN ASTRIUM GERMANY; Matthias Gollor, Professor, University of Applied Science Konstanz (Germany) – Electrical  Engineering; Michael Boss, Astrium GmbH – Friedrichshafen – Germany, Dept. Electronics Equipment Germany – ASE2

2007-021: GENERIC HIGH VOLTAGE POWER SUPPLIES (HVPS) WITH OPTIMUM EFFICIENCY AND MULTI-RANGE; Matthias Gollor, Professor, University of Applied Science Konstanz (Germany) – Electrical Engineering; Michael Boss, Frank Herty, and Bernhand Kiewe, Astrium GmbH – Friedrichshafen – Germany, Dept. of Electronics Equipment Germany – ASE2

2007-023: HOLLOW CATHODE EMISSION AND IGNITION STUDIES AT L-3 ETI; William G. Tighe and Kuei-Ru Chien, L-3 Communications Electron Technologies, Inc., Torrance, CA, 90505; Dan M. Goebel, Jet Propulsion Laboratory, Pasadena, CA, 91109; Robert T. Longo, Private Consultant, Arcadia, CA, 91007

2007-024: ION THRUSTER DEVELOPMENT AT L-3 ETI FOR SMALL SATELLITE APPLICATIONS; William G. Tighe, Kuei-Ru Chien, and Rafael Spears, L-3 Communications Electron Technologies, Inc., Torrance, CA, 90505; Dan M. Goebel, Jet Propulsion Laboratory, Pasadena, CA, 91109

2007-025: TWO-DIMENSIONAL CHARACTERIZATION OF MICROWAVE E-FIELDS AND BEAM PROFILES OF THE ECR ION THRUSTER µ20; Kazutaka Nishiyama and Hitoshi Kuninaka, Japan Aerospace Exploration Agency / Institute of Space and Astronautical Science, Sagamihara, Kanagawa, 229-8510, Japan; Tatsuya Nakai, The University of Tokyo, Bunkyo-ku, Tokyo, 113-8656, Japan

2007-026: INVESTIGATION OF INTEGRAL CHARACTERISTICS OF THE LOW POWER HALL THRUSTER FOR THE SPACECRAFT ORIENTATION PROPULSION SYSTEM DURING TRANSITION TO THE STATIONARY OPERATION MODE AFTER THRUSTER START UP; Oghienko (Ogiienko) Sergii, Zhukovksy National Aerospace University “Kharkov Aviation Institute”, Ukraine

2007-027: IN-SPACE PROPULSION INFLUENCES ON COMSAT MISSIONS; David C. Byers, Las Vegas, NV, 89103, U.S.A.; John W. Dankanich, Gray Research Inc., Cleveland, OH, 44135, U.S.A.

2007-029: NUMERICAL ANALYSIS AND EXPERIMENTS OF A MICROWAVE-EXCITED MICROPLASMA THRUSTER; Takeshi Takahashi, Yoshinori Takao, Koji Eriguchi and Kouichi Ono, Graduate School of Engineering, Kyoto University, Kyoto, 606-8501, Japan

2007-030: SPACECRAFT MOTION AND ATTITUDE CONTROL IN THE HIGH ELLIPTIC ORBIT; V.A. Obukhov, A. I. Pokryshkin, and G. A. Popov, Leningradskoe shosse, 5, 125080 Moscow, Russia; N. V. Yashina, Volokolamskoe shosse, 4. 125871, Moscow, Russia

2007-031: INVESTIGATION OF HIGH-ENERGY IONS WITH HIGH-ANGLE TRAJECTORIES IN HALL THRUSTERS PLUMES; Regina M. Sullivan, California Institute of Technology, Pasadena, CA, 91125, U.S.A.; Paul A. Torrey, Cornell University, Ithaca, NY, 14853, U.S.A.; Lee K. Johnson, Jet Propulsion Laboratory, Pasadenca, CA, 91109, U.S.A.

2007-032: MEASUREMENT OF MAGNETIC DETACHMENT EFFECTS IN A MAGNETIC NOZZLE; Christopher Deline and Brian Gilchrist, University of Michigan, Ann Arbor, MI, 48109; Jared Squire, Ad Astra Rocket Company, Houston, TX, 77058; Jonathan Jones, Greg Chavers, and Chris Dobson, NASA Marshall S pace Flight Center, Huntsville, AL 35805; Roger Bengston, University of Texas, Austin, TX 78712

2007-033: NEXT LONG-DURATION TEST AFTER 11, 570 H AND 237 KG OF XENON PROCESSED; Daniel A. Herman, ASRC Aerospace Corporation, Cleveland, OH, 44135, USA; George C. Soulas and Michael J. Patterson, NASA Glenn Research Center, Cleveland, OH, 44135, USA

2007-034: HALL THRUSTER EROSION PREDICTION USING A HYDRODYNAMIC PLASMA MODEL AND SPUTTERING SIMULATION; John T. Yim and Iain D. Boyd, University of Michigan, Ann Arbor, MI, 48109, USA; Michael Keidar, George Washington University, Wasghington, DC, 20052, USA

2007-035: A SIMPLE ELECTRIC THRUSTER BASED ON ION CHARGE EXCHANGE; Joe Khachan and Lachlan Blackhall, University of Sydney, Sydney, NSW, 2006, Australia

2007-036: LONGE RANGE PARTICLE COLLISIONS FOR THE PIC/DSMC SIMULATION CODE PICLAS; Danilo D’Andrea and Rudolf Schneider, Forschungszentrum Karlsruhe – in der Helmholtz-Gemeinschaft, Institut für Hochleistungsimpuls und Mikrowellentechnik, D-76021 Karlsruhe, Germany, Partner of Karlsruhe Institute of Technology; Martin Quandt and Claus-Dieter Munz, Institut für Aerodynamik und Gasdynamik, Universität Stuttgart, D-70550 Stuttgart Germany; Sabine Roller, Höchstleistungsrechenzentrum Stuttgart, D-70550 Stuttgart, Germany; Markus Fertig, Institut für Raumfahrtsysteme, Universität Stuttgart, D-70550 Stuttgart, Germany

2007-037: A3D MODEL FOR MFD FLOW SIMULATION; Francesc Battista, Research Engineer, CIRA Italian Aerospace Research Centre, Capua, 83100, Italy, Ph.D. Student, Dipartimento di Ingegneria Aerospaziale, Universitá di Pisa, Pisa, 56122, Italy; Tommaso Misuri, Ph.D. Student, Dipartimento di Ingegneria Aerospaziale, Universitá di Pisa, Pisa, 56122, Italy; Giuliano Ranuzzi, Ph.D, Research Engineer, CIRA Italian Aerospace Research Centre, Capua, 83100, Italy; Mariano Andrenucci, Professor, Dipartimento di Ingegneria Aerospaziale, Universitá de Pisa, Pisa, 56122, Italy, Chairman and CEO, ALTA SpA, Ospedaletto, Pisa, 56121, Italy

2007-038: REVIEW OF HALL THRUSTER NEUTRAL FLOW DYNAMICS; Bryan M. Reid and Alec D. Gallimore, University of Michigan, Ann Arbor, MI 48105, USA

2007-039: DIVERGING CUSPED-FIELD HALL THRUSTER (DCHT); Daniel G. Courtney and Manuel Martínez-Sáchez, Massachusetts Institute of Technology, Cambridge, Massachusetts, 02139

2007-041: HIGH DENSITY MAGNETIZED TOROID FORMATION AND TRANSLATION WITHIN XOCOT: AN ANNULAR FIELD REVERSED CONFIGURATION PLASMA CONCEPT; David Kirtley and Dr. Alec D. Gallimore, University of Michigan, Ann Arbor, MI 48109; Dr. James Haas and Michael Reilly, Air Force Research Laboratory, Edwards AFB, CA 93524

2007-042: A HIGH ORDER RELATIVISTIC PARTICLE PUSH METHOD FOR PIC SIMULATIONS; Martin Quandt and Claus-Dieter Munz, Institut Für Hochleistungsimpuls und Mikrowellentechnik, Forschungszentrum Karlsruhe, Germany; Rudolf Schneider, Institut Für Hochleistungsimpuls und Mikrowellentechnik, Forshungszentrum Karlsruhe, Germany

2007-043: FEASIBILITY STUDY ON VISUALIZED ION THRUSTER; Yoshinori Nakayama and Yasuhiro Teraura, National Defense Academy of Japan, Yokosuka, Kanagawa, 239-8686, Japan

2007-044: MATHEMATICAL MODEL AND CALCULATION METHOD FOR HOLLOW CATHODES LIFETIME FORECAST; Sergey Yu. Nesterenko and Anatoliy I. Oranskiy

2007-045: EXPERIMENTAL STUDY OF HETEROGENEITY IN AN AZIMUTHAL DIRECTION OF HALL THRUSTER PLASMA FLOW; Oghienko (Ogiienko) Sergii, Bilokon Volodymyr, and Setrakova Yana, Zhukovsky National Aerospace University “Kharkov Aviation Institute,” Ukraine

2007-046: DISTRIBUTION OF UNIONIZED PROPELLANT XENON IN A HALL THRUSTER PLUME; Makoto Matsui, Shigeru Yokota, Daichi Sakoh, Kimiya Komurasaki, and Yoshihiro Arakawa, The University of Tokyo, Tokyo, 113-8656, Japan

2007-048: SEP-SAMPLE RETURN FROM A MAIN BELT ASTEROID; Horst W. Loeb and Karl-Heinz Schartner, Heinrich-Buff-Ring 16, Giessen, D-35394, Germany; Bernd Bachwald, Weßling-Oberpfaffenhofen, D-82234, Germany; Wolfgang Seboldt, Linder Höhe, Porz-Wahnheide, D-51147, Germany

2007-049: THE PLASMA PLUME OF THE ISS PLASMA CONTACTOR UNIT UNDER THE EFFECT OF THE GEOMAGNETIF FIELD; F. F. Gabdullin, A. G. Korsun, E. G. Lavrenko, A. S. Mitroshin, and E. M. Tverdokhlebova, Central Research Institute of Machine Building (TSNIIMASH), Korolev, Moscow region, 141070, Russia

2007-050: THE DESIGN AND OPERATION OF BEAM DIAGNOSTICS FOR THE DUAL STAGE 4-GRID ION THRUSTER; Cristina Bramanti, ESA-ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands; David G. Fearn, EP Solutions, 23 Bownhurst Road, Church Crookham, Fleet, Hants, GU52 6HS, United Kingdom

2007-051: EFFECT OF A MAGNETIC FIELD IN SIMULATING THE PLUME-FIELD OF AN ANODE LAYER HALL THRUSTER; Yongjun Choi, University of Michigan, Ann Arbor, MI 48109; Michhael Keidar, The George Washington University, Washington DC 20052; Iain D. Boyd, University of Michigan, Ann Arbor, MI 48109

2007-052: ELECTRON KINETIC EFFECTS AND BEAM-RELATED INSTABILITIES IN HALL THRUSTERS; I. D. Kaganovich and Y. Raitses, Plasma Physics Laboratory, Princeton University, Princeton, NJ, 08543, USA; D. Sydorenko, Department of Physics, University of Alberta, Edmonton, Alberta T6G 2G7, Canada

2007-053: ADVANCES IN RADIATION-TOLERANT SOLAR ARRAYS FOR SEP MISSIONS; Henry W. Brandhorst, Jr., Steve R. Best, and Julie A. Rodiek, Space Research Institute, Auburn University, AL, 36849, U.S.A.; Mark J. O’Neill, ENTECH, Inc., Keller, TX, 76248, U.S.A.; Michael I. Eskenazi, ATK-Space, Inc., Goleta, CA, 93117, U.S.A.; Dale C. Ferguson, NASA Marshall Space Flight Center, Huntsville, AL, 35812, U.S.A

2007-055: MICRO-PLASMAJET ARRAY: NUMERICAL SIMULATION ON THRUST IMPROVEMENT OF MULTI-JET EFFECT; Fujimi Sawada, Hideyuki Horisawa, Kosuke Onodera, and Atushi Koshiyama, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2007-056: THRUST PERFORMANCE OF ELECTROMAGNETIC ACCELERATION MODE FOR LASER-ELECTRIC HYBRID THRUSTERS; Yusuke Sasaki and Hideyuki Horisawa, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Ikkou Funaki, Japan Aerospace Exploration Agency, 3-1-1 Sagamihara, Kanagawa, 229-8510, Japan; Itsuro Kimura, University of Tokyo, Bunkyo-ku, Tokyo, 113-8856, Japan

2007-057: ON SUPERSONIC HYDROGEN HEATING: THE TIHTUS ENGINE; Hannah Böhrk and Monika Auweter-Kurtz, Institut für Raumfahrtsysteme, Universität Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Germany

2007-058: RECTANGULAR LASER-ELECTROMAGNETIC HYBRID PULSED PLASMA THRUSTER; Tomohiro Ayabe and Hideyuki Horisawa, Tokai University, Hiratsuka-shhi, Kanagawa, 259-1292, Japan; Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan; Itsuro Kimura, University of Tokyo, Bunkyo-ku, Tokyo, 113-8856, Japan

2007-060: PLASMA PROPULSION SYSTEM FUNCTIONAL CHAIN FIRST THREE YEARS IN ORBIT ON EUROSTAR 3000; Astrium Satellites, 31 rue des Cosmonautes, 31402 Toulouse Cedex 4, France; Dr. Howard L. Gray, Astrium Satellites, Anchorage Road, Portsmouth, Hampshire PO3 5PU, United Kingdom

2007-061: LABORATORY EXPERIMENT OF MAGNETOPLASMA SAIL, PART 1: PURE MAGNETIC SAIL; K. Ueno, t. Kimura, and T. Ayabe, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; I. Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan; H. Horisawa, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; and H. Yamakawa, Kyoto University, Uji, Kyoto, 611-0011, Japan

2007-062: RUSSIAN FLIGHT HALL THRUSTERS SPT-70 & SPT-100 AFTER CATHODE CHANGE START DURING 20-25 MS; Vjacheslav M. Murashko, Aleksandr I. Koryakin, Aleksandr N. Nesterenko, and Sergey V. Olotin, Fakel Experimental Design Bureau, Kaliningrad, Russia; Anatoliy I. Oranskiy, Andriy V. Loyan, Mikola M. Koshelev, Volodimir I. Bilokon, and Sergiy Yu. Nesterenko, Science & Technology Center of Space Power & Engines of National Aerospace University “Kharkiv Aviation Institute” (STC SPE KhAI), Kharkiv, Ukraine

2007-066: ADVANCES ON A HALL THRUSTER HYBRID CODE; I. Maqueda, D. Escobar, and E. Ahedo, Universidad Politécnica de Madrid, Madrid 28040, Spain

2007-067: SIMULATION OF WALL EROSION IN HALL THRUSTERS; E. Ahedo and A. Antón, Universidad Politécnica de Madrid, Madrid 28040, Spain; I. Garmendia and I. Caro, Inasmet-Tecnalia, Mikeletegi 2, San Sebastián 20009, Spain; J. González del Amo, ESA/ESTEC, Keplerlaan, 1, Noordwijk, The Netherlands

2007-069: NON-INVASIVE PLASMA DIAGNOSTIC INSIDE A HALL THRUSTER DISCHARGE; Rostislav Spektor and Edward J. Beiting, The Aerospace Corporation

2007-070: QUASI-LINEAR ANALYSIS OF ANOMALOUS ELECTRON MOBILITY INSIDE A HALL THRUSTER; Rostislav Spektor, The Aerospace Corporation

2007-071: OPERATING CHARACTERISTICS OF CYLINDRICAL AND ANNULAR HELICON SOURCES; Brian E. Beal, Air Force Research Laboratory, Edwards AFB, CA 93524; Fabian Mak, Georgia Institute of Technology, Atlanta, GA 30332

2007-072: SIMPLE PERFORMANCE MODELING OF A RADIO-FREQUENCY ION THRUSTER; Michael M. Tsay and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, MA, 02139, U.S.A.

