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