2013 Index

2013-33: WEAR TEST OF A MAGNETICALLY SHIELDED HALL THRUSTER AT 3000 SECONDS SPECIFIC IMPULSE; Richard R. Hofer, Benjamin A. Jorns, James E. Polk, Ioannis G. Mikellides, and John Steven Snyder, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2013-37: EUROPEAN SPACE AGENCY ACTIVITIES IN ELECTRIC PROPULSION; Jose Gonzalez del Amo, European Space Agency, Noordwijk, 2200AG, The Netherlands

2013-44: PEAK POWER TRACKING AND MULTI-THRUSTER CONTROL IN DIRECT DRIVE SYSTEMS; John Steven Snyder and John R. Brophy, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2013-45: SOLAR ELECTRIC PROPULSION (SEP) BENEFITS FOR NEAR TERM SPACE EXPLORATION; Luke DeMaster-Smith, Scott Kimbrel, Christian Carpenter, Steve Overton, Roger Myers, and David King, Aerojet Rocketdyne, Inc., Redmond, WA 98052

2013-47: INITIAL FLIGHT TEST RESULTS OF THE LIPS-200 ELECTRIC PROPULSION SYSTEM ON SJ-9A SATELLITE; Zhang Tianping, Wang Xiaoyong, Jiang Haocheng, Wang Shaoning, Gao Jun, Xu Jinling, Cui Tieming, Yang Fuqan, Guo Ning, Tang Fujun, Chen Xuekang, Lanzhou Institute of Physics, Lanzhou, Gansun, 730000, China

2013-48: THE ELECTRIC PROPULSION DEVELOPMENT IN LIP; Zhang Tianping, Sun Mingming, Long Jianfei, and Zhou Haocheng, Lanzhou Institute of Physics, Lanzhou, Gansu Province, 730000, China

2013-51: INFLUENCE OF SPT MAGNETIC FIELD ON LIFE TIME CHARACTERISTICS OF THE THRUSTER; Olga A. Mitrofanova and Roman Yu. Gnizdor, EDB “Fakel”, Kaliningrad, Russia

2013-52: DEVELOPMENT AND RESEARCH OF THE PLASMA THRUSTER WITH A HOLLOW MAGNET ANODE PLAS-40; M. Yu. Potapenko, V. V. Gopanchuk, FSUE EDB Fakel, Kaliningrad, 236001, Russia

2013-53: NEAR FIELD MAPS OF XENON ION VELOCITY OF THE SPT-140 HALL THRUSTER BY LASER INDUCED FLUORESCENCE; Edward J. Beiting, Rostislav Spektor, and Kevin D. Diamant, The Aerospace Corporation, P.O. Box 929057 – M2/341, Los Angeles, CA 90009, USA; Ron Corey and Jorge Delgado, Space Systems/Loral, 3825 Fabian Way, Palo Alto, CA 94303, USA

2013-54: AUTONOMOUS TESTS OF THE CATHODE FOR USE IN THE DISCHARGE CHAMBER OF THE HIGH POWER ION THRUSTER; A. S. Lovtsov, P. M. Puchkov, and V. N. Shutov, SSC FSUE Keldysh Research Centre, Onezhskaya, 8, & Moscow, Russia, 125438

2013-55: DEVELOPMENT AND QUALIFICATION OF HALL THRUSTER KM-60 AND THE FLOW CONTROL UNIT; A. N. Kostin, A. S. Lovtsov, A. I. Vasin, and V. V. Vorontsov, SSC FSUE Keldysh Research Centre, Onezhskaya, 8, Moscow, Russia, 125438

2013-56: ON SCALING OF HALL EFFECT THRUSTERS; Andrey A. Shagayda, Keldysh Research Center, Moscow, 125438, Russia

2013-57: FARFIELD PLUME MEASUREMENT AND ANALYSIS ON THE NASA-300M AND NASA-300MS; Wensheng Huang, Rohit Shastry, George C. Soulas, and Hani Kamhawi, National Aeronautics and Space Administration Glenn Research Center, Cleveland, Ohio, 44135, USA

2013-58: EFFECT OF BACKGROUNG PRESSURE ON THE PERFORMANCE AND PLUME OF THE HIVHAC HALL THRUSTER; Wensheng Huang, Hani Kamhawi, and Thomas Haag, National Aeronautics and Space Administration Glenn Research Center, Cleveland, Ohio, 44135, USA

2013-60: HOLLOW CATHODE LIFE TEST FOR THE 80 MN HALL THRUSTER; Qiao Caixia, Kang Xiaolu, Yu Shuilin, Zhang Yan, Hang Guanrong, and Zhao Zhen, Shanghai Institute of Space Propulsion, Shanghai, 201112, China

2013-62: AN ELECTRIC PROPULSION SYSTEM BASED ON CONTROLLED FUSION AND ELECTROMECHANICAL ENERGY CONVERSION; P. J. Turchi, Santa Fe, New Mexico, USA

2013-63: EPS-500 DEVELOPMENT STATUS; F. Marchandise, V. Vial, M. Oberg and N. Cornu, Snecma Direction Moteurs Spatiaux, Vernon, 27200, France, D. Barbier, Sagem Défense Sécurité, Valence, 26000, France, N. Arcis, CNES, Toulouse, 31401, France

2013-64: A NEW ORBIT CONTROL ALGORITHM FOR THE 20 MN CLASS ION ENGINE SYSTEM; Hiroshi Nagano and Yukio Hayakawa, Japan Aerospace Exploration Agency, Chofu, 182-8522, Japan, Hiroyuki Osuga, Toshiyuki Ozaki, and Kazuo Shuto, Mitsubishi Electric Corporation, Kamakura, 247-8520, Japan

2013-65: ACTIVITIES OF VNIIEM IN EPT FIELD HISTORY, OUR DAYS AND PROSPECTS; Vladimir P. Khodnenko, VNIIEM ‘Corporation’ JSD, Address: POB 496, Glavpochtamt, Moscow, 101000, Russia

2013-66: IONOSFERE SATELLITE WITH APPT BASED EPS; Research Institute of Applied Mechanics and Electrodynamics, 4, Volokolamskoye shosse, Moscow, 125810, Russia, Michael N. Kazeev, National Research Centre Kurchatov Institute, I, Kurchatov sq., Moscow, 123182, Russia, Vladimir P. Khodnenko, VNIIEM Corporation’ JSC, 101000, P. O. Box 496, Moscow, Russia

2013-67: NON-EQUIDISTANT PARTICLE-IN-CELL FOR ION THRUSTER PLUMES; K. F. Luskow, J. Duras, O. Kalentev, K. Matyash, J. Geiser, and R. Schneider, Ernst-Moritz-Arndt Universitat Greifswald, Felix-Hausdorff-Strabe 12, 17489 Greifswald, Germany, D. Tskhakaya, Institute of Applied Physics, Vienna University of Technology, Wiedner Hauptstrasse 8-10/E134, A-1040 Vienna, Austria

2013-68: ABLATIVE PULSED PLASMA THRUSTERS R&D IN RUSSIA SINCE THE BEGINNING OF THE 90S; Nickolay N. Antropov and Garry A. Popov, Research Institute of Applied Mechanics and Electrodynamics, 4, Volokolamskoye shosse, Moscow, 125810, Russia, Michael N. Kazeev, National Research Centre Kurchatov Institute, pl. Kurchatove, I. Moscow, 123182, Russia

2013-70: PRECISE ATTITUDE CONTROL OF ALL-ELECTRIC GEO SPACECRAFT USING XENON MICROTHRUSTERS; Mirko Leomanni, Andrea Garulli, and Antonio Giannitrapani, Universitá di Siena, Siena,  53100, Italy, Fabrizio Scortecci, Aerospazio Tecnologie s.r.l., Rapolano Terme, Siena, 53040, Italy