2007-073: EXPERIMENTAL AND NUMERICAL EXAMINATION OF A HALL THRUSTER PLUME; Michael R. Nakles, Lubos Brieda, and Garrett D. Reed, ERC, Inc., Edwards Air Force Base, CA 93524; William A. Hargus, Jr., Air Force Research Laboratory, Edwards Air Force Base, CA 93524; Randy L. Spicer, Virginia Tech, Blacksburg, VA 24061

2007-074: TOTAL AND DIFFERENTIAL SPUTTER YIELDS OF BORON NITRIDE MEASURED BY QUARTZ CRYSTAL MICROBALANCE AND WEIGHT LOSS; Binyamin Rubin, James L. Topper, and Azer P. Yalin, Colorado State University, Fort Collins, Colorado, 80523

2007-075: BORON NITRIDE SPUTTER EROSION MEASUREMENTS BY CAVITY RING-DOWN SPECTROSCOPY; Azer P. Yalin, Lei Tao, and Naoji Yamamoto, Colorado State University, Fort Collins, Colorado, 80523, USA; Timothy B. Smith and Alec D. Gallimore, University of Michigan, Ann Arbor, Michigan, 48109, USA

2007-077: ELECTRIC PROPULSION PLUME INTERACTIONS WITH FORMATION FLYING SPACECRAFT; Raed Kafafy, International Islamic University Malaysia, Kuala Lumpur, 50728, Malaysia; Cao Young, Harbin Institute of Technology, Shenzhen, Public Republic of China; Joseph Wang, Virginia Polytechnic Institute and State University, Blacksburg, VA 24061, USA

2007-078: EFFECT OF CATHODE POSITION ON HALL-EFFECT THRUSTER PERFORMANCE AND CATHODE COUPLING VOLTAGE; Jason D. Sommerville and Lyon B. King, Michigan Technological University, Houghton, Michigan 49931, USA

2007-079: LOW FREQUENCY INSTABILITY AND ENHANCED TRANSFER OF ELECTRONS IN NEAR-ANODE REGION OF HALL THRUSTER; A. Kapulkin and M. Guelman, Asher Space Research Institute, Technion, I. I. T., Haifa, 32000, Israel

2007-080: NANOPARTICLE FIELD EXTRACTION THRUSTER (NANOFET): DESIGN AND RESULTS OF THE MICROPARTICLE EMITTER PROTOTYPE; Louis Musinski, Thomas Liu, Brian Gilchrist, Alec Gallimore, and Michael Keidar, University of Michigan, Ann Arbor, MI 48109

2007-081: PRELIMINARY THRUST CHARACTERIZATION OF THE T-SERIES HOLLOW CATHODES FOR ALL-ELECTRIC SPACECRAFT; Angelo N. Grubisic and Stephen B. Gabriel, Astronautics Research Group, University of Southampton, Southampton, SO17 1BJ, United Kingdom; David G. Fearn, Electric Propulsion Solutions, Fleet, Hants, GU14 0LX, United Kingdom

2007-082: CHARACTERIZING SPECIES COMPOSITION IN RADIO-FREQUENCY PLASMA PRODUCED FROM WATER VAPOR; Sonca Nguyen, Kristina Lemmer, John Foster, and Alec Gallimore, University of Michigan, Ann Arbor, Michigan, 48109, USA

2007-083: THE DAWN ION PROPULSION SYSTEM – GETTING TO LAUNCH; John r. Brophy, M. Andy Etters, Jason Gates, Charles e. Garner, Marlin Klatte, C. John Lo, Michael G. Marcucci, Steve Mikes, Masashi Mizukami, Barry Nakazono, and Greg Pixler, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109, USA

2007-084: IN ORBIT OPERATION OF 20MN CLASS XENON ION ENGINE FOR ETS-VIII; Toshiyuki Ozaki, Yukikazu Kasai, and Takafumi Nakagawa, Mitsubishi Electric Corporation, Kamakura, Kanagawa, 247-8520, Japan; Takashi Itoh, Kenichi Kajiwara, and Masafumi Ikeda, Japan Aerospace Exploration Agency, Tsukuba, Ibaraki, 305-8505, Japan

2007-085: DEVELOPMENT AND THRUST PERFORMANCE OF A MIRCOWAVE DISCHARGE HALL THRUSTER; Hirohisa Kuwano, Kyushu University, 6-1, Kasuga-Kouen, Kasuga 816-8580, Japan; Akira Ohno, The University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan; Hitoshi Kuninaka, Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA), 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan; Hideki Nakashima, Kyushu University, 6-1, Kasuga-Kouen, Kasuga 816-8580, Japan

2007-086: TWO-DIMENSIONAL PARTICLE-IN-CELL SIMULATION OF A CYLINDRICAL HALL THRUSTER; Hae June Lee, Pusan National University, Busan, 609-735, South Korea; Jongho Seon, Satrec initiative, Daejeon, 305-81, South Korea; Wonho Choe, Jungsub Lee, and Youbong Lim, Advanced Institute of Science and Technology, Daejeon 305-701, South Korea

2007-087: NUMERICAL STURDY OF ELECTRODE GEOMETRY EFFECTS ON FLOWFIELD IN TWO-DIMENSIONAL MPD THRUSTERS; K. Kubota, Tokyo Institute of Technology, Yokohama, Kanagawa, 226-8502, Japan; I. Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan; Y. Okuno, Tokyo Institute of Techology, Yokohama, Kanagawa, 226-8502, Japan

2007-088: REALIZATION OF LOW FREQUENCY OSCILLATION FREE OPERATION IN A HALL THRUSTER; Taichiro Tamida and Ikuro Suga, Advanced Technology R&D Center, Mitsubishi Electric Corporation, 8-1-1 Tukaguchi-honmachi, Amagasaki, Hyogo, 661-8661, Japan; Takafumi Nakagawa, Hiroyuki Osuga, and Toshiyuki Ozaki, Space System Department, Kamakura Works, Mitsubishi Electric Corporation, 325 Kamimachiya, Kamakura, Kanagawa, 247-8520, Japan; Katsuaki Matsui, Institute for Unmanned Space Experiment Free Flyer 2-12, Kanda-Ogawamachi, Chiyoda-Ku, Tokyo, 101-0052, Japan

2007-089: HOLLOW CATHODE LIFE TEST FOR THE NEXT-GENERATION ION ENGINE IN JAXA; Yasushi Ohkawa, Yukio Hayakawa, Hideki Yoshida, Katsuhiro Miyazaki, Hiroshi Nagano, and Shoji Kitamura, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan

2007-090: MEASUREMENTS OF HOLE SHAPE ON CARBON-CARBON COMPOSITE GRID AFTER 20,000-HOUR ENDURANCE TEST; Miyuki Usui, University of Tokyo, Hongo, Tokyo, 113-8656, Japan; Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2007-091: MONTE CARLO SIMULATION OF GAS FLOWS IN SPT-ATON; Yan Guojun, Liu Hui, Wang Chunsheng, and Yu Daren, Harbin Institute of Technology Plasma Propulsion Laboratory, Harbin, 150001

2007-092: INVESTIGATION OF INTERNAL PLASMA STRUCTURE IN AN ANODE-LAYER HALL THRUSTER; Nanako Takahashi, Naoji Yamamoto, and Hideki Nakashima, Department of Advanced Energy Engineering Science, Kyushu University, 6-1 Kasuga-kouen, Kasuga, Fukuoka 816-8580, Japan; Shigeru Yokota, Kimiya Komurasaki, and Yoshihiro Arakawa, Department of Aeronautics and Astronautics, The University of Tokyo, Hongo 7-3-1, Bunkyo-ku, Tokyo, 113-8656, Japan

2007-093: DEVELOPMENT STATUS OF POWER PROCESSING UNIT FOR 250MN-CLASS HALL THRUSTER; Hiroyuki Osuga, Kentaro Suzuki, Toshiyuki Ozaki, and Takafumi Nakagawa, Space System Department, Kamakura Works, Mitsubishi Electric Corporation, 325 Kamimachiya, Kamakura, Kanagawa, 247-8520, Japan; Ikuro Suga and Taichiro Tamida, Advanced Technology R&D Center, Mitsubishi Electric  Corporation, 8-1-1 Tukaguchi-honmachi, Amagasaki, Hyogo, 661-8661, Japan; Yoshiyuki Akuzawa, Fumitoshi Soga, and Hirokazu Suzuki, Department, Kamakura Engineering Office, Mitsubishi Electric Engineering Comp, 730 Kamimachiya, Kamakura, Kanagawa, 247-0065, Japan; Katsuaki Matui, Institute for Unmanned Space Experiment Free Flyer, 2-12 Kanda-Ogawamachi, Chiyoda-Ku, Tokyo, 101-0052, Japan

2007-094: LABORATORY EXPERIMENT OF MAGNETOPLASMA SAIL, PART 2: MAGNETIC FIELD INFLATION; I. Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan; T. Kimura, K. Ueno, T. Ayabe, and H. Horisawa, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; H. Yamakawa, Kyoto University, Uji, Kyoto, 611-0011, Japan; Y. Kajimura and H. Nakashima, Kyushu University, Kasuga, Fukuoka, 816-8580, Japan

2007-095: NUMERICAL ANALYSIS OF ANODE SHEATH STRUCTURE TRANSITION IN AN ANODE-LAYER TYPE HALL THRUSTER; Shigeru Yokota, Kimiya Komurasaki, and Yoshihiro Arakawa, The University of Tokyo, Tokyo, 113-8656, Japan

2007-096: FORWARD LASER PLASMA ACCELERATOR FOR RELATIVISTIC PLASMA PROPULSION; Sota Sumida, Masakuni Takagi, and Hideyuki Horisawa, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan; Itsuro Kimura, University of Tokyo, Bunkyo-ku, Tokyo, 113-8856, Japan

2007-097: CHEMICALLY-AUGMENTED PULSED LASER-RAMJET; Tomoki Kaneko, Hideyuki Horisawa, and Kazunobu Tamadao, Department of Aeronautics and Astronautics, Tokai University, 1117 Kitakaname, Hiratsuka, Kanagawa, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo Bunkyo-ku, Tokyo, Japan 113-8856

2007-098: DEVELOPMENT OF A TWO-AXIS DUAL PENDULUM THRUST STAND FOR THRUST VECTOR MEASUREMENT OF HALL THRUSTERS; Naoki Nagao, Shigeru Yokota, Kimiya Komurasaki, and Yoshihiro Arakawa, The University of Tokyo, Tokyo, 113-8656

2007-099: DESIGN AND FABRICATION OF AN INTEGRATED MEMS-BASED COLLOID MICROPROPULSION SYSTEM; R. Krpoun, M. Räber, and H. R. Shea, Ecole Polytechnique Fédérale de Lausanne, CH-1015 Lausanne, Switzerland; K. L. Smith and J. P. W. Stark, Queen Mary University of London, London, E1 4NS, United Kingdom

2007-100: PERFORMANCE INVESTIGATION OF SPT-20M LOW POWER HALL EFFECT THRUSTER; A. V. Loyan and T. A. Maksymenko, National Aerospace University, “KhAI”, 61070 Kharkiv, Ukraine

2007-101: INTERNAL PLASMA STRUCTURE MEASUREMENT IN A MINIATURE MICROWAVE DISCHARGE ION THRUSTER; Shinya Kondo, Takayuki Chikaoka, Teppei Tsuru, Naoji Yamamoto, and Hideki Nakashima, Department of Advanced Energy Engineering Science, Kyushu University, 6-1 Kasuga-koen, kasuga, Fukuoka 816-8580, Japan; Amane Majima, Takao Yamada, Kentaro Tomita, and Kiichiro Uchino, Department of Applied Science for Electronics and Materials, Kyushu University, 6-1 Kasuga-koen, Fukuoka 816-8580, Japan

2007-102: MULTI-MODE THRUSTER WITH ANODE LAYER DEVELOPMENT STATUS; Alexander E. Solodukhin, Alexander V. Semenkin, Leonid E. Zakharenkov, Anatoly V. Rusakov, and Alexander G. Karabadzhak, Central Research Institute of Machine Building (TsNIIMASH), Pionerskaya 4, Korolev, Moscow region, Russia 141070; Alexander N. Nesterenko, Experimental Design Bureau “FAKEL”, 181 Moskovsky prospect, Kaliningrad 236001 Russia

2007-103: INVESTIGATION OF HOLLOW CATHODE FOR LOW POWER HALL EFFECT THRUSTER; N. N. Koshelev and A. V. Loyan, National Aerospace University, “KhAI”, 61070 Kharkiv, Ukraine

2007-104: PIC SIMULATIONS ON CHARGE MITIGATION BY PLASMA RELEASE; Hideyuki Usui and Koujirou Imasato, Research Institute for Sustainalbe Humanosphere, Kyoto University, Uji, Kyoto 611-0011, Japan

2007-105: VISUALIZATION OF THE CHARGED PARTICLES MOVEMENT FEATURES IN CONDITIONS, WHICH ARE CHARACTERISTIC FOR THE HALL THRUSTER DISCHARGE INTERVAL AS THE TECHNIQUE FOR THE STUDENTS TRAINING IN SPACE ELECTRIC PROPULSION; Oghienko (Ogiienko) Sergii, Setrakova Yana, Vakulenko Tamara, and Kulish Olga, Zhukovsky National Aerospace University, “Kharkov Aviation Institute”, Ukraine

