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 Index Continued