2013-71: ION BEAM INSTABILITY IN HALL THRUSTERS; A. Kapulkin and E. Behar, Asher Space Research Institute, Technion-Israel Institute of Technology, Haifa, 32000, Israel, Y. Raitses, Princeton Plasma Physics Laboratory, Princeton University, Princeton, NJ, 08543, USA

2013-72: GENERATION OF MICROWAVE RANGE ELECTROMAGNETIC RADIATION IN THE HALL THRUSTER PLASMA; Sergey A. Oghienko, National Aerospace University “Kharkiv Aviation Institute”, Kharkiv, 61070, Ukraine

2013-73: SELF-CONSISTENT SIMULATIONS OF INTERACTIONS BETWEEN SPACECRAFT AND PLUMES OF ELECTRIC THRUSTERS; Carlos Ardura, Sogeti High Tech of Astrium Satellites, Toulouse, 31000 France, and Fred Gengembre, ESAESTEC, Noordwijk 2201, The Netherlands

2013-76: HIGH CURRENT HOLLOW CATHODE PLASMA PLUME MEASUREMENTS; Robert e. Thomas and Hani Kamhawi, NASA Glenn Research Center, Cleveland, OH, 44135, USA, George J. Williams, Jr., Ohio Aerospace Institute, Cleveland, OH, 44135, USA

2013-77: WALL-INDUCED CROSS-FIELD ELECTRON TRANSPORT WITH OBLIQUE MAGNETIC FIELD LINES; Jan Miedzik and Serge Barral, Institute of Plasma Physics and Laser Microfusion, 01-497 Warsaw, Poland, Stephan Zurbach, Snecma, Safran Group, 27208 Vernon, France

2013-079: SPATIALLY RESOLVED MOMENTUM FLUX MEASUREMENTS FOR THRUSTER PLUME DIAGNOSTICS; Alexander Spethmann, Thomas Trottenberg, and Holger Kersten, Institute of Experimental and Applied Physics, University of Kiel, 24098 Kiel, Germany

2013-80: AZIMUTHAL OSCILLATIONS AND DYNAMICS OF ELECTRONS INTO CHANNEL OF STATIONARY PLASMA THRUSTER; A. N. Veselovzorov, A. A. Pogorelov, E. B. Svirsky, V. A. Smirnov, National Research Centre ‘Kurchatov Institute’ Moscow, Russia

2013-82: NEAR-EARTH ASTEROID RETRIEVAL MISSION (ARM) STUDY; John R. Brophy and Brian Muirhead, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA

2013-83: EXPERIMENTAL RESEARCH OF DEFLECTION OF SPT THRUST VECTOR; Marina V. Kozintseva, Andrew M. Bishaev, Antonina I. Bugrova, Gleb E. Bugrov, Alexey V. Desyatskov, Alexander S. Lipatov, Vadim K. Kharchevnikov, and Pavel G. Smirnov, Moscow State Technical University of Radioengineering, Electronics and Automation, Moscow, 119454, Russia

2013-85: NUMERICAL DETERMINIATION OF INDUCED ELECTRIC EDDY FIELDS INSIDE ARBITRARILY SHAPED INDUCTION COILS; Chris Volkmar, Jens Simon, and Ubbo Ricklefs, Technische Hochschule Mittelhessen University of Applied Sciences, 35390 Giessen, Germany

2013-86: TRAVELING MAGNETIC FIELD PLASMA ACCELERATOR; Andrea Lucca Fabris, University of Padova, Padova, 35131, Italy; Mark A. Cappelli, Stanford University, Stanford, CA 94305, USA

2013-88: ENTROPY CLOSURE MODEL FOR TRANSPORT IN HALL THRUSTER SIMULATIONS; M. A. Cappelli and E. Cha, Stanford University, Stanford, CA 94305, USA, and E. Fernandez, Eckerd College, St. Petersburg, FL 33711

2013-89: LOW AND HIGH FREQUENCY OSCILLATIONS OF THE ACCELERATING ELECTRIC FIELD IN A HALL THRUSTER; J. Vaudolon, B. Khiar, and S. Mazouffre, CNRS – ICARE (Institut de Combustion, Aerothermique, Reactivite et Environnement), 1C, Avenue de la Recherche Scientifique, 45071 Orleans Cedex 2, France

2013-90: EXPERIMENTAL VALIDATION OF RIT MICRO-PROPULSION SUBSYSTEM PERFORMANCE AT EPL; D. Di Cara, A. Bulit, J. Gonzalez del Amo, and J. A. Romera, ESA/ESTEC, 2201AZ Noordwijk, The Netherlands, H. Leiter, D. Lauer, C. Altmann, and R. Kukies, Astrium GmbH BL Equipement and Propulsion, 74215 Mockmuhl, Germany, A. Polli, L. Ceruti, and A. Antimiani, SELEX ES, 20014 Nerviano, Italy, D. Feili and B. Lotz, I. Physics Institute of Justus Liebig University, Giessen, 35392, Germany, L. Serafini, Astrium SrL, 00196, Rome, Italy

2013-93: ALL EP PLATFORM: MISSION DESIGN CHALLENGES AND SUBSYSTEM DESIGN OPPORTUNITIES; E. Rezugina and A. Demairé, OHB Sweden AB, Solna, SE-17122, Sweden; A. Edfors, B. Andersson, P. Rathsman, E. Lamoureux and F. Sjöberg, OHB Sweden AB, Solna, SE-17122, Sweden; M. De Tata, OHB System AG, Bremen, 28359, Germany

2013-94: PERFORMANCE CHARACTERISTICS OF STEADY-STATE MPD THRUSTERS WITH PERMANENT MAGNETS AND MULTI HOLLOW CATHODES FOR IN-SPACE PROPULSION; Norihide Koyama, Tomoya Suzuki, Taisuke Kubota, and Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-Ku, Osaka 535-8585, Japan

2013-95: PERFORMANCE CHARACTERISTICS OF LOW-POWER ARCJET THRUSTERS USING LOW TOXICITY PROPELLANT HAN DECOMPASED GAS; Kazuma Matsumoto, Akira Iwakai, Fumihiro Inoue, and Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-Ku, Osaka 535-8585, Japan, Taiichi Nagata and Ideo Masuda, Japan Aerospace Exploration Agency, 2-1-1, Sengen, Tsukuba, Ibaraki 305-8505, Japan

2013-96: PERFORMANCE CHARACTERISTICS OF HIGH-POWER, HIGH SPECIFIC-IMPULSE HALL THRUSTERS FOR JAPANESE IN-SPACE PROPULSION; Yohei Mito, Masato Nishida, Taisuke Kagota, Tsuyoshi Kawamura, Tomoyuki Ikeda, and Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-ku, Osaka 535-8585, Japan

2013-97: RESEARCH AND DEVELOPMENT OF ELECTROTHERMAL PULSED PLASMA THRUSTER SYSTEMS ONBOARD OSAKA INSTITUTE OF TECHNOLOGY PROITERES NANO-SATELLITES; Shuya Kisaki, Rikio Muraoka, Chen Huanjun, Masato Tanaka, and Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-Ku, Osaka 535-8585, Japan, Takashi Wakizono, High Serve, 780-7, Tomehara, Akiruno, Tokyo 190-0152, Japan

2013-98: THREE-DIMENSIONAL HYBRID-PIC SIMULATION OF MICROWAVE NEUTRALIZER; K. Kubota, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan; H. Watanabe and I. Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 252-5210, Japan; N. Yamamoto and H. Nakashima, Kyushu University, Kasuga, Fukuoka, 816-8580, Japan; and T. Miyasaka, Gifu University, Gifu, Gifu, 501-1193, Japan