2007-106:            1D SIMULATIONS ON THE HELICON DOUBLE LAYER; Marco Manente, CISAS University of Padua, Padova Italy; Johan Carlsson, Tech-X Corporation, Boulder, Colorado, USA; Ivano Musso, CISAS University of Padua, Padova Italy – ISTI-CNR Pisa Italy; Cristina Bramanti, Advanced Concept Team ESA ESTEC Noordwijk – The Netherlands; Cinzia Giacomuzzo and Daniele Pavarin, CISAS University of Padua, Padova Italy

2007-107: NUMERICAL INVESTIGATION OF COUPLED ELECTRODYNAMIC TETHER / ELECTROSTATIC PROPULSION SYSTEMS; Torsten Stindl and Markus Fertig, Institut für Raumfahrtsysteme, Universität Stuttgart, 70550 Stuttgart, Germany; Monika Auweter-Kurtz, Universität Hamburg, 20146 Hamburg, Germany

2007-108: PHYSICS AND EVOLUTION OF HEMP-THRUSTERS; Günter Kornfeld, Norbert Koch, and Hans-Peter Harmann, Thales Electron Devices GmbH, Söflingerstr. 100, 89077 Ulm, Germany

2007-109: DEVELOPMENT AND FLIGHT TESTS OF THE FIRST ELECTRIC PROPULSION SYSTEM IN SPACE; V. A. Khrabrov, Russian Scientific Center “Kurchatov Institute”, Moscow, 123098, Russia

2007-110: STATUS OF THE THALES HIGH EFFICIENCY MULTI STAGE PLASMA THRUSTER DEVELOPMENT FOR HEMP-T 3050 AND HEMP-T 30250; N. Koch, H. –P. Harmann and G. Kornfeld, THALES Electron Devices GmbH, D-89077 Ulm, Germany

2007-111: EUROPEAN STUDENT MOON ORBITER SOLAR ELECTRIC PROPULSION SUBSYSTEM ARCHITECTURE – AN ALL – ELECTRIC SPACECRAFT; M. Coletti and A. Grubisic, University of Southampton, Southampton, SO17 1BJ, United Kingdom; N. Wallace, QinetiQ, Farnborough, GU14 0LX, United Kingdom; N. Wells, QinetiQ, Farnborough, GU14 0LX, United Kingdom

2007-112: SCALING OF A COLLOID THRUSTER SYSTEM FOR MICRONEWTON TO MILLINEWTON THRUST LEVELS; Katharine L. Smith, Matthew S. Alexander, Mark D. Paine, and John P. W. Stark, School of Engineering and Materials  Science, Queen Mary University of London, London, E1 4NS, UK

2007-113: NUMERICAL SIMULATION OF THE INSERT CHEMISTRY OF THE HOLLOW CATHODE FROM THE DEEP SPACE 1 ION ENGINE 30,000 HRS LIFE TEST; M. Coletti and A. Grubisic, University of Southampton, Southampton, SO17 1BJ, United Kingdom; S. B. Gabriel, University of Southampton, Southampton, SO17 1BJ, United Kingdom

2007-114: LOW COMPLEXITY AND LOW COST ELECTRIC PROPULSION SYSTEM FOR TELECON SATELLITES BASED ON HEMP THRUSTER ASSEMBLY; Hans-Peter Harmann, Norbert Koch, and Guenter Kornfeld, Thales Electron Devices, 89077 Ulm, Germany

2007-115: AN EXPERIMENTAL STUDY OF THE ELECTRODE FALL VOLTAGE IN A MPD THRUSTER; Daisuke Nakata, University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan; Kyoichiro Toki, Tokyo University of Agriculture and Technology, 2-24-16, Nakacho, Koganei-shi, Tokyo 184-8588, Japan; Yukio Shimizu, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara-shi, Kanagawa 229-8510, Japan; Ikkoh Funaki, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara-shi, Kanagawa 229-8510, Japan; Hitoshi Kuninaka, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara-shi, Kanagawa 229-8510, Japan; Yoshihiro Arakawa, University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

2007-116: PULSED PLASMA THRUSTER USING POWDERED PROPELLANT; Takefumi Saito, University of Tokyo, Bunkyo, Tokyo, 113-8656, Japan; Hiroyuki Koizumi and Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Institute of Space and Aeronautical Science, Sagamihara, Kanagawa, 229-8510, Japan

2007-117: STATUS OF THE THALES TUNGSTEN/OSMIUM MIXED-METAL HOLLOW CATHODE NEUTRALIZER DEVELOPMENT; N. Koch, H. –P. Harmann, and G. Kornfeld, THALES Electron Devices GmbH, D-89073 Ulm, Germany

2007-118: THRUST MEASUREMENTS WITH THE ONERA MICRONEWTON BALANCE; Denis Packan, Jean Bonnet, and Simone Rocca, ONERA, Chemin de la Huniére, 91120 Palaiseau, France

2007-119: THE ULAN TEST STATION AND ITS DIAGNOSTIC PACKAGE FOR THRUSTER CHARACTERIZATION; Hans-Peter Harmann, Norbert Koch and Guenter Kornfeld, Thales Electron Devices, 89077 Ulm, Germany

2007-120: ELECTROSTATIC INFLUENCE ON CHARGE TO MASS SPECTRUM IN MIXED ION/DROPLET MODE: IMPLICATIONS FOR COLLOID THRUSTER DESIGN; Sobash Jhuree, Matthew S. Alexander, and John PW Stark, School of Engineering & Materials Science, Queen Mary, University of London, UK

2007-121: MODEL ANALYSIS OF A DOUBLE STAGE HALL EFFECT THRUSTER WITH DOUBLE-PEAKED MAGNETIC FIELD AND INTERMEDIATE ELECTRODE; J. Pérez-Luna, G.J.M. Hagelaar, L. Garrigues, and J. P. Boeuf, Laboratoire Plasma et Conversion d’Energie, LAPLACE, CNRS – Université Paul Sabatier, 118 Route de Narbonne, 31062 Toulouse cedex 9, France

2007-122: STATUS OF THE INDIUM FEEP MICROPROPULSION SUBSYSTEM DEVELOPMENT FOR LISA PATHFINDER; C. Scharlemann, A. Genovese, N. Buldrini, R. Schnitzer, and M. Tajmar, Austrian Research Centers GmbH-ARC, 2444 Seibersdorf, Austria; H. Früholz, Astrium Friedrichshafen GmbH, D-88039 Friedrichshafen, Germany; R. Killinger, Astrium Space Transportation, D-74239 Lampoldshausen, Germany

2007-123: FIELD EMISSION PERFORMANCE OF MACROSCOPICALLY GATED MULTIWALLED CARBON NANOTUBES FOR A SPACECRAFT NEUTRALIZER; Karen L. Aplin and Barry J. Kent, Rutherford Appleton Laboratory, Didcot, Oxfordshire, OX11 0QX, UK; Chris Castelli, Science and Technology Facilities Council, Swindon, Wiltshire, SN2 1SZ, UK; Wenhui Song, Brunel University, Uxbridge, Middlesex, UB8 3PH, UK

2007-124: INFLUENCE OF AZIMUTHAL INSTABILITES ON ELECTRON MOTION IN A HALL EFFECT THRUSTER; J. Pérez-Luna, G.J.M. Hagelaar, L. Garrigues, N. Duduit and J. P. Boeuf, Laboratorie Plasma et Conversion d’Energie, LAPLACE, CNRS – Université Paul Sabatier, 118 Route de Narbonne, 31062 Toulouse cedex 9, France

2007-125: MICRO PULSED PLASMA THRUSTER DEVELOPMENT; S. J. Pottinger and C. A. Scharlemann, Austrian Research Centers GmbH – ARC, A-2444 Seibersdorf, Ausria

2007-126: LOW BANK ENERGY APPT FOR MICRO SATELLITES; Nikolay N. Antropov and Garry A. Popov, Research Institute of Applied Mechanics and Electrodynamics, 4, Voloklamskoye shosse, Moscow, 125810, Russia; Michael N. Kazeev, Russian Research Center Kurchatov Institute, 1, Kurchatov sq., Moscow, 123182, Russia; Enrico Chesta, Centre National D’Etudes Spatiales (CNES), 18, Avenue Edouard Belin, 31401 Toulouse Cedex, France; Vladimir P. Khodnenko, All-Russian Research Institute of Electromechanics, 101000, P.O. Box 496, Moscow, Russia

2007-127: THERMAL STATE INVESTIGATIONS OF TWO-STAGE THRUSTER WITH ANODE LAYER; A. S. Mitroshin, V. I. Garkusha, A. V. Semenkin, and A. E. Solodukhin, Central Research Institute of Machine Building (TsNIIMASH), Pionerskaya 4, Korolev, Moscow region, Russia 141070

2007-128: DEVELOPMENT AND STUDY OF THE VERY HIGH SPECIFIC IMPULSE BISMUTH TAL; L. Zakharenkov and A. Semenkin, Central Research Institute of Machine Building (TSNIIMASH), Korolev, Moscow region, Pionerkaya 4, 141070, Russia; S. Tverdokhlebov, JSC “TSNIIMASH-EXPORT”, Russia; A. Sengupta and C. Marrese-Reading, Jet Propulsion Laboratory (JPL), USA

2007-129: DEVELOPMENT OF LOW-POWER HALL THRUSTER WITH LIFETIME UP TO 3000 HOURS; Mikhail B. Belikov, Oleg A. Gorshkov, Evgeny N. Dyshlyuk, Aleksandr S. Lovtzov, and Adrey A. Shagayda, Keldysh Research Center, Moscow, 125438, Russia

2007-130: DEVELOPMENT OF VERNIER PROPULSION SYSTEM FOR MICRO SATELLITE ON THE BASIS OF ABLATIVE PULSED PLASMA THRUSTER; A. V. Bogatiy, Engineer, RIAME; G. A. Diakonov, Senior Researcher, RIAME

2007-131: PROBE MEASUREMENTS IN THE CHANNEL OF 1.5KW HALL THRUSTER WITH DISCHARGE VOLTAGE UP TO 1000 V; M. B. Belikov, O. A. Gorshkov, A. S. Lovtsov, and A. A. Shagayda, Keldysh Research Center, 8 Onezhskaya street, Moscow, 125438, Russia

2007-132: APPT HEAT FLUXES MEASUREMENT AND CALCULATION; Garry A. Popov, Nikolay N. Antropov, Vladimir N. Jakovlev, and Valery K. Tyutin, Research Institute of Applied Mechanics and Electrodynamics, 4, Volokolamskoye shosse, Moscow, 125810, Russia; Michael N. Kazeev and Vladimir F. Kozlov, Russian Research Centre Kurchatov Institute, 1, Kurchatov sq., Moscow, 123182, Russia

2007-133: ANALYSIS OF CERAMIC EROSION CHARACTERISTIC IN HALL-EFFECT THRUSTER WITH HIGHER SPECIFIC IMPULSE; Vladimir V. Abashkin, Oleg A. Gorshkov, Alexander S. Lovtsov, and Andrey A. Shagaida, Keldysh Research Center (KeRC), Moscow, Russia, 125438

2007-134: DEVELOPMENT OF NEXT GENERATION APPT AT RIAME; Garry A. Popov, Director, RIAME; Nikolay N. Antropov, Header Department, RIAME, Research Institute of Applied Mechanics and Electrodynamics (RIAME), Moscow, 125080, Russia

2007-135: SCALING OF THE CURRENT CONDUCTION ZONE IN LITHIUM-FED ARC MULTICHANNEL AND SINGLE-CHANNEL HOLLOW CATHODES; Leonard D. Cassady, Ad Astra Rocket Company, Bay Area Plaza, 141 Bay Area Blvd., Webster, TX 77599, USA; E. Y. Choueiri, Princeton University, Princeton, New Jersey 08544, USA

2007-136: DEVELOPMENT OF HIGH POWER MAGNETOPLASMADYNAMIC THRUSTERS IN THE USSR; O. A. Gorshkov and V. N. Shutov, Keldysh Research Center, Moscow, 125438, Russia; K. N. Kozubsky, EDB “Fakel”, Kaliningrad, Russia; V. G. Ostrovsky, RSC “Energia”, 141070, Russia; V. A. Obukhov, RIAME MAI, Moscow, 125871, Russia

2007-137: SUBSCALE LIFECYCLE TEST OF THERMAL ARCJET THRUSTER TALOS FOR THE LUNAR MISSION BW1; D. Bock, G. Herdich and H. –P. Röser, Institut für Raumfahrtsystem, Pfaffenwaldring 31, 70569 Stuttgart, Germany; M. Auweter-Kurtz, Universität Hamburg, Hamburg, Germany

2007-138: NUMERICAL SIMULATIONS OF MAGNETOPLASMADYNAMIC THRUSTERS WITH COAXIAL APPLIED MAGNETIC FIELD; Daniel Haag and Markus Fertig, Universität Stuttgart, Institut für Raumfahrtsysteme, Pfaffenwaldring 31, 70569 Stuttgart, Germany; Monika Auweter-Kurtz, Universität Hamburg, Edmund-Siemers-Allec 1, 20146 Hamburg, Germany

2007-139: LASER INDUCED ELECTRON BURSTS FOR THE DIAGNOSTIC OF HALL THRUSTER PLASMA; T. Gilbert, A. Leufroy, and A. Bouchoule, Groupe de Recherches sur l’Energétique des Milieux Ionisés, Orléans, 45000, France; A. Lazurenko, Thales Electron Devices GmgH, Ulm, D89077, Germany

2007-140: 3000 HOUR LIFETIME TEST OF AN INDIUM FEEP CLUSTER FOR THE LISA PATHFINDER MISSION; A. Genovese, N. Buldrini, R. Schnitzer, M. Tajmar, and C. Scharlemann, Austrian Research Centers GmbH-ARC, 2444 Seibersdorf, Austria

2007-141: EXPERIMENTAL INVESTIGATIONS OF MAGNETOPLASMADYAMIC THRUSTERS WITH COAXIAL APPLIED MAGNETIC FIELD; Daniel Haag, Markus Fertig, Georg Herdrich, Helmut Kurtz, and Michael Winter, Universität Stuttgart, Institut für Raumfahrtsysteme, Pfaffenwaldring 31, 70569 Stuttgart, Germany; Monika Auweter-Kurtz, Universität Hamburg, Edmund-Siemers-Allee 1, 20146 Hamburg, Germany

2007-142: HISTORY OF THE HALL THRUSTERS DEVELOPMENT IN USSR; V. Kim, Research Institute of Applied Mechanics and Electrodynamics (RIAME), Moscow, 125871, Russia; K. N. Kozubsky and V. M. Murashko, Design bureau Fakel, Kaliningrad, 236001, Russia; A. V. Semenkin, Tsentral Research Institute of Machinebuilding (TsNIIMASH), Korolev, 141070, Russia