2013-99: FLOWFIELD SIMULATION AND PERFORMANCE MEASUREMENT OF ELECTROTHERMAL PULSED PLASMA THRUSTERS ONBOARD OSAKA INSTITUTE OF TECHNOLOGY PROITERES NANO-SATELLITE SERIES; Masato Tanaka, Rikio Muraoka, Shuya Kisaki, Chen Huanjun, and Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-Ku, Osaka 535*8585, Japan, Takashi Wakizono, High Serve, 780-7, Tomehara, Akiruno, Tokyo 190-0152, Japan

2013-100: R&D, LAUNCH AND INITIAL OPERATION OF THE OSAKA INSTITUTE OF TECHNOLOGY 1ST PROITERES NANO-SATELLITE WITH ELECTROTHERMAL PULSED PLASMA THRUSTERS AND DEVELOPMENT OF THE 2ND SATELLITE; Naoki Egami, Takaaki Matsuoka, Masaaki Sakamoto, Yoichi Inoue, Tomoyuki Ikeda, and Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-Ku, Osaka 535-8585, Japan

2013-101: RESEARCH AND DEVELOPMENT OF HALL THRUSTER SERIES AT OSAKA INSTITUTE OF TECHNOLOGY; Masato Nishida, Yohei Mito, Taisuke Kagota, Tsuyoshi Kawamura, Tomoyuki Ikeda, and Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-Ku, Osaka 535-8585, Japan

2013-102: PERFORMANCE PREDICTION OF ELECTROTHERMAL PULSED PLASMA THRUST SYSTEMS ONBOARD OSAKA INSTITUTE OF TECHNOLOGY PROITERES NANO-SATELLITE SERIES; Chen Huanjun, Rikio Muraoka, Shuya Kisaki, Masato Tanaka, and Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-Ku, Osaka 535-8585, Japan, Takashi Wakizono, High Serve, 780-7, Tomehara, Akiruno, Tokyo 190-0152, Japan

2013-103: RESEARCH AND DEVELOPMENT OF OSAKA INSTITUTE OF TECHNOLOGY PROITERES NANO-SATELLITE SERIES WITH ELECTRIC ROCKET ENGINES; Rikio Muraoka, Shuya Kisaki, Chen Huanjun, Masato Tanaka, and hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-Ku, Osaka 535-8585, Japan; Takashi Wakizono, High Serve, 780-7, Tomehara, Akiruno, Tokyo 190-0152, Japan

2013-104: THE ISS SPACE PLASMA LABORATORY: A PROPOSED ELECTRIC PROPULSION ON-ORBIT WORKBENCH; Edgar A. Bering, III, and Gregg Edeen, University of Houston, Houston, Texas, 77204-5005; Spiro K. Antiochos, C. Richard DeVore, and Barbara J. Thompson, NASA/Goddard Space Flight Center, Greenbelt, Maryland, 20771; Mark Carter, Matthew Giambusso, Chris Olsen, and Jared Squire, Ad Astra Rocket Company, Webster, Texas, 77598; Davin Larson and James P. McFadden, University of California Berkeley, California, 94720; Benjamin Longmier, University of Michigan, Ann Arbor, Michigan, 48109; and David M. Smith, University of California, Santa Cruz, California, 95064

2013-105: FULL KINETIC ANALYSIS OF SMALL-SCALE MAGNETO PLASMA SAIL IN MAGNETIZED SOLAR WIND; Yasumasa Ashida, Kyoto University, Kyoto, 611-0011, Japan, Ikkoh Funaki, Japan Aerospace Exploration Agency, Kanagawa, 252-5210, Japan, Hiroshi Yamakawa, Kyoto University, Kyoto, 611-0011, Japan, Yoshihiro Kajimura, Akashi National College of Technology, Hyogo, 674-8501, Japan

2013-106: NEUTRAL PRESSURE MEASUREMENT IN AN ION THRUSTER DISCHARGE CHAMBER; Yoshinori Nakayama and Keninchi Narisawa, Department of Aerospace Engineering, National Defense Academy of Japan, 1-10-20, Hashirimizu, Tokosuka, Kanagawa 239-8686, Japan

2013-107: EXPERIMENTAL VISUALIZATION OF ION THRUSTER NEUTRALIZATION PHENOMENA; Futoshi Tanaka and Yoshinori Nakayama, National Defense Academy of Japan, Yokosuka, Kanagawa, 239-8686, Japan

2013-108: FLIGHT DEMONSTRATION AND APPLICATION OF ELECTRIC PROPULSION AT CAST; Chen Jian, Shen Yan, Hu Yanlin, Gao Jun, Beijing Institute of Control Engineering, Beijing, 100190, China

2013-109: DEVELOPMENT OF LOW-POWER CYLINDRICAL TYPE HALL THRUSTERS FOR NANO SATELLITE; Tomoyuki Ikeda, Yohei Mito, Masato Nishida, Taisuke Kagota, Tsuyoshi kawamura, and Hirokazu Tahara, Osaka Institute of Technology, Asahi-ku, Osaka, 535-858, Japan

2013-110: INVESTIGATION OF SIDE BY SIDE HALL THRUSTER SYSTEM; Takeshi Miyasaka and Katsuo Asato, Ryosuke Muraki, Daiki Furuta, and Kei Kubota, Gifu University, Gifu, 501-1193, Japan

2013-111: THEORETICAL MODEL OF A LANTHANUM HEXABORIDE HOLLOW CATHODE; Daniela Pedrini, University of Pisa, Pisa, 56126, Itlay, Riccardo Albertoni, Alta SpA, Ospedaletto, Pisa, 56121, Italy, Fabrizio Paganucci, University of Pisa, Pisa, 56126, Italy, and Mariano Andrenucci, Alta SpA, Ospedaletto, Pisa, 56121, Italy

2013-112: EXPERIMENTAL STUDY ON ELECTRODELESS ELECTROMAGNETIC ACCELERATION IN HELICON PLASMA THRUSTER; D. Kuwahara, S. Waseda, H. Ishii, N. Teshigahara, H. Fujitsuka, T. Ishii, S. Otsuka, T. Nakagawa, and S. Shinohara, Tokyo University of Agriculture and Technology, Koganei, Tokyo, 184-8588, Japan

2013-114: DEVELOPMENT AND QUALIFICATION STATUS OF THE ELECTRIC PROPULSION SYSTEM FOR THE BEPICOLOMBO MISSION; H. L. Gray, Astrium Ltd, Portsmouth, Hants, PO3 5PU, UK, O. Sutherland, European Space Agency, Noordwijk, 2200AG, The Netherlands

2013-115: GEOMETRIC EFFECTS ON THE ACCELERATION MECHANISMA IN APPLIED-FIELD MAGNETOPLASMADYNAMIC THRUSTERS; Meng-Di Kong and Hai-Bin Tang, Beihang University, Beijing, 100191, China

2013-119: REAL-TIME BORON NITRIDE EROSION MEASUREMENTS OF THE HIVHAC THRUSTER VIA CAVITY RING-DOWN SPECTROSCOPY; Brian C. Lee and Azer P. Yalin, Colorado State University, Fort Collins, CO, 80523, USA, Alec Gallimore, University of Michigan, Ann Arbor, MI, 48109, USA, Wensheng Huang and Hani Kamhawi, NASA Glenn Research Center, Cleveland, OH, 44135, USA

2013-120: EMI TESTS OF THE HEMP THRUSTER PROPULSION SYSTEM; Edward J. Beiting, William A. Cox, Kevin D. Diamant, Jason A. Young, and Rostislav Spektor, The Aerospace Corporation, Los Angeles, CA 90009, USA, Stefan Weis and Benjamin van Reijen, Thales Electronic Systems GmbH, 89077 Ulm, Germany, Klaus Ruf, Deutsches Zentrum für Luft-und Raumfahrt e. V. (DLR), D-53227 Bonn, Germany

2013-121: STATUS OF NASA’S EVOLUTIONARY XENON THRUSTER (NEXT) LONG-DURATION TEST AS OF 50,000 H AND 900 KG THROUGHOUT; Rohit Shastry, Daniel A. Herman, George C. Soulas, and Michael J. Patterson, NASA Glenn Research Center, Cleveland, OH, 44135, USA

2013-122: LANGMUIR PROBE MEASUREMENTS WITHIN THE DISCHARGE CHANNEL OF THE 20-KW NASA-300M AND NASA-300MS HALL THRUSTERS; Rohit Shastry, Wensheng Huang, Thomas W. Haag, and Hani Kamhawi, NASA Glenn Research Center, Cleveland, OH, 44135, USA

2013-123: AN EXPERIMENTAL STUDY OF PLASMA DETACHMENT FROM A MAGNETIC NOZZLE IN THE PLUME OF THE VASIMR ENGINE; Christopher S. Olsen, Maxwell G. Ballenger, Mark D. Carter, Franklin R. Chang Díaz, Matthew Giambusso, Timothy W. Glover, Andrew V. Ilin, and Jared P. Squire, Ad Astra Rocket Company, Webster, TX, 77598, USA; Benjamin W. Longmier, University of Michigan, Department of Aerospace Engineering, Ann Arbor, Michigan, 48109, USA; Edgar A. Bering III, University of Houston, Department of Physics and ECE, Houston, Texas, 77204, USA; and Paul A. Cloutier, Rice University, Department of Physics and Astronomy, Houston, Texas, 77005, USA

2013-124: SOLAR ELECTRIC PROPULSION FOR DISCOVERY CLASS MISSIONS; David Y. Oh, John Steven Snyder, Dan M. Goebel, Richard R. Hofer, Damon F. Landau, and Thomas M. Randolph, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109, USA

2013-125: PLASMA TRANSPORT IN A CONVERGING MAGNETIC FIELD WITH APPLICATIONS TO HELICON PLASMA THRUSTERS; Justin M. Little and Edgar Y. Choueiri, Princeton University, Princeton, New Jersey, 08450, USA

2013-126: STRATEGY OF MULTISCALE MODELLING FOR COMBINED THRUSTER-PLUME MODELS; O. Kalentev, J. Duras, K. F. Lüskow, K. Matyash, and R. Schneider, Ernst-Moritz-Arndt, Universität Greifswald, D-17489, Germany

2013-127: DESIGN AND FABRICATION OF THE THRUSTER HEADS FOR THE MICROTHRUST MEMS ELECTROSPRAY PROPULSION SYSTEM; Simon Dandavino, Caglar Ataman, Subha Chakraborty, and Herbert Shea, Ecole Polytechnique Federale de Lausanne (EPEL), Neuchatel, 2000, Switzerland, Charles Ryan and John Stark, Queen Mary University London, London, E1 4NS, United Kingdom

2013-128: CONCEPTS FOR MICRO-THRUSTERS BASED ON SOLID STATE ION CONDUCTORS; Niklas Wolf and Stefan Kolling, THM University of Applied Sciences, Wiesenstrasse 14, DE-35390 Giessen, Germany; Jürgen Janek, Institute of Physical Chemistry, Justus Liebig University, Heinrich-Buff-Ring 58, DE-35392 Giessen, Germany

2013-129: THRUST MEASUREMENTS ON THE T6 HOLLOW CATHODE THRUSTER USING DIRECT THRUST BALANCES; D. Frollani, University of Southampton, Southampton, SO17 1BJ, UK, M. Coletti, Mars Space Ltd, Southampton, SO14 5FE, UK, and S. B. Gabriel, University of Southampton, Southampton, SO17 1BJ, UK

2013-130: EXB PROBE INVESTIGATION OF THE PEGASES THRUSTER ION BEAM IN XE AND SF6; D. Gerst, D. Renaud, and S. Mazouffre, ICARE – CNRS, 45071 Orleans, France, P. Chabert and A. Aanesland, LPP, Ecole Polytechnique, Palaiseau, France

2013-133: BEPICOLOMBO ELECTRIC PROPULSION THRUSTER AND HIGH POWER ELECTRONICS COUPLING TEST PERFORMANCES; Stephen D. Clark and Mark S. Hutchins, QinetiQ, Cody Technology Park, Farnborough, GU14 0LX, UK, Ismat Rudwan and Neil C. Wallace, Mars-Space Ltd, Southampton, Hampshire, SO14 5FE, UK, Javier Palencia, EADS Astrium CRISA, C/. Tores Quevedo, 9(P.T.M.), 28760 Tres Cantos, Madrid, Spain, Howard Gray, Astrium, Anchorage Road, Portsmouth, Hampshire P03 5PU, UK

2013-137: PRELIMINARY CHARACTERIZATION OF A LAB6 HOLLOW CATHODE FOR LOW-POWER HALL EFFECT THRUSTERS; R. Albertoni and M. Andrenucci, Alta SpA, Ospedaletto, Pisa, 56121, Italy; D. Pedrini and F. Paganucci, University of Pisa, Pisa, 56126, Italy

2013-139: 2D FLUID MODEL OF A MAGNETIZED PLASMA IN A CLOSED CHAMBER; P.-Q. Elias, ONERA – the French Aerospace Lab, Palaiseau, 91123, France

2013-140: HT100D PERFORMANCE EVALUATION AND ENDURANCE TEST RESULTS; Ducci C., Oslyak S., Dignani D., Albertoni R., and Andrenucci M., Alta SpA, Pisa 56121, Italy

2013-141: INVESTIGATION OF THE EMISSION BEHAVIOR OF MINIATURIZED SU-8 BASED COLLOID EMITTERS; K. Huhn, M. Piechotka, T. Henning, and P. J. Klar, Institute of Experimental Physics I, Justus Liebig University, DE-35392 Giessen, Germany

2013-142: NUMERICAL SIMULATIONS OF THE PARTIALLY-IONIZED GAS IN A 100-A LAB6 HOLLOW CATHODE; Ioannis G. Mikellides, Dan M. Goebel, Benjamin A. Jorns, James E. Polk, and Pablo Guerrero, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109

2013-143: AZIMUTHAL SPOKE PROPAGATION IN HALL EFFECT THRUSTERS; Michael J. Sekerak, Benjamin W. Longmier, and Alec D. Gallimore, University of Michigan, Ann Arbor, MI, 48109, Daniel L. Brown, U.S. Air Force Research Laboratory, Edwards Air Force Base, California 93524, Richard R. Hofer and James E. Polk, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2013-144: SGEO ELECTRIC PROPULSION SUBSYSTEM DEVELOPMENT STATUS AND FUTURE OPPORTUNITIES; Marco De Tata, Pierre-Etienne Frigot, Stefan Beekmans, Hendrik Lubberstedt, and Dieter Birrecl, OHB System AG, Bremen, 28359, Germany, Alain Demaire, Peter Rathsman, and Ekaterina Rezugina, OHB Sweden AB, Solna, SE-171 04, Sweden, Niccola Kutufa, ESA-ESTEC, Noordwijk, The Netherlands

2013-145: MAGNETOHYDRODYNAMICS AND PARTICLE-IN-CELL CODES SIMULATION OF PLASMA PROCESSES IN MICRO HEMP-THRUSTERS; Tim Brandt, Frank Jensen, Rodion Groll, and Claus Braxmaier, DLR, Institute of Space Systems, Robert-Hooke Str. 7, 28359 Bremen, Germany, ZARM, University of Bremen, Am Fallturm, 28359 Bremen Germany, Ulrich Johann and Andreas Keller, Astrium GmbH, Claude-Dornierstrabe 1, 88090 Immenstaad, Germany, Justus-Liebig-University Gieben, I. Physikalisches Institut