2007-143: INVESTIGATION OF ELECTRON TRANSPORT PROPERTIES IN HALL THRUSTERS THROUGH MEASUREMENTS OF MAGNETIC FIELD FLUCTUATIONS; G. Coduti, A. Lazurenko, S. Mazouffre, and M. Dudeck, ICARE Laboratory CNRS, Orleans, Centre, 45071, France; A. Bouchoule, GREMI Laboratory, Orleans University, Centre, 45071, France

2007-144: MASS-SPECTROMETRIC MEASUREMENTS OF A PARTICLE CHARGE STRUCTURE IN THE PLASMA JET OF THE STATIONARY PLASMA THRUSTER; A. N. Veselovzorov, E. E. Barkalov, A. A. Pogorelov, E. B. Svirsky, and V. A. Smirnov, Russian Research Centre ‘Kurchatov Institute’ Moscow, Russia

2007-145: FABRICATION AND CHARACTERIZATION OF POROUS METAL EMITTERS FOR ELECTROSPRAY THRUSTERS; Robert S. Legge Jr., Paulo Lozano, and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, MA, 02139, USA

2007-146: 2D OOPIC SIMULATIONS OF THE HELICON DOUBLE LAYER; I. Musso, Center for Studies and Activities for Space, University of Padua, Padova Italy, Institute of Information Science and Technology, National Research Council of Italy, Pisa, Italy; M. Manente, Center for Studies and Activities for Space, University of Padua, Padova, Italy; J. Carlsson, Tech-X Corporation, Boulder Colorado, USA; C. Bramanti, European Space Research and Technology Center, European Space Agency, Noordwijk, The Netherlands; D. Pavarin, Cener for Studies and Activities for Space, University of Padua, Padova, Italy

2007-147: THE BRAZILIAN ELECTRIC PROPULSION PROGRAM; Gilberto M. Sandonato, José Américo N. Goncalves, Ricardo T. Irita, George F. Fernandes, and Paolo Gessini, Institutio Nacional de Pesquisas Espaciais, Sao José doc Campos, SP, 12227-010, Brazil; Rodrigo I. Marques and Stephen B. Gabriel, University of Southampton, Southampton, United Kingdom, SO17, 1BJ

2007-148: ION BEAM CHARACTERIZATION BY ADVANCED PLASMA DIAGNOSTICS WITH LEVITATED PARTICLES; Holger Kersten and Thomas Trottenberg, Institute of Experimental and Applied Physics, University of Kiel, 24098 Kiel, Germany; Ruben Wiese, INP Greifswald, F. –Hausdorff-Strass 02, 17489 Greifswald, Germany; Frank Scholze, Michael Tartz, and Horst Neumann, IOM Leipzig Permoserstrasse 15, 04318 Leipzig, Germany

2007-149: A PENDULUM TARGET BALANCE FOR ION ENGINE THURST MEASUREMENT; Paolo Gessini, Gilberto Marrega Sandonato, Ricardo Toshiyuki Irita, José Américo Neves Goncalves and George Favale e Fernandes, Instituto Nacional de Pesquisas Espaciais (INPE), Sao José dos Campos, SP, 12227-010, Brazil

2007-150: ELECTRIC PROPULSION DIAGNOSTIC PACKAGE FOR THE FEEP THRUSTER ON LISA PATH FINDER; REVIEW OF STATUS OF ACHIEVEMENTS AT TAS-I; M. Cpacci, G. Matticari, M. Materassi, E. Artina, and V. Vettorello, Thales Alenia Space Italia, Florence Site, 50013 Campi Bisenzio, Italy, Thales Alenia Space Italia, Milano Site, 50013 Vimodrone, Italy

2007-151: INVESTIGATION OF THE SPT OPERATION AND DISCHARGE CHAMBER WALL EROISION RATE UNDER INCREASED DISCHARGE VOLTAGES; V. Kim, V. I. Kozlov, A. I. Skrylnikov, and E. K. Sidorenko, Research Institute of Applied Mechanics and Electrodynamics, Moscow, 125871, Russia; V. M. Murashko and A. N. Nesterenko, Design Bureau Fakel, Russia

2007-152: PROGRESS ON RE-GENERABLE FIELD EMISSION CATHODES FOR LOW-POWER ELECTRIC PROPULSION; Jason M. Makela and Lyon B. King, Michigan Technological University, Houghton, MI, 49931, USA

2007-153: CONFINEMENT TIME IN AN ELCTRON TRAP USED FOR ELECTRON-MOBILITY STUDIES IN HALL THRUSTER-LIKE FIELDS; Emily C. Fossum and Lyon B. King, Michigan Technological University, Houghton, MI, 49931, USA

2007-154: DEVELOPMENT AND QUALIFICATION OF A NEUTRALIZER DEVICE FOR THE FEEP MICRO PROPULSION ON MICROSCOPE AND LISA PATH FINDER; M. Capacci, G. Matticari, M. Materassi, and G. Noci, Thales Alenia Space Italia, Florence Site, 50013 Campi Bisenzio, Italy

2007-155: ADVANCED FLUIDIC COMPONENTS FOR ELECTRIC AND COLD GAS PROPULSION APPLICATIONS: REVIEW OF STATUS OF ACHIEVEMENTS AT TAS-I FLORENCE; G. Noci, G. Matticari, P. Siciliano, and L. Fallerini, Thales Alenia Space Italia, Florence Site, 50013 Campi Bisenzio, Italy

2007-157: TWO DIMENSIONAL HYBRID MODEL OF A MINIATURIZED CYLINDRICAL HALL THRUSTER; L. Garrigues, G.J.M. Hagelaar, and J. P. Boeuf, LAPLACE, CNRS-Université Paul Sabatier, 31062 Toulouse, France; Y. Raitses, A. Smirnov, and N. J. Fisch, Princeton Plasma Physics Laboratory, Princeton University, Princeton, NJ, 08543

2007-158: SOLID STATE MPD THRUSTER WITH APPLIED MAGNETIC FIELD; M. Coletti, University of Southampton, Southampton, SO17 1DR, United Kingdom; A. Balestra and M. Sensini, University of Rome “La Sapienza”, Rome, 00185, Italy; G. Paccani, University of Rome “La Sapienza”, Rome, 00185, Italy

2007-159: SPECTROSCOPIC TEMPERATURE MEASUREMENT IN A APPLIED FIELD MPD; M. Coletti, University of Southampton, Southampton, SO17 1DR, United Kingdom; S. Ciampone, Queen Mary University of London, London, E1 4NS, United Kingdom; G. Paccani, University of Rome “La Sapienza”, Rome, 00185, Italy; G. Mazzitelli, ENEA, Frascati, Rome, 00040, Italy

2007-160: A LASER SPECTROSCOPIC STUDY ON XE+ ION TRANSPORT PHENOMENA IN A 5 KW-CLASS HALL EFFECT THRUSTER; S. Mazouffre, D. Gawron, and W. Kulaev, CARE Institute – CNRS, 1c Av. de la Recherche Scientifique, 45071 Orléans-France; N. Sadeghi, Laboratoire de Spectrométrie Physique, Université Joseph Fourier – CNRS, 140 Av. de la Physique, BP 87, 38402 Saint Martin d’Héres – France

2007-161: REVIEW OF TWO RETARDING POTENTIAL ANALYZERS FOR USE IN HIGH DENSITY HELICON PLASMA; Kristina M. Lemmer, Alec D. Gallimore, Timothy B. Smith, and Daniel R. Austin, University of Michigan, Ann Arbor, MI, 48109, USA

2007-162: RAM ELECTRIC PROPULSION FOR LOW EARTH ORBIT OPERATION: AN ESA STUDY; D. Di Cara, J. Gonzalez del Amo, A. Santovincenzo, B. Carnicero Dominguez, M. Arcioni, A. Caldwell, and I. Roma; ESA/ESTEC, Keplerlaan 1, 2200 AG Noordwijk ZH, The Netherlands

2007-164: PPS 1350-G QUALIFICATION STATUS 10500 H; Frank Darnon, CNES – Centre Spatial de Toulouse, 18 avenue Edouard Belin, 31401 Toulouse Cedex 4, France; Denis Estublier, ESA/ESTEC – Keplerlaan 1, 2200 AG Noordwijk ZH, The Netherlands

2007-165: CURRENT SHEET FORMATION IN A CONICAL THETA PINCH FARADAY ACCELERATOR WITH RADIO-FREQUENCY ASSISTED DISCHARGE; Ashley K. Hallock and Edgar Y. Choueiri, Princeton University, Princeton, NJ, 08540, USA; Kurt A. Polzin, NASA – Marshall Space Flight Center, Huntsville, AL, 35812, USA

2007-166: MEASUREMENT AND MODELING OF THE INSIDE CHANNEL DEPOSITION OF THE SPUTTERED CERAMICS ON HET PPSX000-ML. A TOOL TO PREDICT THE EROSION ALONG THE THRUSTER LIFETIME; D. Pagnon, Laboratoire d’Analyse Spectroscopique et d’Energétique des Plasmas, Université d’Orléans, rue G. Berger, BP 4043 – 18028 Bourges – France; P. Lasgorceix and C. Legentil, Laboratoire d’Aérothermique, 1C Av. de la Recherche Scientifique, 45071 Orléans, France

2007-167: SPECIFIC LABORATORY TESTING EQUIPMENT & METHODOLOGY FOR SPUTTERING TESTS OF ELECTRIC PROPULSION MATERIALS; J. Ustarroz, I. Caro, P. Corengia, I. Garmendia, and J. Macros, INASMET-Tecnalia, San Sebastián, 20009, Spain; E. Ahedo, Universidad Politécnica de Madrid, Madrid 28040, Spain; J. González del Amo, ESA/ESTEC, Keplerlaan, 1, Noordwijk, The Netherlands

2007-168: SIMP-LEX: SYSTEMATIC GEOMETRY VARIATION USING THRUST BALANCE MEASUREMENTS; Anuscheh Nawaz, Georg Herdrich, Helmut Kurtz and Tony Schönherr, Institut für Raumfahrtsysteme, Universität Stuttgart, 70569, Germany; Monika Auweter-Kurtz, Universität Hamburg, Edmund-Siemers-Allee 1, Hamburg, Germany

2007-169: MULTI-PHOTON SPECTROSCOPY ON XENON FOR APPLICATION ON ION THRUSTER PLASMA PARAMETER INVESTIGATIONS: EXPERIMENT AND THEORY; Christoph Eichhorn and Michael Winter, Institut für Raumfahrtsysteme IRS, Universität Stuttgart, Pfaffenwaldring 31, D-70569 Stuttgart, Germany; Monika Auweter-Kurtz, Universität Hamburg, Edmund-Siemers-Allee 1, D-20196 Hamburg, Germany; Stefan Löhle, DLR Institut für Verbrennungstechnik, Pfaffenwaldring 38-40, D-70569 Stuttgart, Germany

2007-170: DISPENSER TEMPERATURE PROFILE MEASUREMENT AND DISCHARGE CURRENT DIVISION IN THE T5 & T6 KAUFMAN-TYPE ION THRUSTERS; Ismat M. Ahmed Rudwan, N. C. Wallace, and Mike Kelly, Space Division, QinetiQ Plc Ltd, Farnborough, Hampshire, GU14 0LX, UK

2007-171: DEVELOPMENT AND TESTING OF A FIELD-EMISSION NEUTRALISER FOR MICRO-ELECTRIC PROPULSION; Pierre-Etienne Frigot, AOES B.V., Haagse Schouwweg 6G, 2332 KG Leiden, The Netherlands; Karen l. Aplin and Barry J. Kent, Rutherford Appleton Laboratory, Oxfordshire OX11 0QX, United Kingdom; Davide Nicolini and José Antonio Gonzalez del Amo, European Space Agency, ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands

2007-172: ION VELOCITY MEASUREMENTS WITHIN THE ACCELERATION CHANNEL OF A LOW POWER HALL THRUSTER; William A. Hargus, Jr., Air Force Research Laboratory, Edwards AFB, CA 93524; Michael R. Nakles, E.R.C., Inc., Edwards AFB, CA 93524

2007-173: STATUS ON PLASMA DIAGNOSTIC MEASUREMENTS ON A RIT-10 ION THRUSTER; Michael W. Winter, Christoph Eichhorn, Monika Auweter-Kurtz, and Thomas Pfrommer, Universität Stuttgart,  Institut für Raumfahrtsysteme (IRS), Pfaffenwaldring 31, 70550 Stuttgart, Germany

2007-174: EFFECTS OF VARIED PROPELLANT COMPOSITIONS ON THE ION ENERGY DISTRIBUTIONS IN HOLLOW CATHODES; JoHanna N. Przybylowski, California Institute of Technology, Pasadena, CA, 91125; James E. Polk, Jet Propulsion Laboratory, Pasadena, CA, 91109; Joseph E. Shepard and Angela M. Capece, California Institute of Technology, Pasadena, CA, 91125

2007-177: PERFORMANCE MEASUREMENTS FROM A CLUSTER OF FOUR HALL THRUSTERS; Robert B. Lobbia and Alec D. Gallimore, The University of Michigan, Ann Arbor, MI, 48109, U.S.A.

2007-178: HIGH-POWER ELECTRIC PROPULSION UTILIZING LASER-DRIVEN PONDEROMOTIVE FIELDS; George J. Williams, Jr., The Ohio Aerospace Institute, 22800 Cedar Point Rd., Brookpark, OH 44142

2007-179: FEASIBLITY OF ELECTROSTATIC MICROPARTICLE THRUSTERS; Thomas Trottenberg and Holger Kersten, IEAP, Christian-Albrechts- Universität zu Kiel, D-24118 Kiel, Germany

2007-181: HIGH POWER VASIMR EXPERIMENTS USING DEUTERIUM, NEON AND ARGON; Jared P. Squire, Franklin R. Chang-Díaz, Mark D. Carter, Leonardl D. Cassady, William J. Chancery, Tim W. Glover, Verlin T. Jacobson, and Greg E. McCaskill, Ad Astra Rocket Company, Houston, Texas, 77058, USA; Roger D. Bengtson, The University of Texas at Austin, Austin, Texas, 78712, USA; Edgar A. Bering, The University of Houston, Houston, Texas, 77004, USA; Christopher A. Deline, The University of Michigan, Ann Arbor, Michigan, 48109, USA

2007-185: SPECTROSCOPIC ELECTRON TEMPERATURE MEASUREMENT OF THE RECOMBINING PLASMA ON THE VASIMR EXPERIMENT; Ella M. Sciamma and Roger D. Bengtson, The University of Texas at Austin, Austin, TX, 78712, U.S.A.; Franklin R. Chang-Diaz, Verlin T. Jacobson, Jared P. Squire, and W. J. Chancery, Ad Astra Rocket Company, Texas 77058, U.S.A.

2007-186: PHYSICAL MODELS AND PERFORMANCE IMPLICATIONS FOR THE NANOPARTICLE FIELD EXTRACTION THRUSTER; Thomas M. Liu and Louis D. Musinski, University of Michigan, Ann Arbor, MI 48109, USA; Michael Keidar, Alec D. Gallimore, and Brian e. Gilchrist, University of Michigan, Ann Arbor, MI 48109, USA

2007-187: THE PLANAR HALL THRUSTER FOR INVESTIGATING ELECTRON MOBILILTY IN EXB DEVICES; Joshua L. Rovey, Matthew P. Giacomi, Robert A. Stubbers, and Brian e. Jurczyk, Starfire Industries LLC, Champaign, IL, 61820

2007-188: ANALYTICAL EXTRACTION OF PLASMA PROPERTIES USING A HALL THRUSTER EFFICIENCY ARCHITECTURE; Daniel L. Brown, C. William Larson, and James M. Haas, Air Force Research Laboratory, Edwards AFB, CA, 93524, USA; Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, MI, 48109, USA

2007-189: PLASMA FLOW BEHAVIORS AND THEIR EFFECTS ON THE PERFORMANCE OF PULSED PLASMA THRUSTERS; Hiroyuki Koizumi, Institute of Space and Astronautical Science / Japan Aerospace Exploration Agency, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan; Ryosuke Noji, Kimiya Komurasaki, and Third Author, University of Tokyo, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

2007-190: NUMERICAL SIMULATION OF INTERNAL PLASMA IN A MINIATURE MICROWAVE DISCHARGE ION THRUSTER; Takayasu Kanagawa, Naoji Yamamoto, Yoshihiro Kajimura, and Hideki Nakashima, Department of Advanced Energy Engineering Science, Graduate School of Engineering Science, Kyushu University, 6-1 Kasuga-koen, Kasuga, Fukuoka 816-8580, Japan; Hirokazu Masui, Department of Electrical Engineering Kyushu Institute of Technology, 1-1 Sensui, Tobata, Kitakyushu, Fukuoka, 804-8550, Japan

2007-191: ION HEATING AND ACCELERATION EXPERIMENT IN HYDROGEN PLASMA FOR THE VASIMR-TYPE THRUSTER; Akira Ando, Yuji Kasashima, Tatsuya Hagiwara, Kunihiko Hattori, and Masaaki Inutake, Department of Electrical Engineering, Graduate School of Engineering, Tohoku University, 6-6-05, Aoba-yama, Sendai, 980-8579, Japan

2007-192: SCALING AND SYSTEMS CONSIDERATIONS IN PULSED INDUCTIVE THRUSTERS; Kurt A. Polzin, NASA-Marshall Space Flight Center, Huntsville, AL 35812

2007-193: XIPS 25-CM THRUSTER CATHODE LIFE QUALIFICATION FOR USE ON DEEP SPACE MISSIONS; James E. Polk and Dan M. Goebel, Jet Propulsion Laboratory, M/S 125-109, 4800 Oak Grove Drive, Pasadena, CA 91109; William Tighe, L-3 ETI, Torrance, CA 90505

2007-195: MHD ANALYSIS ON PROPULSIVE CHARACTERISTICS OF MAGNETO PLASMA SAIL; Hiroyuki Nishida, University of Tokyo, Hongo, Tokyo, 113-8656, Japan; Ikkoh Funaki, Hiroyuki Ogawa, and Yoshifumi Inatani, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2007-196: EFFECTS OF HELICON WAVE PROPAGATION BASED ON A CONICAL ANTENNA DESIGN: PART I; Michael P. Reilly and George H. Miley, University of Illinois @ Urbana-Champaign, Urbana, IL, 61801, United States of America; David E. Kirtley University of Michigan, Ann Arbor, MI, 48109, United States of America; William A. Hargus, Jr., Air Force Research Laboratory, Edwards AFB, CA, 93524, United States of America

2007-197: DEVELOPMENT OF NUMERICAL PLASMA PLUME ANALYSIS MODULE FOR SPACECRAFT ENVIRONMENT SIMULATOR; Takanobu Muranaka, Japan Aerospace Exploration Agency, 3-1-1 Yoshinodai, Sagamihara, Kanagawa, 229-8510, Japan; Hiroko O. Ueda, Japan Aerospace Exploration Agency, 2-1-1 Sengen, Tsukuba, Ibaraki 305-8505, Japan; Shinji Hatta and Jeongho Kim, MUSCAT Space Engineering Co., Ltd, 1-1 Sensui-cho, Tobata-ku, Kitakyushu, Fukuoka 229-8510, Japan; Mengu Cho, Kyushu Institute of Technology, 1-1 Sensui-cho, Tobata-ku, Kitakyushu, Fukuoka 804-8550, Japan; Kiyokazu Koga and Tateo Goka, Japan Aerospace Exploration Agency, 2-1-1 Sengen, Tsukuba, Ibaraki 305-8505, Japan; Hideyuki Usui, Kyoto University, Gokasho, Ujk, Kyoto 611-0011, Japan; Iku Shinohara, Japan Aerospace Exploration Agency, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2007-199: PULSED MAGNETOPLASMADYNAMIC DETONATION PROPULSION; Kyoichi Kuriki, Junichiro Aoyagi, and Haruki T akegahara, Tokyo Metropolitan University, Tokyo, 191-0065, Japan

2007-200: NUMERICAL CALCULATION OF WALL EROSION ON HALL THRUSTERS USING 2D-HYBRID-PIC MODELING; Hiroyuki Koizumi, Institute of Space and Astronautical Science/Japan Aerospace Exploration Agency, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2007-201: MICRO-PLASMAJET ARRAY: MULTI-JET-EFFECT FOR THRUST PERFORMANCE IMPROVEMENT; Atsushi Koshiyama, Fujimi Sawada, and Hideyuki Horisawa, Dept. of Aeronautics and Astronautics, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; Ikkoh Funaki, Japan Aerospace Exploration Agency, 3-1-1 Sagamihara, Kanagawa, 229-8510, Japan

2007-202: CHARACTERIZATION OF AN ANNULAR HELICON PLASMA SOURCE; Douglas Palmer, Cengiz Akinli, Logan Williams, and Mitchell L. R. Walker II, High-Power Electric Propulsion Laboratory, Georgia Institute of Technology, Atlanta, GA, 30332, USA

2007-203: SPECTRAL MEASUREMENTS OF MHTX HELICON DISCHARGE PLASMA; Murat Celik, Oleg Batishchev, and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, MA, 02139, USA

2007-204: NUMERICAL SIMULATION OF THE FREE MOLECULEMICRO-RESISTOJET FLOW; Mao-lin Chen, Mao Gen-wang, Yang Juan, and Xia Guang-qing, Northwestern Polytechnical University, Xi’an, shannxi, 710072, China

2007-205: MICROWAVE DISCHARGE ION THRUSTER USING ARGON AS A PROPELLANT; Makoto Miyoshi, Naoji Yamamoto, and Hideki Nakashima, Department of Advanced Energy Engineering Science, Graduate School of Engineering Sciences, Kyushu University, 6-1 Kasuga-kouen, Kasuga, Fukuoka Prefecture, 816-8580, Japan

2007-206: CNES ELECTRIC PROPULSION ACTIVITIES OVERVIEW: FLIGHT PROGRAMS, R&T ACTIONS, NOVEL MISSION DESIGNS; Enrico Chesta, Denis Arrat, Régis Bertrand, Franck Darnon, Stéphane D’Escrivan, and Nicolas Pillet, Centre National d’Etudes Spatiales (CNES), 18 avenue Edouard Belin, F-31401 Toulouse, France

2007-207: THE “NEW GRID SYSTEMS FOR ION ENGINES” TECHNOLOGY PROJECT – FINAL ASSESSMENT; Hans J. Leiter, Ralf Kukies, Werner Kadrnoschka, and Rainer Killinger, Astrium Space Transportation GmbH, P.O. 1119, 74215 Möckmühl, Germany

2007-209: RIT-µX – THE NEW MODULAR HIGH PRECISION MICRO ION PROPUSLION SYSTEM; Hans Leiter and Rainer Killinger, Astrium GmbH BL Equipment and Propulsion, P.O. 1119, 74215, Möckmühl, Germany, Michael Boss, Michael Braeg, and Matthias Gollor, Astrium Satellites GmbH, 88039 Friedrichshafen, Germany; Michael Tartz and Horst Neumann, IOM Leipzig, Permoserstr. 15, 04318 Leipiz, Germany; Jens Haderspeck and Dagmar Bock, IRS Stuttgart Pfaffenwaldring 31, 70569, Stuttgart, Germany; Davina Maria Di Cara, ESA ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands

2007-210: THRUST CONTROL ALGORITHMS FOR THE GOCE ION PROPULSION ASSEMBLY; M. H. Corbett, QinetiQ Ltd, Cody Technology Park, Farnborough, GU14 0LX, U.K.; C. H. Edwards, ESA-ESTEC, Keplerlaan 1, 2200 AG, Noordwijk ZH, The Netherlands

2007-211: NUMERICAL SIMULATION OF MICROWAVE PLASMA THRUSTER FLOW: Mao-Lin Chen, Mao Gen-wang, Yang Juan, and Xia Guang-qing; Northwestern Polytechnical University, Xi’an, shannxi, 710071, China

2007-212: THE ANALYSIS OF INFLUENCE OF ELECTRIAL PROPULSION CHARACTERISTICS ON EFFICIENCY OF TRANSPORT MANEUVERS; M. Konstantinov, Research Institute of Applied Mechanics and Electrodynamics, Moscow, Russia

2007-213: MICROSCOPE MISSION PHASE B PROPULSION SYSTEM ACTIVITIES AT SPACECRAFT LEVEL: REQUIREMENTS CONSOLIDATION AND ASSESSMENT OF NEUTRALIZATION AND CONTAMINATION EFFECTS; Enrico Chesta, Yves André, Laurent Perraud, Benjamin Pouilloux, Pascal Prieur, Thierry Tirolien, Centre National d’Etudes (CNES), 18 Avenue Edouard Belin, F-31401 Toulouse, France; Jean-Francois Russel, Thomas Tondu, Jean-Charles Mateo Velez, ONERA, 2 Avenue Edouard Belin, F-31055 Toulouse, France

2007-214: SIMULATION OF THE ENERGY DEPOSITION ON DIELECTRIC WALL SURFACES IN HALL THRUSTERS; C. Focsa and M. Ziskind, Laboratoire de Physique des Lasers, Atomes et Molécules (UMR CNRS 8523), Centre d’Etudes et de Recherches Lasers et Applications (FR CNRS 2416), Université de Lille 1, 59655 Villeneuve d’Ascq, France; S. Gurlui, Universitatea “Al. I. Cuza”, Iasi-700506, Romania; D. Pagnon, Laboratoire de Physique des Gaz et des Plasmas, Université de Paris XL, 91405 Orsay, France; S. Pellerin, Laboratoire d’Analyse Spectroscopique et d”Energétique des Plasmas, 18028 Bourges, Université d’Orléans, France; N. Pellerin, Centre de Recherche sur les Matériaux á Hautes Température, 45071 Orléans, France; M. Dudeck, Laboratoire ICARE, CNRS Orléans, 45071 Orléans, France

2007-215: DISCHARGE MODES AND CHARACTERISTICS OF HOLLOW CATHODE; Shunsuke Sakai, Toshiyuki Katayama, Junichiro Aoyagi, and Haruki Takegahara, Tokyo Metropolitan University, Tokyo, 191-0065, Japan

2007-217: PERFORMANCE INVESTIGATION OF SPT-20M LOW POWER HALL EFFECT THRUSTER; A. V. Loyan and T. A. Maksymenko, National Aerospace University “KhAI”, 61070 Kharkiv, Ukraine

2007-218: THE µNRIT-4 ION ENGINE: A FIRST STEP TOWARDS A EUROPEAN MINI-ION ENGINE SYSTEM DEVELOPMENT; D. Feili, D. M. Di Cara, H. J. Leiter, J. G. Del Amo, H. W. Loeb, St. Weis, D. Kirmse, P. E. Frigot, M. Orlandi, H. Müller, and B. K. Meyer, Giessen University, Electric Propulsion Group, Heinrich-Buff-Ring 16, 35390, Giessen, Germany

2007-219: NEUTRAL VELOCITY VECTOR AND ABSOLUTE NUMBER DENSITY LIF OPTICAL MEASUREMENT WITH APPLICATION TO A FLIGHT MODE MICROSCOPE CESIUM FEEP THRUSTER; Denis Packan, Jean Bonnet, Alexandre Bresson, and Brigitte Attal-Tretout, ONERA, Chemin de la Hunire, 91120 Palaiseau, France

2007-220: OPTIMISED THRUST STEERING OF A GRIDDED ION ENGINE; P. Jameson, QinetiQ Ltd, Cody Technology Park, Farnborough, GU14 0LX, U.K.