2013-146: EXPERIMENTAL PROGRESS TOWARDS THE MICROTHRUST EMEMS ELECTROSPRAY ELECTRIC PROPULSION SYSTEM; C. Ryan, A Daykin-Iliopoulos, and J. Stark, Queen Mary University of London, London, E1 4NS, United Kingdom; A. Z. Salaverri, E. Vargas and P. Rangsten, SSC NanoSpace, Uppsala Science Park, SE-751 83, Uppsala, Sweden; S. Dandavino, C. Ataman, S. Chakraborty, D. Courtney, and H. Shea, Ecole Polytechnique Férérale de Lausanne (EPFL), Neuchatel, 2000, Switzerland

2013-147: INVESTIGATIONS ON THE FLOWING PULSED PLASMA OF A 20J PULSED PLASMA THRUSTER; Zun Zhang and Haibin Tang, Beihang University, Beijing, 100191, China

2013-148: PHYSICS OF HALL-EFFECT DISCHARGE BY PARTICLE; F. Taccogna, P. Minelli, and N. Oudini, Istituto di Metodologie Inorganiche e di Plasmi – CNR, via Amendola 122/D, 70126 Bari, Italy

2013-149: VASIMR SPACEFLIGHT ENGINE SYSTEM MASS STUDY AND SCALING WITH POWER; Jared P. Squire, Mark D. Carter, Franklin R. Chang Diaz, Matthew Giambusso, Timothy W. Glover, Andrew V. Ilin, Jorge Oguilve-Araya, and Christopher S. Olsen, Ad Astra Rocket Company, Webster, Texas 77598, USA, Edgar A. Bering III, University of Houston, Houston, Texas 77204, USA, and Benjamin W. Longmier, University of Michigan, Ann Arbor, MI 48109, USA

2013-150: MODELING MAGNETIC NOZZLE EFFECTS IN DIFFERENT PLASMA RADII WITH AN AXISYMMETRIC PARTICLE-IN-CELL METHOD; Min Li and Hai-bin Tang, Beihang University, Beijing, 100191, China

2013-153: LOW POWER RADIO-FREQUENCY PLASMA THRUSTER DEVELOPMENT AND TESTING; F. Trezzolani, A. Lucca Fabris, and D. Pavarin, University of Padova, Italy, A. Selmo, RESIA, Albaredo d’Adige, Italy, A. I. Tsaglov, A. V. Loyan, and O. P. Rubalov, National Aerospace University ‘Kharkiv Aviation Institute (KhAI)’, Ukraine, M. Manente, HIT09 s.r.l., Padova, Italy

2013-155: THRUST BALANCE CHARACTERIZATION OF A 200W QUAD CONFINEMENT THRUSTER FOR HIGH THRUST REGIMES; Aaron Knoll, Dimitrios Lamprou, and Vaios Lappas, University of Surrey, Guildford, Surrey, GU2 7XH, United Kingdom; Mark Pollard, Surrey Satellite Technology Ltd., Stephenson Road, Surrey Research Park, Guildford, GU2 7YE, United Kingdom; Paolo Bianco, Astrium Ltd., Anchorage Road, Portsmough, Hampshire, PO3 5PU, United Kingdom

2013-157: THE IMPACT OF BACK-SPUTTERED CARBON ON THE ACCELERATOR GRID WEAR RATES OF THE NEXT AND NSTAR ION THRUSTERS; George C. Soulas, NASA Glenn Research Center, Cleveland, OH, 44135, USA

2013-158: CHARACTERIZATION OF ERODED BORON ATOMS IN THE PLUME OF A HALL THRUSTER; Horatiu C. Dragnea and Iain D. Boyd, University of Michigan, Ann Arbor, MI, 48109, USA, Brian C. Lee and Azer P. Yalin, Colorado State University, For Collins, CO, 80523, USA

2013-159: PLASMA ADIABATICITY IN A DIVERGING MAGNETIC NOZZLE; J. P. Sheehan and Benjamin W. Longmier, University of Michigan, Ann Arbor, MI, 48103, USA; Edgar A. Bering, University of Houston, Houston, TX, 77204, USA; Christopher S. Olsen, Jared P. Squire, Mark D. Carter, Franklin R. Chang Díaz, Timothy W. Glover, and Andrew V. Ilin, Ad Astra Rocket Company, Webster, TX, 77598, USA; Leonard D. Cassady, Jacobs Engineering, Bingham Farms, MI, 48025, USA

2013-160: EXPERIMENTAL INVESTIGATION OF THRUST CHARACTERISTICS OF MAGNETOPLASMA SAIL; Yuya Oshio, Kazuma Ueno, and Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, kanagawa, 252-5210, Japan

2013-161: THE RELIABILITY EVALUATION OF LHC-5 HOLLOW CATHODE HEATER; Jia Yanhui, Guo Ning, Chen Juanjuan, Zhang Tianping, Yang Wei, Liang Kai, Sun Yunkui, Geng Hai, and Tian Huabing, Lanzhou Institute of Physics, Lanzhou, GanSu,730000, China

2013-162: PIC/MCC SIMULATION COMPUTATIONAL MODELING OF A ION THRUSTER DISCHARGE CHAMBER; Chen Juanjuan, Zhang Tianping, Liu Mingzheng, and Jia Yanhui, Lanzhou Institute of Physics, Lanzhou 73000, China

2013-163: HELICON PLASMA THRUSTER EXPERIMENT CONTROLLING CROSS-FIELD DIFFUSION WITHIN A MAGNETIC NOZZLE; K. Takahashi, Department of Electrical Engineering, Tohoku University, Sendai, 980-8579, Japan, C. Charles and R. W. Bowell, Space Plasma Power and Propulsion Laboratory, Research School of Physics and Engineering, The Australian National University, Canberra ACT 0200, Australia, A. Ando, Department of Electrical Engineering, Tohoku University, Sendai, 980-8579, Japan

2013-164: PPTCUP LIFETIME TEST RESULTS; S. Ciaralli, University of Southampton, Southampton, UK, SO17 1BJ, M. Coletti and F. Guarducci, Mars Space Ltd. Southampton, UK, SO14 5FE, and S. B. Gabriel, University of Southampton, Southampton, UK, SO17 1BJ

2013-165: µ-PPTS DIAGNOSTICS: A HIGH ACCURACY IMPULSIVE THRUST BALANCE; S. Ciaralli, University of Southampton, Southampton, UK, SO17 1BJ, M. Coletti, Mars Space Ltd, Southampton, UK, SO14 5FE, and S. B. Gabriel, University of Southampton, Southampton, UK, SO17 1BJ

2013-166: STUDY ON THE INFECTIONS OF MAGNETIC FIELD IN LHT-100 THRUSTER; Jianfei Long, Tianping Zhang, and Mingming Sun, Lanzhou Institute of Physics, Lanzhou, GanSu, 730000, China

2013-167: NUMERICAL INVESTIGATION OF THE INFLUENCE OF AMBIPOLAR ELECTRIC FIELD ON MAGNETIC NOZZLE DETACHMENT; Yujie Xu and Haibin Tang, School of Astronautics, Beihang Unversity, Beijing 100191, China

2013-171: PARTICLE-IN-CELL SIMULATIONS FOR A VARIABLE MAGNET LENGTH CUSPED-FIELD THRUSTER; Yinjian Zhao, Hui Liu, Daren Yu, and Chengyu Ma, Institute of Advanced Power, Harbin Institute of Technology, Harbin, Heilongjiang Province, 150001, China