2007-221: TWO-MODES OPERATION OF SPT OF SECOND GENERATION; A. I. Bugrova, A. V. Desyatskov, V. K. Kharchevnikov, and A. S. Lipatov, Moscow Institute of Radio-engineering, Electronics and Automatics, Moscow, Russia

2007-222: OVERRUN DISCHARGE CURRENT OPERATION OF LOW POWER CYLINDRICAL HALL THRUSTERS; Yevgeny Raitses, Artem Smirnov, Erik Granstedt, and Nathaniel J. Fisch, Princeton Plasma Physics Laboratory, Princeton University, Princeton, NJ, 08543

2007-223: FEASIBILITY STUDY OF PLASMA CHEMICAL THRUSTER; Junichiro Aoyagi, Kyoichi Kuriki, and Haruki Takegahara, Tokyo Metropolitan University, Tokyo, 191-0065, Japan; Jun Yokote, Akira Kakami, and Takeshi Tachibana, Kyushu Institute of Technology, Kitakyushu, 800-0000, Japan

2007-226: PRELIMINARY STUDY ON RADIO FREQUENCY NEUTRALIZER FOR ION ENGINE; Tomoyuki Hatakeyama, Masatoshi Irie, Hiroki Watanabe, Aasami Okutsu, Junichiro Aoyagi, and Haruki Takegahara, Tokyo Metropolitan University, Hino, Tokyo, 191-0065, Japan

2007-227: MULTI-CHANNEL HALL-EFFECT THRUSTERS: MISSION APPLICATIONS AND ARCHITECTURE TRADE-OFFS; Olivier Duchemin, Anthony Lorand, Michael Notarianni, and Dominique Valentian, Snecma, Safran Group, Division Moteurs Spatiaux, 27208 Vernon, France; Enrico Chesta, CNES, Centre Spatial de Toulouse, 31401 Toulouse, France

2007-228: FEASIBILITY STUDY OF AN MPD ARCJET AS A PLASMA INJECTOR FOR MARS’S ATMOSPHERE DYNAMICS RESEARCH; Yukio Shimizu, Institute of Space and Astronautical Science of Japan Aerospace Exploration Agency, Sagamihara 229-8510, Japan; Naoki Terada, National Institute of Information and Communications Technology, Koganei 184-8795, Japan; Hitoshi Kuninaka, Institute of Space and Astronautical Science of Japan Aerospace Exploration Agency, Sagamihara 229-8510, Japan; Daisuke Nakata, Department of Aeronautics and Astronautics, University of Tokyo, Tokyo 113-8656, Japan

2007-229: OPTOGALVANIC AND LASER-INDUCED FLUORESCENCE SPECTROSCOPY OF THE ZEEMAN EFFECT IN XENON, Timothy B. Smith, Wensheng Huang, Bailo B. Ngom, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, MI 48105, USA

2007-230: FUNDAMENTAL STUDY OF LASER MICRO PROPULSION USING POWERED-PROPELLANT; S. Yokoyama and H. Horisawa, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; I Funaki and H. Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2007-231: OPTIMISATION AND ASSESSMENT OF THE TOTAL IMPULSE CAPABILITY OF THE T6 ION THRUSTER; Mr. N. C. Wallace and Dr. Michael Corbett, QinetiQ Ltd., Cody Technology Park, Farnborough, Hampshire, GU14 0LX, UK

2007-232: GEOMETRY AND ELECTRIC POWER EFFECTS ON SPECIFIC IMPULSE AND EFFICIENCY OF AN ARC-JET THRUSTER; A. Kaminska and A. Bialek, IEPE, Poznan University of Technology, Poxnan 60-965, Poland; M. Dudeck, ICARE Laboratory, Orléans 45071 and University of Paris 6, Paris 75252, France

2007-233: A FULLY-INTEGRATED MICROFABRICATED EXTERNALLY-WETTED ELECTROSPRAY THRUSTER; B. Gassend, L. F. Velásquez-García, A. I. Akinwande, and M. Martínez-Sánchez, Massachusetts Institute of Technology, Cambridge, Massachusetts, 02139, USA

2007-234: PLUME DIVERGENCE IN THE HALL THRUSTER DUE TO PLASMA PRESSURE; Avi Cohen-Zur and Amnon Fruchtman, Holon Institute of Technology, Holon, 58102, Israel; Alon Gany, Technioin-Israel Institute of Technology, Haifa, 32000, Israel

2007-236: COMPARTISON OF THE THEORETICAL AND EXPERIMENTAL PERFORMANCE OF AN ANNULAR HELICON PLASMA SOURCE; Cengiz B. Akinli, Douglas D. Palmer, and Mitchell L. R. Walker II, Georgia Institute of Technology, Atlanta, GA, 30332, USA

2007-237: FUNDAMENTALS OF DISCHARGE INITIATION IN PULSED PLASMA THRUSTERS: THRESHOLD CRITERIA FOR UNDERVOLTAGE BREAKDOWN; James E. Cooley and Edgar Y. Choueiri, Princeton University, Princeton, NJ, 08544, USA

2007-238: CAPILLARY DISCHARGE BASED PULSED PLASMA THRUSTERS; Jean-Luc Cambier, Air Force Research Lab, 10. E. Saturn Blvd. Edwards AFB, CA 93524, United States; Marcus Young and Leonid Pekker, ERC Inc., 10. E. Saturn Blvd, Edwards AFB, CA 93524, United States; Anthony Pancotti, University of Southern California, 854 W 36th Place, RRB 101, Los Angeles, CA 90089, United States

2007-239: CURRENT AND PLASMA OSCILLATION INSPECT IN PPS-X000 HET THRUSTER – EMD APPROACH; Jacek Kurzyna, Karol Makowski, and Zbigniew Peradzynski, Institute of Fundamental Technological Research, Polish Academy of Sciences, Swietokrzyska 21, 00049 Warsaw, Poland; Alexey Lazurenko, Stephane Mazouffre, Giovanni Coduti, and Michel Dudeck, ICARE – CNRS, 1C Avenue de la Recherche Scientifique, 45071 Orléans Cedex 2, France

2007-240: DEVELOPMENT OF THE ELECTRODELESS PLASMA THRUSTER AT HIGH POWER: INVESTIGATIONS ON THE MICROWAVE-PLASMA COUPLING; Geogory D. Emsellem, The Elwing Company, Wilmington, DE, 19801, USA; Serge Larigaldie, ONERA – Office National d’Etude et Recherche Aéronautique, Palaiseau, 91120, France

2007-243: RESEARCH AND DEVELOPMENT ON COAXIAL PULSED PLASMA THRUSTER FOR SMALL SATELLITES; Masayuki Mukai, Yukiya Kamishima, Tsubasa Sasaki, Kouhei Shintani, Junichiro Aoyagi, and Haruki Takegahara, Tokyo Metropolitan University, Hino, Tokyo, 191-0065, Japan; Takashi Wakizono, HI-SERVE Corporation, Akiruno, Tokyo, 190-0252, Japan; Mitsuteru Sugiki, Astro Research Corporation, Yokohama, Kanagawa, 190-0152, Japan

2007-244: PROJECTED LUNAR CARGO CAPABILITIES OF HIGH-POWER VASIMR PROPULSION; Tim W. Glover, Franklin R. Chang Diaz, and Andrew V. Ilin, Ad Astra Rocket Company, Houston, Texas, 77058, USA; Robert Vondra, P.O. Box 596, Wrightwood, California 92397, USA

2007-245: LASER-AUGMENTED MICRO-PULSEJET THRUSTER; Sou Eto and Hideyuki Horisawa, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo, Bunkyo-ku, Tokyo, 113-8856, Japan

2007-246: NEW WALL CONDUCTIVITY IN HALL THRUSTERS. CYLINDRICAL GEOMETRY EFFECT; K. Makowski, Institute of Fundamental Technological Research, Polish Academy of Sciences, Warsaw 00-49, Poland; Z. Peradzynski, Faculty of Mathematics, Informatics and Mechanics, Warsaw University, Warsaw 02-097, Poland; M. Kolanowski, S. Barral, J. Kurzyna, Institute of Fundamental Technological Research, Polish Academy of Sciences, Warsaw 00-049, Poland; M. Dudeck, Laboratoire d’Aérothermique du CNRS, Orleans 45071, France

2007-247: CHARACTERIZATION OF HIGH FREQUENCY PLASMA OSCILLATIONS IN A HALL EFFECT THRUSTER; Gérard Bonhomme, Nicolas Lemoine, and Frédéric Brochard, LPMIA, UMR 7040 CNRS-Université Henri Poincaré, BP 239, F-54506 Vandoeuvre-lés-Nancy, France; Alexey Lazurenko, Stéphane Mazouffre, and Michel Dudeck, ICARE, CNRS, 1c Av. de la Recherche Scientifique, 45071 Orléans, France

2007-250: MODELING OF HALL THRUSTER LIFETIME AND EROSION MECHANISMS; Shannon Y. Cheng and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, MA, 02139, USA

2007-252: NEAR-FIELD LASER-INDUCED FLUORESCENCE VELOCIMETRY OF NEUTRAL XENON IN A 6-KW HALL THRUSTER PLUME; Timothy B. Smith, Wensheng Huang, Bryan M. Reid, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, MI 48105, USA

2007-253: A MEMS CNT-BASED NEUTRALIZER FOR MICRO-PROPULSION APPLICATIONS; Luis F. Valásquez-García and Akintunde I. Akinwande, Massachusetts Institute of Technology, Cambridge, MA 02139, USA

2007-254: NUMERICAL SIMULATION OF THE ZEEMAN EFFECT FROM LASER-INDUCED FLUORESCENCE OF NEUTRAL XENON; Bailo B. Ngom, Timothy B. Smith, Wensheng Huang, and Alec D. Gallimore, University of Michigan, Ann Arbor, MI 48109

2007-255: EXPERIMENTS OF ION ACCELERATION IN A MAGNETIC NOZZLE FOR AN ADVANCED PLASMA THRUSTER; Tatsuya Hagiwara, Akira Ando, Yuji Kasashima, Kunihiko Hattori, and Masaaki Inutake, Department of Electrical Engineering, Graduate School of Engineering, Tohoku University, 6-6-05, Aoba-yama, Sendai, 980-8579, Japan

2007-256: EMITTER DEPLETION MEASUREMENT AND MODELING IN THE T5&T6 KAUFMAN-TYPE ION THRUSTERS; Ismat M. Ahmed Rudwan and N. C. Wallace, Space Division, QinetiQ Plc Ltd, Farnborough, Hampshire, GU14 0LX, UK; Michele Coletti and Stephen B. Gabriel, Astronautics Research Group, SES, Southampton University, Hampshire, SO15 1BJ, UK

2007-257: ENVIRONMENTAL CONSIDERATIONS FOR XENON ELECTRIC PROPULSION; Mark W. Crofton and Toby D. Hain, The Aerospace Corporation, Los Angeles, CA, 90009, U.S.A.

2007-258: THE ROLE OF THE ELECTRON ENERGY BALANCE IN HALL THRUSTER PLASMA INSTABILITIES; Zbigniew Peradzynski, Institute of Applied Mathematics and Mechanics, University of Warsaw, 02-097, Warsaw, Poland, Institute of Fundamental Technological Research, Polish Academy of Sciences, 00-049, Warwaw, Poland; Karol Makowski, Serge Barral, and Jacek Kurzyna, Institute of Fundamental Technological Research, Polish Academy of Sciences, Warsaw, 00-049, Poland; Michel Dudeck, ICARE-CNRS, 45071 Orleans Cedex 2, France

2007-260: IONIZATION EFFICIENCY IN ELECTRIC PROPULSION DEVICES; Jerry L. Ross and Lyon B. King, Michigan Technological University, Houghton, MI

2007-261: THEORETICAL ANALYSIS OF THE INFLUENCE OF THE POWER SUPPLY ON BREATHING OSCILLATIONS IN HALL THRUSTERS; S. Barral, Instytut Podstawowych Problemów Techniki – PAN, Warsaw, 00049, Poland

2007-262: DEVELOPMENT HISTORY AND CURRENT STATUS OF DC-TYPE ION ENGINES AT JAXA; Shoji Kitamura, Kenichi Kajiwara, Hiroshi Nagano, and Yukio Hayakawa, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan

2007-264: EXPERIMENTAL INVESTIGATION OF INFLUENCING FACTORS FOR RELIABLE STARTUP AND STEADY WORK OF 100W MICROWAVE PLASMA THRUSTER; Xia Guang-qing, Mao Gen-wang, Yang Juan, and Chen Mao-lin, Northwestern Polytechnical University, National Key Laboratory of Combustion, Flow and Thermo-Structure, Xi’an, Shaanxi Province, 710072, P. R. China

2007-265: XIPS ION THRUSTER GRID EROSION ASSESSMENT FOR DEEP SPACE MISSIONS; Richard E. Wirz, John R. Anderson, Dan Goebel, and Ira Katz, California Institute of Technology, Jet Propulsion Laboratory, Pasadena, CA, 91109, USA

2007-266: RF PLASMA CATHODE-NEUTRALIZER FOR SPACE APPLICATIONS; Valery Godyak, Yevgeny Raitses, and Nathaniel J. Fisch, Princeton Plasma Physics Laboratory, Princeton, NJ 08543, USA

2007-267: BPT-4000 HALL THRUSTER DISCHARGE CHAMBER EROSION MODEL COMPARISON WITH QUALIFICATION LIFE TEST DATA; Richard R. Hofer, Ioannis G. Mikellides, Ira Katz, and Dan M. Goebel, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2007-268: ABSOLUTE EMISSION FROM THE MID-INFRARED TO THE EXTREME ULTRAVIOLET FROM A PULSED PLASMA THRUSTER (PPT); Edward J. Beiting, Jun Qian, Ray W. Russell, and James E. Pollard, The Aerospace Corporation, Los Angeles, CA 90009; Will Caven and Ron Corey, Space Systems/Loral, Palo Alto, CA 94303

2007-269: ELECTROMAGNETIC EMISSIONS FROM DC TO 17 GHZ FROM A PULSED PLASMA THRUSTER (PPT); Michael L. Garrett and  Edward J. Beiting, The Aerospace Corporation, Los Angeles, CA 90009; Will Caven and Ron Cory, Space Systems/Loral, Palo Alto, CA 94303

2007-270: COMPARATIVE HIGH-CURRENT-DENSITY EMITTERS POISONING OF HOLLOW CATHODES ELECTRIC PROPULSION; A. Taran, A. Loyan, and D. Voronovich, National Aerospace University “Kharkiv Aviation Institute”, Kharkiv, 61070, Ukraine

2007-271: QUALIFICATION OF COMMERCIAL ELECTRIC PROPULSION SYSTEMS FOR DEEP SPACE MISSIONS; Thomas M. Randolph, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California, 91109, U.S.A.

2007-272: DEVELOPMENT STATUS OF THE NONAMBIPOLAR ELECTRON SOURCE; Ben Longmier and Noah Hershkowitz, University of Wisconsin – Madison, Madison, WI 53706

2007-274: SOLELY EP BASED ORBIT CONTROL SYSTEM ON SMALL GEO SATELLITE; H. Lübberstedt, Th. Miesner, and A. Winkler, OHB-System AG, D-28359 Bremen, Germany; P. Rathsman and J. Kugelberg, Swedish Space Corporation, SE-17104 Solna, Sweden

2007-275: OVERVIEW OF ELECTRIC PROPULSION ACTIVITY IN RUSSIA; Semenkin A. V., Central Research Institute of Machine Building (TSNIIMASH), Pionerskaya 4, Korolev, Moscow region, Russia 141070; Testoedov N. A., Yakimov E. N., Ermoshkin Yu. M., Volkov D. V., Yukseev S. V., Scientific and Production Association of Applied Mechanic (NPO PM), Krasnoyarsk; Sevast’yanov N. N., Verkhoturov V. I., Romanov S. Yu., Samitov R. M., Borisenko A. A., and Ostrovsky V. G., Rocket and Space Corporation “Energia” (RSC “Energia”), Korolev city, Moscow, region; Makridenko L. A., Volkova S. N., and Khodnenko B. P., All-Russia Scientific Research Institute of Electro-Mechanic (VNIIEM), Moscow; Poletaev B. I., Lyannoy E. G., Romanov A. V., and Pavlov A. Yu, Design Bureau “Arsenal”, Saint-Petersburg; Partola I. S. and Kuznetsov S. V., State Space Scientific and Production Center named after M. V. Khrunichev, Moscow; Resh G. F., Arakin M. V., Savosin G. V., Prokhorchuk Yu. A., Maksimov I.I., Lizunov A. A., Kabanov B. A., Scientific and Production Association of Machine Building (NPO MASH), Reutov city, Moscow, region; Murashko V. M., Experimental Design Bureau “Fakel”, (EDB “Fakel”), Kaliningrad; Popov G. A., Kim V. P., Obukhov V. A, and Antropov N. N., Research Institute of Applied Mechanic and Eletrodynamics, (RIAME) Moscow; Morozov A. I. (Kurchatov Institute), Bugrova A. I., Sigov A. S., Lipatov A. S., and Kharchevnicov V. K., Moscow Institute of Radio Electronic and Automatic (MIREA), Moscoq; Lukyachenko V. I., Semenkin A. V., Garkusha V. I., and Tverdokhlebova E. M., Central Research Institute of Machine Building, (TSNIIMASH), Korolev city, Moscow region

2007-276: ENVIRONMENTAL TESTING OF THE NEXT PM1R ION ENGINER; John Steven Snyder and John R. Anderson, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109; Jonathan L. Van Noord and George C. Soulas, NASA Glenn Research Center, Cleveland, OH, 44135

2007-277: PLASMA POTENTIAL BEHAVIOR AND PLUME MODE TRANSITIONS IN HOLLOW CATHODE DISCHARGES; Dan M. Goebel, Kristina K. Jameson, Ira Katz, and Ioannis G. Mikellides, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2007-278: CATHODE COUPLING IN HALL THRUSTERS; Kristina K. Jameson, Dan M. Goebel, Richard R. Hofer, and Ron M. Watkins, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2007-279: PROPELLANT THROUGHPUT CAPABILITY OF THE DAWN ION THRUSTERS; John R. Brophy, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91101, USA

2007-280: MULTIIPLE BARE TETHERS FOR ELECTRODYNAMIC TETHER PROPULSION; Teppei Ikeda, Yasuhiro Nakamura, Yoshiki Yamagiwa, and Hirotaka Otsu, Shizuoka University, Hamamatsu, Shizuoka, 432-8561, Japan; Satomi Kawamoto, Yasushi Ohkawa, and Atsushi Nakajima, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan

2007-281: SIMULATION OF ARGON PLASMA FLOWS IN MAGNETOPLASMADYNAMIC THRUSTERS; M. H. Moghimi and M. Farshchi, Aerospace Engineering Department, Sharif University of Technology, Tehran, Iran

2007-283: POWER CONTROL UNIT FOR µN FEEP PROPULSION SUBSYSTEM; Luca Ceruti, Andrea Antimiani, and Aldo Polli, Galileo Avoinica S.p.A. Space Business Unit, Via Montefeltro, 8-20156 Milan, Italy

2007-284: FIELD EMISSION ELECTRIC THRUSTER OPTICAL DIAGNOSTICS BASED ON AN INDIUM COLLISIONAL-RADIATIVE MODEL; Konstantinos Katsonis, Laboratoire de Physique des Gaz et des Plasmas, UMR 8578, Université Paris-sud, 91405 Orsay, France; J. Bonnet and D. Packan, ONERA, 91761 Palaiseau, France; Marguerite Cornille, LUTH, Observatoire de Paris, CNRS, Univ. Paris Diderot, Place Jules Janssen, 92190 Meudon, France; Chloe Berenguer and Abdoulaziz Ndiaye, Laboratoire de Physique des Gaz et des Plasmas, UMR 8578, Université Paris-sud, 91405 Orsay, France

2007-285: A XENON COLLISIONAL-RADIATIVE MODEL FOR PLASMA THRUSTER OPTICAL DIAGNOSTICS AND MODELING; Konstantinos Katsonis and Chloe Berenguer, Laboratoire de Physique des Gaz et des Plasmas, UMR 8578, Université Paris-sud, 91405 Orsay, France; J. Bonnet and D. Packan, ONERA, 91761 Palaiseau, France; R.E.H. Clark, NDS, IAEA, Wagramerstr. 5, A-1400 Vienna, Austria; Marguerite Cornille, LUTH, Observatoire de Paris, CNRS, Univ. Paris Diderot, Place Jules Janssen, 92190 Meudon, France; Gilles Maynard, Laboratoire de Physique des Gaz et des Plasmas, UMR 8578, Université Paris-sud, 91405 Orsay, France

2007-286: PRELIMINARY EXPERIMENTAL MEASUREMENTS FOR A GALLIUM ELECTROMAGNETIC (GEM) THRUSTER; Robert E. Thomas, Rodney L. Burton, and Nick G. Glumac, University of Illinois, Urbana, IL, 61801; Kurt A. Polzin, NASA-Marshall Space Flight Center, Huntsville, AL 35812

2007-287: ELECTRIC PROPULSION PERFORMANCE FROM GEO-TRANSFER TO GEOSYNCHRONOUS ORBITS; John W. Dankanich and Gordon R. Woodcock, Gray Research Inc., Cleveland, OH, 44135, U.S.A.

2007-288: FLIGHT HARDWARE DEVELOPMENT OF COLLOID MICROTHRUSTER TECHNOLOGY FOR THE SPACE TECHNOLOGY 7 AND LISA MISSIONS; John K. Ziemer, Thomas M. Randolph, and Manuel Gamero-Castaño, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109; Vlad Hruby, William Connolly, Nathaniel Demmons, Eric Ehrbar, Roy Martin, and Tom Roy, Douglas Spence, Jurg Zwahlen, Busek Co., Natick, MA 01760

2007-290: A PULSED PLASMA THRUSTER USING MERCURY PROPELLANT: A LATE-1960S PROJECT AT THE ROYAL AEROSPACE ESTABLISHMENT, FARNBOROUGH; David G. Fearn, EP Solutions, 23 Bowenhurst Road, Church Crookham, Fleet, Hants, GU62 6HS, UK

2007-291: HALL THRUSTER ELECTRON MOBILITY INVESTIGATION USING FULL 3D MONTE CARLO TRAJECTORY SIMULATIONS; Darren A. Alman, Joshua L. Rovey, Robert A. Stubbers, and Brian E. Jurczyk, Starfire Industries LLC, Champaign, IL, 61820

2007-293: VERIFICATION OF ANALYSIS TOOL OF THRUSTER PLUME INTERACTIONS FOR SPACECRAFT; Satoshi Hosoda, Japan Aerospace Exploration Agency, Sagamihara, Kangagawa, 229-8510, Japan; Naomi Kurahara and Mengu Cho, Kyushu Institute of Technology, Kitakyushu, Fukuoka, 804-8550, Japan; Takanobu Muranaka and Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, Kangagawa, 229-8510, Japan; Hiroko O. Ueda, Kiyokazu Koga, and Tateo Goka, Japan Aerospace Exploration Agency, Tsukuba, Ibaraki, 305-8505, Japan

2007-294: INNOVATIVE ARCHITECTURES DEVELOPED FOR THE POWER SUPPLY CONTROL UNITS OF THE ION THRUSTERS FOR INCOMING PROGRAMS; C. Tato, F. de la Cruz, and J. Palencia, Electronic Engineer, Madrid – Tres Cantos 28760 – Spain

2007-295: POWER CONTROL UNIT FOR ION PROPULSION ASSEMBLY IN GOCE PROGRAM; C. Tato, F. de la Cruz, and J. Palencia, Electronic Engineer, Madrid – Tres Cantos 28760 – Spain

2007-300: HIGH FREQUENCY BURST PULSED PLASMA THRUSTER RESEARCH AT THE UNIVERSITY OF SOUTHAMPTON; R. I. Marques and S. B. Gabriel, University of Southampton, SO17 1BJ, United Kingdom; F. de S. Costa, Instituto Nacional de Pesquisas Espaciais, Cachoeira Paulista, SP, 12630-000, Brazil

2007-301: THALES ALENIA SPACE EXPERIENCE ON PLASMA PROPULSION; Michael Lyszyk and Laurent Lecardonnel, Thales Alenia Space, Cannes, 06150, France

2007-302: IONS FORMATION DENSITY DISTRIBUTION IN SPT ATON CHANNEL; M. V. Kozintseva, G. E. Bugrov, and I. A. Tarelkin, Moscow Institute of Radio-engineering, Electronics and Automatics, Moscow, Russia

2007-304: POWER CONSTRAINED ELECTRIC PROPULSION MISSIONS TO THE OUTER PLANETS; K. Geurts, C. Casaregola, P. Pergola, and M. Andrenucci, ALTA S.p.A., Via Gherardesca 5, 56121, Pisa, Italy

2007-305: THREE BODY INVARIANT MANIFOLD TRANSITION WITH ELECTRIC PROPULSION; P. Pergola, K. Geurts, C. Casaregola, and M. Andrenucci, ALTA S.p.A., Via Gherardesca 5, 56121, Pisa, Italy

2007-306: A VEGA DEDICATED ELECTRIC PROPULSION TRANSFER MODULE TO THE MOON; C. Casaregola, K. Geurts, P. Pergola, L. Biagioni, M. Andrenucci, Alta S.p.A., Pisa, 56121, Italy

2007-307: ANALYSIS OF HALL-EFFECT THRUSTERS APPLICATION TO FORMATION FLYING AND DRAG COMPENSATION; P. Rossetti, Alta S.p.A., Pisa, 56121, Italia; D. Valentian, Snecma, Vernon, 27208, France

2007-308: NUMERICAL ANALYSIS OF THE ACCELERATION PROCESS IN CLUSTER FRAGMENTATION ION SOURCES; P. Rossetti, F. Paganucci, and F. Nania, Alta SpA, Pisa, 56121, Italia; C. R. Gebhardt, Clustec Gmbh, Munchen, 81475, Germany; H. Schröder, Max-Planck-Institut für Quantenoptik, Garching, D-85748, Germany

2007-309: REVIEW OF RF PLASMA THRUSTER DEVELOPMENT; Ivana Hrbud, G. Elijah Kemp, Allen H. Yan, and Jacob G. Gedrimas, Purdue University, West Lafayette, IN 47907, USA

2007-311: HIGH POWER THRUSTERS DESIGN OPTIONS; Tommaso Misuri, Ph.D. Student, Dipartimento di Ingegneria Aerospaziale, Universitá di Pisa, Pisa, 56122, Italy; Francesco Battista, Research Engineer, CIRA Italian Aerospace Research Centre, Capua, 83100, Italy, Ph.D. Student, Dipartimento di Ingegneria Aerospaziale, Universitá di Pisa, Pisa, 56122, Italy; Christian Barbieri, Graduate Student, Dipartimento di Ingegneria Aerospaziale, Universitá di Pisa, Pisa, 56122, Italy; Enrico Alessio De Marco, Ph.D. Student, Dipartimento di Ingegneria Aerospaziale, Universitá di Pisa, Pisa, 56122, Italy; Mariano Andrenucci, Professor of Electric Propulsion, Dipartimento di Ingegneria Aerospaziale, Universitá di Pisa, Pisa, 56122, Italy, Chairman of ALTA SpA, Ospedaletto, Pisa, 56121, Italy

2007-313: A REVIEW OF THE HALL THRUSTER SCALING METHODOLOGY; Francesco Battista, Research Engineer, CIRA Italian Aerospace Research Centre, Capua, 83100, Italy, Ph.D. Student, Dipartimento di Ingegneria Aerospaziale, Universitá di Pisa, Pisa, 56122, Italy; Enrico Alessio De Marco and Tommaso Misuri, Ph.D. Students, Dipartimento di Ingegneria Aerospaziale, Universitá di Pisa, Pisa, 56122, Italy; Mariano Andrenucci, Professor of Electric Propulsion, Dipartimento di Ingegneria Aerospaziale, Universitá di Pisa, Pisa, 56122, Italy, Chairman of ALTA SpA, Ospedaletto, Pisa, 56121, Italy

2007-316: STUDY ON PLASMA LENS OF HALL THRUSTERS IN DIFFERENT OPERATING MODES; Jie Li, Da-Ren Yu, and Yong Li, harbin Institute of Technology, Harbin, Heilongjiang, 150001, China

2007-317: NUMERICAL SIMULATION FOR MAGNETIC MIRROR EFFECT ON ELECTRON MOVEMENT IN A HALL THRUSTER; Daren Yu, Hui Lu, and Haiyang Fu, HIT Plasma Propulsion Laboratory, Harbin, Heilongjiang, 15001, China

2007-319: VICTOR B. TIKHONOV’S MHD CHANNEL THEORY: A REVIEW; Tommaso Misuri, Ph.D. Student, Dipartimento di Ingegneria Aerospaziale, Universitá di Pisa, Pisa, 56122, Italy; Mariano Andrenucci, Professor of Electric Propulsion, Dipartimento di Ingegneria Aerospaziale, Universitá di Pisa, Pisa, 56122, Italy, Chairman of ALTA SpA, Ospedaletto, Pisa, 56121, Italy

2007-320: EXPERIMENTAL CHARACTERIZATION OF THE HT-100 HALL THRUSTER IN TWIN ENGINE CLUSTER CONFIGURATION; M. Saverdi, M. Signori, and L. Biagioni, Alta SpA, via A. Gherardesca 5, I-56014 Ospedaletto (PI), Italy

2007-321: THE IV10 SPACE SIMULATOR FOR HIGH POWER ELECTRIC PROPULSION TESTING: PERFORMANCE IMPROVEMENTS AND OPERATION STATUS; M. Saverdi, M. Signori, L. Milaneschi, U. Cesari, and L. Biagioni, Alta SpA, via A. Gherardesca 5, I-56014 Ospedaletto (PI), Italy

2007-325: VALIDATION STATUS OF THE PICPLUS PLUME SIMULATION AND SPACECRAFT ITNERACTION TOOLS: LESSON LEARNT FROM FLIGHT AND GROUND EXPERIMENTAL DATA; A. Passaro, A. Vicini, and F. Nania, Alta SpA, Pisa, 56121, Italy

2007-328: CAPILLARY DISCHARGE BASED PULSED PLASMA THRUSTERS; Jean-Luc Cambier, Air Force Research Lab, 10. E. Saturn Blvd. Edwards AFB, CA 93524, United States; Marcus Young and Leonid Pekker, ERC Inc., 10. E. Saturn Blvd. Edwards AFB, CA 93524, United States; Anthony Pancotti, University of Southern California, 854 W. 36th Place, RRB 101, Los Angeles, CA 90089, United States