2013-172: LIFETIME ASSESSMENT OF HALL THRUSTER; Hu Yanlin, Chen Jian, Mao Wei, Shen Yan, and Chen Jun, Beijing Institute of Control Engineering, Beijing, 100190, China

2013-175: GRADIENT DRIFT INSTABILITY IN HALL PLASMA DEVICES; W. Frias and A.I. Smolyakov, University of Saskatchewan, Saskatoon, SK, S7N 5E2, Canada; Y. Raitses and I. D. Kaganovich, Princeton Plasma Physics Laboratory, Princeton University, Princeton, NJ, 08543, USA

2013-176: DRIVING LOW FREQUENCY AZIMUTHAL MODE IN CYLINDRICAL HALL THRUSTER WITH A SEGMENTED ANODE; Yuan Shi, Scott Keller, Yevgeny Raitses, and Ahmed Diallo, Princeton Plasma Physics Laboratory, Princeton, New Jersey 08543, USA

2013-177: INFLUENCE OF CATHODE SHAPE ON VACUUM ARC THRUSTER PERFORMANCE AND OPERATION; Jonathan Lun, University of the Witwatersrand, Johannesburg, Gauteng, 2000, South Africa, South African National Space Agency: Space Science, Hermanus, Western Cape, 7200, South Africa, Craig Law, University of Witwatersrand, Johannesburg, Gauteng, 2000, South Africa

2013-178: DEVELOPMENT OF A HALL THRUSTER FULLY KINETIC SIMULATION MODEL USING ARTIFICAL ELECTRON MASS; Shinatora Cho, Japan Aerospace Exploration Agency, Tokyo, 182-8522, Japan, Kimmiya Komurasaki and Yoshihiro Arakawa, The University of Tokyo, Tokyo, 113-8656, Japan

2013-179: 6-DOF FLIGHT DYNAMICS OF LASER-BOOSTED VEHICLE DRIVEN BY BLAST WAVE; Masayuki Takahashi and Naofumi Ohnishu, Tohoku University, Sendai, Miyagi, 980-8579, Japan

2013-181: IMPULSE VECTOR CHARACTERISTICS OF A LASER ABLATION PROPULSION SYSTEM; Takumi Oyama, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan, Hideyuki Horisawa, Yuji Oigawa, and Keiji Hagiwara

2013-182: NUMERICAL STUDY ON THE OPERATIN LIMITS OF MPD THRUSTERS; Arsad Quraishi and M. Mahendhran, Indian Institute of Technology Madras, Chennai-600036, India, Amit Kumar, Indian Institute of Technology Madras, Chennaii-600036, India

2013-186: THREE-DIMENSIONAL PARTICLE-IN-CELL SIMULATION OF A MINIATURE MICROWAVE DISCHARGE ION THRUSTER µ1; Yoshinori Takao, Koji Eriguchi, and Kouichi Ono, Kyoto University, Kyoto, 615-8540, Japan, Yuto Sugita, Shizuoka University, Shizuoka, 422-8529, Japan, Hiroyuki Koizumi and Kimiya Komurasaki, The University of Tokyo, Tokyo, 113-8636, Japan

2013-187: LANGMUIR PROBE MEASUREMENTS OF A MAGNETOPLASMADYNAMIC THRUSTER; Yang Li, Hai-Bin Tang, Zun Zhang, and Yuan Yang, Beihang University, Beijing, 100191, China

2013-188: MEASUREMENT OF THE DIELECTRIC WALL EROSION IN HELICON PLASMA THRUSTERS: AN APPLICATION TO THE VASIMR VX-CR EXPERIMENT; Juan Del Valle, Jose A. Castro, Norberto Arce, Erick Chinchilla, Estaban Echeverría, Daniel Lexama, Carlos Martínez, Jorge Oguilve, Allan Rivera, Max Rodríguez, Juan Valverde, and Rónold Chang Díaz, Ad Astra Rocket Company, Liberia, Guanacaste, Costa Rica, Christopher S. Olsen, Andrew V. Ilin, Matthew Giambusso, Mark D. Carter, Jared P. Squire, and Franklin R. Chang Díaz, Ad Astra Rocket Company, Webster, Texas, USA

2013-190: A SIMPLE COLLISIONAL-RADIATIVE MODEL APPLICABLE TO ARGON ARCJET; Su-Rong Sun and Hai-Xing Wang, School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing, 100191, China

2013-191: EMITTANCE MEASUREMENT SETUP FACILITATING PLASMA DIAGNOSTIC OF ION THRUSTERS; K. Holste, S. Schippers, and A. Müller, Justus-Liebig Universität Gießen, 35392, Germany, P. Spädtke, GSI Darmstadt, Planckstraße 1, 64291 Darmstadt, Germany, M. Smirnova, Justus-Liebig Universität Gießen, I. Physikalisches Institut, Heinrich-Buff-Ring 16, 35392 Gießen, Germany, D. Feili, Astronautics Research Group, Southampton S017 1BJ, United Kingdom

2013-192: CREW WASTE WATER ELECTRIC PROPULSION SYSTEM DEVELOPMENT AND SMALL SATELLITE DEPLOYMENT FROM ISS WITH ITS ARCJET THRUSTER; Yuichiro Nogawa, Earth-Track Corporation, Tokyo, Japan; Hirokazu Tahara, Osaka Institute of Technology, Osaka, Japan, and Akira Tsuchida, Earth-Track Corporation, Tokyo, Japan

2013-193: CHARACTERISTICS OF HIGH-REPETITION RATE OPERATION OF A LASER-ASSISTED PULSED PLASMA THRUSTER; Mizuki Karima, Hideyuki Horisawa, and Yuki Oigawa, Dept. Aeronautics and Astronautics, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan

2013-194: NUMERICAL SIMULATIONS OF A MINIATURE MICROWAVE ION THRUSTER; Pierre-Yves C. R. Taunay, Sven G. Bilén, and Michael M. Micci, The Pennsylvania State University University Park, PA 16802, USA

2013-196: EXAMINATION OF THE EXTERNAL MAGNETIC FIELD GENERATED BY A RADIO-FREQUENCY ION THRUSTER (RIT); Timo Baruth and Rainer Thueringer, Technische Hochschule Mittelhessen University of Applied Sciences, Giessen, 35390, Germany

2013-198: PPT DEVELOPMENT FOR NANOSATELLITES APPLICATIONS: EXPERIMENTAL RESULTS; M. Coletti, Mars Space Ltd, Southampton, SO14 5FE, UK, S. Ciaralli and S. B. Gabriel, University of Southampton, Southampton, SO17 1BJ, UK

2013-199: A PLAN TO STUDY THE RADIATED EMISSIONS FROM A VASIMR ENGINE EXHAUST PLUME; Matthew Giambusso, Edgar A. Bering, III, Gregg A. Edeen, University of Houston, Houston, Texas, 77294, USA, Mark D. Carter, Christopher S. Olsen, and Jared P. Squire, Ad Astra Rocket Company, Webster, Texas, 77598, USA

2013-201: MAGNETICALLY SHIELDED MINIATURE HALL THRUSTER: DEVELOPMENT AND INITIAL TESTING; Ryan W. Conversano, University of California Los Angeles, Los Angeles, CA, 90095, USA, Dan M. Goebel and Richard R. Hofer, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 991109, Taylor S. Matlock and Richard E. Wirz, University of California Los Angeles, Los Angeles, CA, 90095, USA