2007-330: EXPERIMENTAL ASSESSMENT OF A PASSIVE METHOD FOR MHD INSTABILITY SUPPRESSION IN MPD THRUSTERS; F. Paganucci and M. Andrenucci, Alta/Centrospazio, via A. Gherardesca 5, 56014 Pisa, Italy, Department of Aerospace Engineering, University of Pisa, via Caruso, 56122 Pisa, Italy; P. Rossetti and M. De Tata, Alta/Centrospazio, via A. Gherardesca 5, 56014 Pisa, Italy; V. Antoni, R. Cavazzana, E. Martines, G. Serianni, and F. Tarallo, Consorzio RFX, Associazione Euratom-Enea sulla Fusione, corso Stati Uniti 4, 35127 Padova, Italy

2007-331: MAGNETIC FLUCTUATIONS IN A MPD THRUSTER WITH PASSIVE SYSTEMS FOR THE CONTROL OF MHD INSTABILITIES; M. Zuin, V. Antoni, R. Cavazzana, E. Matines, G. Serianni, and F. Tarallo, Consorzio RFX, Associazione Euratom-Enea Sulla Fusione, corso Stati Uniti 4, 35127 Padova, Italy; M. Andrenucci and F. Paganucci, Alta/Centrospazio, via A. Gherardesca 5, 56014 Pisa, Italy, Department of Aerospace Engineering, University of Pisa, via Caruso, 56122 Pisa, Italy

2007-334: AEDC PLUME MEASUREMENTS USING BI-DIRECTIONAL ION FLUX PROBES; Yevgeny Raitses, Princeton Plasma Physics Laboratory, Princeton, NJ, 08543, USA; Trevor Moeller, University of Tennessee Space Institute, Tullahoma, TN, 37355, USA; James Szabo, Busek Co., Inc., Natick, MA, 01760, USA

2007-335: PERFORMANCE AND PLASMA CHARACTERISTICS OF A CUSP AND DIVERGENT-NOZZLE APPLIED-MAGNETIC-FIELD MPD THRUSTER; Hirokazu Tahara and Yoichi Kagaya, Osaka Institute of Technology, Asahi, Osaka 535-8585, Japan

2007-336: INFLUENCES OF MAGNETIC FIELD TOPOGRAPHY AND DISCHARGE CHANNEL STRUCTURE ON PERFORMANCE OF ANODE-LAYER HALL THRUSTERS; Seiro Yuge, Yoshihiro Kuwamura, and Hirokazu Tahara, Osaka Institute of Technology, Asahi, Osaka 535-8585, Japan

2007-337: PERFORMANCE CHARACTERISTICS OF ELECTROTHERMAL PULSED PLASMA THRUSTERS WITH INSULATOR-ROD-ARRANGED CAVITIES AND TEFLON-ALTERNATIVE PROPELLANTS; Hirokazu Tahara, Toshiaki Edamitsu, and Hirokazu Sugihara, Osaka Institute of Technology, Asahi, Osaka 535-8585, Japan

2007-338: EFFECTS OF MAGNETIC FIELD CONFIGURATION AND ELECTRICALLY-FLOATING METAL PLATES IN HALL THRUSTERS WITH CIRCULAR CROSS-SECTIONAL DISCHARGE CHAMBERS; Hirokazu Tahara and Atsushi Shirasaki, Osaka Institute of Technology, Asahi, Osaka 535-8585, Japan

2007-339: RESEARCH AND DEVELOPMENT OF COMPACT LASER ABLATIVE THRUSTERS FOR SMALL SATELLITES; Hirokazu Tahara, Osaka Institute of Technology, Asahi, Osaka 535-8585, Japan

2007-340: GROUND-BASED EXPERIMENT OF CURRENT COLLECTION TO BARE TETHER IN HIGH-SPEED MAGNETIZED PLASMA; Hirokazu Tahara, Osaka Institute of Technology, Asahi, Osaka 535-8585, Japan

2007-343: A 3D MODEL OF ELECTRON DYNAMICS NEAR THE OUTLET SECTION OF SPT THRUSTER; Grigory Toropov, Moscow Aviation Institute (State Technical University) MAI, Engineering Plasma Computational Laboratory (EPCLab), 24b-120, Zalineynaya str., Vologda, 160010, Russia; Sergey Khartov, Moscow Aviation Institute (State Technical University) MAI, Electric Propulsion and Space Power Plants Department, 4, Volokolamskoe sh., Moscow, 125971, Russia

2007-346: CONTINUING DEVELOPMENT OF THE PROPORTIONAL FLOW CONTROL VALVE (PFCV) FOR ELECTRIC PROPULSION SYSTEMS; David M. Pehrson, Moog Inc., Space and Defense Group, East Aurora, NY, 14052, USA

2007-347: DEVELOPMENT OF NEUTRALIZER WITH CARBON NANOTUBE CATHODE FOR SMALL SCALE ION ENGINER; Yoshiyuki Takao, Akihiro Kugimiya, and Shinobu Nagai, Oita National College of Technology, 1666 Maki, Oita City, 870-0152, Japan; Naoji Yamamoto and Hideki Nakashima, Kyushu University, Kasuga, 816-8580, Japan

2007-352: ELECTRIC SAIL PROPULSION MODELING AND MISSION ANALYSIS; Pekka Janhunen, Finnish Meteorological Institute, FIN-00101 Helsinki, Finland; Giovanni Mengali and Alessandro A. Quarta, University of Pisa, I-56122 Pisa, Italy

2007-353: APPLICATION OF A VARIATIONAL MHD PRINCIPLE TO THE STUDY OF PLASMA THRUSTERS; Tommaso Andreussi, Scuola Normale Superiore, Pisa, 56100, Italy; Francesco Pegoraro, Phys. Dept., University of Pisa, Pisa, 56127, Italy

2007-354: ELECTRIC PROPULSION REQUIREMENTS AND MISSION ANALYSIS UNDER NASA’S IN-SPACE PROPULSION TECHNOLOGY PROJECT; Leonard A. Dudzinski and Eric J. Pencil, NASA Glenn Research Center, Cleveland, OH 44135, USA; John W. Dankanich, Gray Research, Inc., Cleveland, OH 44135, USA

2007-356: INDIRECT OPTIMIZATION METHOD FOR LOW-THRUST INTERPLANETARY TRAJECTORIES; Lorenzo Casalino, Guido Colasurdo, and Matteo Rosa Sentinella, Politecnico di Torino, Turin, 10129, Italy

2007-357: NUCLEAR ACTIVIATION ENHANCED MHD AND MPD THRUSTER; Samim Anghaie, Innovative Nuclear Space Power & Propulsion Institute (INSPI), University of Florida, Gainesville, FL 32611-8300; Angelo Ferrair, New Era Technology, Inc. (NeTecH) 3720 NW 43rd Street, Suite 105, Gainesville, FL 32606

2007-358: ADVANCING JAPANESE ELECTRIC PROPULSION; Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, 299-8510, Japan; Kimiya Komurasaki, The University of Tokyo, Kashiwa, 277-8561, Japan

2007-359: THE NEW NASA-STD-4005 AND NASA-HDBK-4006, ESSENTIALS FOR DIRECT-DRIVE SOLAR ELECTRIC PROPULSION; Dale C. Ferguson, NASA Marshall Space Flight Center, Huntsville, Alabama, 35812, USA

2007-360: RELATIONSHIP BETWEEN ANODE SPOTS AND ONSET VOLTAGE HASH IN QUASI-STEADY MAGNETOPLASMADYNAMIC THRUSTERS; Luke Uribarri and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory, Princeton Unviersity, Princeton, NJ, 08544

2007-361: UKRAINIAN SPT-20 HALL EFFECT THRUSTER: ANALYSIS OF THE PLUME BY OPTICAL EMISSION SPECTROSCOPY; D. Pagnon, Laboratoire de Physique des Gaz et des Plasmas, Orsay 91405, France; S. Pellerin Laboratoire d’Analyse Spectroscopique et d’Energétique de Plasmas, Bourges 18028, France; M. Dudeck, Laboratoire ICARE, Orléans 45071, France; A. V. Loyan, T. A. Maksymenko, and N. N. Koshelev, National Aerospace University “KhAI”, 61070 Kharkov, Ukraine

2007-362: SPIS MODELING OF FEEP THRUSTERS FOR LISA PATHFINDER; Bjarne Adnersson, Davide Nicolini, and Eric Gengembre, European Space Agency, ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands

2007-363: LISA PATHFINDER FIELD EMISSION THRUSTER SYSTEM DEVELOPMENT PROGRAM; Davide Nicolini, European Space Agency, ESTEC, Noordwijk, 2201 AZ, The Netherlands

2007-364: ANALYSIS OF RF THRUSTERS WITH TOPICA AND A GLOBAL SYSTEM-LEVEL MODEL; Vito Lancellotti, Giuseppe Vecchi, and Riccardo Maggiora, Dipartimento di Elettronica, Politecnico di Torino, Torino, I-10129, Italy; Daniele Pavarin and Simone Rocca, CISAS G. Colombo, Padova, I-35131 Italy; Cristina Bramanti, Advanced Concepts Team, ESA-ESTEC, Noordwijk, The Netherlands

2007-365: ION CURRENT IN HALL THRUSTERS; Ira Katz, Richard R. Hofer, and Dan M. Goebel, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2007 FILE DIRECTORY

IEPC-2007-001.pdf 03-Sep-2007 02:38  2.7M

IEPC-2007-002.pdf 01-Sep-2007 19:39  2.9M

IEPC-2007-004.pdf 01-Sep-2007 19:31  809K

IEPC-2007-005.pdf 02-Sep-2007 10:11  2.1M

IEPC-2007-006.pdf 29-Aug-2007 10:04  588K

IEPC-2007-007.pdf 31-Aug-2007 21:34  162K

IEPC-2007-008.pdf 29-Aug-2007 10:08  587K

IEPC-2007-009.pdf 16-Aug-2007 14:36  852K

IEPC-2007-010.pdf 02-Sep-2007 10:10  598K

IEPC-2007-011.pdf 06-Jul-2007 17:44  286K

IEPC-2007-012.pdf 30-Aug-2007 11:17  1.5M

IEPC-2007-014.pdf 04-Sep-2007 18:09  417K

IEPC-2007-015.pdf 03-Sep-2007 02:15  1.3M

IEPC-2007-016.pdf 03-Sep-2007 02:18  1.7M

IEPC-2007-017.pdf 01-Sep-2007 07:36  408K

IEPC-2007-018.pdf 05-Sep-2007 05:34  476K

IEPC-2007-019.pdf 04-Sep-2007 19:42  445K

IEPC-2007-020.pdf 30-Aug-2007 01:54  1.2M

IEPC-2007-021.pdf 30-Aug-2007 16:53  265K

IEPC-2007-023.pdf 02-Sep-2007 23:27  305K

IEPC-2007-024.pdf 02-Sep-2007 23:25  1.3M

IEPC-2007-025.pdf 06-Sep-2007 10:39  1.3M

IEPC-2007-026.pdf 03-Jul-2007 13:39  281K

IEPC-2007-027.pdf 30-Aug-2007 06:01  612K

IEPC-2007-029.pdf 28-Aug-2007 18:04  611K

IEPC-2007-030.pdf 09-Sep-2007 14:04  447K

IEPC-2007-031.pdf 09-Sep-2007 14:04  1.1M

IEPC-2007-032.pdf 30-Aug-2007 21:36  252K

IEPC-2007-033.pdf 31-Aug-2007 20:31  2.5M

IEPC-2007-034.pdf 02-Sep-2007 02:34  320K

IEPC-2007-035.pdf 30-Aug-2007 10:01  184K

IEPC-2007-036.pdf 30-Aug-2007 18:55  583K

IEPC-2007-037.pdf 15-Sep-2007 01:57  1.2M

IEPC-2007-038.pdf 03-Sep-2007 09:01  649K

IEPC-2007-039.pdf 01-Sep-2007 20:48  1.0M

IEPC-2007-041.pdf 01-Sep-2007 02:54  1.3M

IEPC-2007-042.pdf 02-Sep-2007 19:42  235K

IEPC-2007-043.pdf 30-Aug-2007 16:55  566K

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IEPC-2007-048.pdf 30-Aug-2007 01:12  1.7M

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IEPC-2007-055.pdf 02-Sep-2007 17:44  330K

IEPC-2007-056.pdf 01-Sep-2007 11:40  541K

IEPC-2007-057.pdf 02-Sep-2007 21:58  775K

IEPC-2007-058.pdf 01-Sep-2007 14:34  469K

IEPC-2007-060.pdf 31-Aug-2007 16:54  399K

IEPC-2007-061.pdf 02-Sep-2007 22:15  1.2M

IEPC-2007-062.pdf 09-Sep-2007 14:06  967K

IEPC-2007-066.pdf 07-Sep-2007 03:46  668K

IEPC-2007-067.pdf 04-Sep-2007 21:28  1.0M

IEPC-2007-069.pdf 30-Aug-2007 00:54  843K

IEPC-2007-070.pdf 30-Aug-2007 00:58  268K

IEPC-2007-071.pdf 31-Aug-2007 04:20  560K

IEPC-2007-072.pdf 06-Aug-2007 22:26  386K

IEPC-2007-073.pdf 31-Aug-2007 04:30  3.3M

IEPC-2007-074.pdf 08-Sep-2007 04:27  1.3M

IEPC-2007-075.pdf 08-Sep-2007 04:27  311K

IEPC-2007-077.pdf 04-Sep-2007 05:05  3.7M

IEPC-2007-078.pdf 03-Sep-2007 00:45  4.5M

IEPC-2007-079.pdf 09-Sep-2007 14:06  188K

IEPC-2007-080.pdf 02-Sep-2007 23:38  1.0M

IEPC-2007-081.pdf 03-Sep-2007 04:00  783K

IEPC-2007-082.pdf 03-Sep-2007 09:12  367K

IEPC-2007-083.pdf 08-Sep-2007 03:54  1.7M

IEPC-2007-084.pdf 31-Aug-2007 13:22  285K

IEPC-2007-085.pdf 06-Sep-2007 16:26  524K

IEPC-2007-086.pdf 02-Sep-2007 22:09  3.0M

IEPC-2007-087.pdf 04-Sep-2007 15:54  1.5M

IEPC-2007-088.pdf 31-Aug-2007 13:47  453K

IEPC-2007-089.pdf 31-Aug-2007 14:08  489K

IEPC-2007-090.pdf 01-Sep-2007 11:52  1.7M

IEPC-2007-091.pdf 01-Sep-2007 21:58  125K