2013-202: VASIMR VX-CR EXPERIMENT: STATUS, DIAGNOSTICS AND PLASMA PLUME CHARACTERIZATION; Jose A. Castro Nieto, Juan Del Valle, Carlos Martínez, Allan Rivera, and Jorge Oguilve, Ad Astra Rocket Company, Liberia, Guanacaste, Costa Rica, Christopher S. Olsen, Matthew Giambusso, Mark d. Carter, Jared P. Squire, and Franklin R. Chang Díaz, Ad Astra Rocket Company, Webster, Texas, USA

2013-205: RESONANT MODE TRANSITION IN THE RF-CONTROLLED HOLLOW CATHODE; Matthew L. Plasek, Christopher J. Wordingham, Edgar Y. Choueiri, Princeton University, Princeton, NJ, 08544, USA

2013-209: EXPERIMENT RESEARCH ON A VARIABLE MAGNET LENGTH CUSPED FIELD THRUSTER; Chengyu Ma, Hui Liu, Daren Yu, Yinjian Zhao, Pengbo Chen, and Guoshun Sun, Institute of Advanced Power, Harbin Institute of Technology, Harbin, Heilongjiang Province, 150001, China

2013-210: NUMERICAL STUDY OF LISSAJOUS ACCELERATION FOR ELECTRODELSS PLASMA THRUSTER; Ryosuke Nomura and Naofumi Ohnishi, Tohoku University, Sendai, Miyagi, 980-8579, Japan; Takahiro Nakamura and Hiroyuki Nishida, Tokyo University of Agriculture and Technology, Koganei, Tokyo, 184-8588, Japan

2013-211: THE 250MN THRUST BALANCE FOR THE DLR GOETTINGEN EP TEST FACILITY; Andreas Neumann and Julian Sinske, German Aerospace Center DLR, Goettingen, Germany and Hans-Peter Harmann, AST Advanced Space Technologies GmbH, Stuhr, Germany

2013-212: TWO-DIMENSIONAL SIMULATIONS OF COHERENT FLUCTUATION-DRIVEN TRANSPORT IN A HALL THRUSTER; Cheryl M. Lam and Mark A. Cappelli, Stanfod Plasma Physics Laboratory, Stanford University, Stanford, CA 94305, USA; Eduardo Fernandez, Department of Mathematics and Physics, Eckerd College, St. Petersburg, FL, 33711, USA

2013-213: POWER PROCESSING UNIT ACTIVITIES AT THALES ALENIA SPACE BELGIUM (ETCA); Eric Bourguignon, Stéphane Fraselle, and Thierry Scalais, Thales Alenia Space Belgium (ETCA), B-6032 Charleroi, Belgium

2013-214: TIME-AVERAGED AND TIME-VARYING PLASMA POTENTIAL IN THE NEAR-FIELD PLUME OF A HALL THRUSTER; A. Petin and S. Mazouffre, ICARE, CNRS, 1c Avenue de la recherché scientifique, 45071 Orleans, France, K. Dannenmayer, ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, Netherlands, P. Kudrna and M. Tichyu, Charles University, Faculty of Mathematics and Phuysics, Prague, Czech Repulic

2013-216: IMPLEMENTATION OF AN ENTROPY CLOSURE MODEL FOR TWO-DIMENSIONAL HYBRID HALL THRUSTER SIMULATIONS; Eunsun Cha and Mark A. Cappelli, Stanford University, Stanford, CA, 94305, USA, and Eduardo Fernandez, Eckerd College, St. Petersburg, FL, 33711, USA

2013-217: SMALL ELECTRIC PROPULSION PLATFORM FOR ACTIVE SPACE DEBRIS REMOVAL; A. Ruggiero, P. Pergola, and M. Andrenucci, Alta, Pisa, 56100, Italy

2013-219: DEVELOPMENT AND TEST OF XR-150, A NEW HIGH-THRUST 100 W RESISTOJET; A. Passaro, Alta S.p.A., Pisa, 56121, Italy, A. Bulit, ESA-ESTEC, Noordwijk, 2201 AZ, The Netherlands

2013-222: ELECTRIC PROPULSION THRUSTER ASSEMBLY FOR SMALL GEO: END-TO-END TESTING AND FINAL DELIVERY; Olivier Duchemin, Vaitua Leroi, Michael Oberg, and David Le Mehaute, Snecma, Safran Group, Space Engines Division, 27208 Vernon, France, Ramon Perez Vara, IberEspacio, Magallanes 3, 4a Planta, 28015 Madrid, Spain, Alain Demaire, Mikael Bjorklund and Staffan Persson, OHB-Sweden AB, SE-17122 Solna, Sweden, Marco De Tata and Stefan Beekmans, OHB-System AG, 28359 Bremen, Germany, Niccola Kutufa, ESA/ESTEC, Keplerlaan 1, Postbus 299, 2200 AG Noordwijk, The Netherlands

2013-223: MICROWAVE-PLASMA INTERACTION IN A MINIATURE PLASMA ION THRUSTER; Indranuh Dey, Yuji Toyoda, Naoji Yamamoto, and Hideki Nakashima, Department of Advanced Energy Engineering Science, Kyushu University, Kasuga, 816-8580, Japan

2013-224: COMPUTATIONAL MODELING OF A HIGH POWER PLASMA SOURCE FOR MATERIAL INTERACTION EXPERIMENTS; Christopher A. Dodson, Richard E. Wirz, and Taylor S. Matlock, University of California, Los Angeles, CA, 90095

2013-227: µFCU – A MINIATURIZED FLOW CONTROL UNIT FOR XENON; H. –P. Harmann, S. Rothaus, and G. Wanot, AST Advanced Space Technologies GmbH, D-28816 Stuhr, Germany

2013-228: µFCU – RESULTS OF A PREQUALIFICATION TEST CAMPAIGN; S. Rothaus, H. –P. Harmann, and T. Kopp, AST Advanced Space Technologies GmbH, D-28816 Stuhr, Germany

2013-234: EXPERIMENTAL STUDY OF A 1-MW-CLASS QUASI-STEADY-STATE SELF-FIELD MAGNETOPLASMADYNAMIC THRUSTER; Kenji Miyazaki and Syunm Takenaka, Tokai University, Hiratsuka, Kanagawa 259-1292, Japan, Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, kanagawa 252-5210, Japan, Hideyuki Horisawa, Tokai University, Hiratsuka, Kanagawa 259-1292, Japan

2013-235: EXPERIMENTAL INVESTIGATIONS OF COMPONENT DETERMINING CAMILA HALL THRUSTER PERFORMANCE; M. Rubanovich, V. Balabanov, A. Kapulkin, and e. Behar, Asher Space Research Institute, Technion-Israel Institute of Technology, Haifa, 32000, Israel

2013-238: DEVELOPMENT OF A 1 KW CLASS THERMAL ARCJET THRUSTER TALOS; Q. H. Le and G. Herdrich, Institute of Space Systems, University of Stuttgart, Stuttgart, 70569, Germany

2013-239: TIME-DEPENDENT ION VELOCITY DISTRIBUTION: A NOVEL HETERODYNE LASER-INDUCED FLUORESCENCE WITH COUPLED WAVE EXCITATION; A Diallo, Y. Shi, S. Keller, and Y. Raitses, Princeton Plasma Physics Laboratory, Princeton, NJ, 08536, USA, S. Mazouffre, ICARE, CNRS, Orléans, France

2013-241: MECHANICAL PROBE AND MODELING EFFORTS FOR EVALUATION OF PLASMA CREATION AND ACCELERATION IN PPT; Tony Schönherr, W. Alexander Zach, and Kimiya Komurasaki, The University of Tokyo, Bunkyo, Tokyo, 113-8656, Japan, Sebastian Hörner and Yoshihiro Arakawa, The University of Tokyo, Kashiwa, Chiba, 277-8561, Japan, Georg Herdrich, University of Stuttgart, Stuttgart, Baden-Württemberg, 70569, Germany

2013-242: DESIGN AND PERFORMANCE EVALUATION OF THRUSTER WITH ANODE LAYER UT-58 FOR HIGH-POWER APPLICATION; Tony Schönherr, Rei Kawashima, Hiroyuki Koizumi, and Kimiya Komurasaki, The University of Tokyo, Bunkyo, Tokyo, 113-8656, Japan, Daiki Fujita and Yuki Ito, The University of Tokyo, Kashiwa, Chiba, 277-8561, Japan

2013-243: APPLICATION OF THE HOLLOW CATHODE TO DC ARCJET; Masahiro Kinoshita, The University of Tokyo, Bunkyo-ku, Tokyo, 113-8656, Japan, Daisuke Nakata, Muroran Institute of Technology, Hokkaido, 050-8585, Japan, Kiyoshi Kinefuchi, Japan Aerospace Exploration Agency, Tsukuba, Ibaragi, 305-8505, Japan, Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 252-5210, Japan

2013-244: DEVELOPMENTS OF ROBUST ANODE-LAYER INTELLILGENT THRUSTER FOR JAPAN IN-SPACE PROPULSION SYSTEM; Naoji Yamamoto, Kyushu University, Kasuga, Fukuoka, 816-8580, Japan, Takeshi Miyasaka, Gifu University, Gifu, Gifu, 501-1193, Japan, Kimiya Komurasaki, Hiroyuki Koizumi, and Tony Schonherr, The University of Tokyo, Tokyo, Tokyo, 113-8656, Japan, Hirokazu Tahara, Osaka Institute of Technology, Osaka, Japan, Haruki Takegahara and Junichiro Aoyagi, Tokyo Metropolitan University, Tokyo, Japan, Masakatsu Nakano, Tokyo Metropolitan College of Industrial Technology, Tokyo, Japan, Ikkoh Funaki, Hiroki Watanabe, and Yasushi Ohkawa, Japan Aerospace Exploration Agency, Japan, Akirai Kakami, University of Miyazaki, Miyazaki, Japan, Yoshiyuki Takao, Nishinippon Institute of Technology, Fukuoka, Japan, Shigeru Yokota, Nagoya University, Nagoya, Japan, Toshiyuki Ozaki and Hiroyuki Osuga, Mitsubishi Electric Corporation, Kamakura, Japan

2013-245: PLASMA DIAGNOSTICS IN A MINIATURE MICROWAVE DISCHARGE ION THRUSTER; Yuto Sugita, Shizuoka University, Shizuoka, 432-8561, Japan, Hiroyuki Koizumi, The University of Tokyo, Tokyo, 113-8656, Japan, Ryudo Tsukizaki and Hitoshi Kuninaka, The Institute of Space and Astronautical Science, Sagamihara, 252-5210, Japan, Yoshinori Takao, Kyoto University, Kyoto, 615-8540, Japan, Yoshiki Yamagiwa and Makoto Matsui, Shizuoka University, ,Shizuoka, 432-8561, Japan

2013-246: STEADY-STATE, APPLIED-FIELD, RECTANGULAR MPD THRUSTERS; Shigeru Yokota, Daisuke Ichihara, Hisashi Kataoka, Shota Harada, and Akihiro Sasoh, Nagoya University, Nagoya, Aichi, 464-8603, Japan

2013-247: INFLUENCE OF ELECTRON AND ION THERMODYNAMICS ON THE MAGNETIC NOZZLE PLASMA ESPANSION; Mario Merino and Eduardo Ahedo, Universidad Carlos III de Mardrid, Avda. de la Universidad 30, 28911 Leganés (Madrid). Spain

2013-248: DEVELOPMENT OF A NOVEL PROCESSING UNIT FOR HALL THRUSTERS; Naoji Yamamoto, Kyushu University, Kasuga, Fukuoka, 816-8580, Japan; Haruki Takegahara, Junichiro Aoyagi, and Kyoichi Kuriki, Tokyo Metropolitan University, 191-0065, Tokyo, Japan; Taichiro Tamida, Mitsubishi Electric Corporation, Hyogo, 661-8661, Japan; and Hiroyuki Osuga, Mitsubishi Electric Corporation, Kamakura, 247-8520, Japan

2013-249: TWO-DIMENSIONAL PARTICLE-IN-CELL MODEL OF THE EXTRACTION REGION OF THE PEGASES ION-ION PLASMA SOURCE; L. Garrigues, G. J. M. Hagelaar, D. Levko, LAPLACE (Laboratoire Plasma et Conversion d’Energie), Universite de Toulouse, UPS, INPT Toulouse, 118, route de Narbonne, F-31062 Toulouse, France, CNRS; LAPLACE; F-31062 Toulouse, France, A. Aanesland, Laboratoire de Physique des Plasmas, CNRS, Ecole Polytechnique, 91128 Palaiseau cedex France

2013-250: DESIGN AND FIRST TEST CAMPAIGN RESULTS WITH A NEW FLEXIBLE MAGNETIC CIRCUIT FOR A HALL THRUSTER; L. Garrigues, LAPLACE (Laboratoire Plasma et Conversion d’Energie), Université de Toulouse, UPS, INPT Toulouse, S. Mazouffre, G. Bourgeois, and J. Vaudolon, ICARE (Institut de Combustion Aérothermique Réactivité et Environnement), C. Hénaux, R. Vilamot, A. Rossi, and D. Harribey, CNRS; LAPLACE; F-31062 Toulouse, France, S. Zurbach, Snecma, Safran Group; 27200 Vernon, France

2013-251: EXPERIMENTAL TEST CAMPAIGN OF GAS-FED STEADY STATE APPLIED-FIELD MAGNETOPLASMADYNAMIC THRUSTER SX3; Adam Boxberger and Georg Herdrich, University of Stuttgart, Institute of Space Systems (IRS), 70569 Stuttgart, Pfaffenwaldring 29, Germany

2013-252: A TWO-DIMENSIONAL (AZIMUTHAL-AXIAL) PARTICLE-IN-CELL OF A HALL THRUSTER; L. Garrigues, LAPLACE (Laboratoire Plasma et Conversion d’Energie). Université de Toulouse, UPS, INPT Toulouse, 118 route de Narbonne, F-31062 Toulouse cedex 9, France; P. Coche LAPLACE (Laboratoire Plasma et Conversion d’Energie). Université de Toulouse, UPS, INPT Toulouse, 118 route de Narbonne, F-31062 Toulouse cedex 9, France, CNRS; LAPLACE, F-31062 Toulouse, France

2013-253: THRUST CHARACTERISTICS OF HELICON PLASMA THRUSTERS; S. Tonooka, The Graduate University for Advanced Studies, Sagamihara, Kanagawa, 252-5210, Japan, S. Iwabuchi, T. Nakamura, S. Shinohara, and H. Nishida, Tokyo University of Agriculture and Technology, Koganei, Tokyo, 184-8588, Japan

2013-254: EFFECTS OF ELECTRIC CHARGE IN CAPACITORS ON PULSED PLASMA THRUSTER PERFORMANCE WITH EXTERNAL MAGNETIC FIELD, Shinya Mori, Takahiro Shindo, Keisuke Tajiri, Yuya Tamugi, Junichiro Aoyagi, and Haruki Takegahara, Tokyo Metropolitan University, Hino, Tokyo, 191-0065, Japan

2013-255: PULSED PLASMA THRUSTER ENDURANCE OPERATION STRESS TESTING IN IRS; M. Lau and G. Herdrich, University of Stuttgart, Institute of Space Systems, Stuttgert, Baden-Württemberg. 70659, USA

2013-257: ELECTRIC PROPULSION IN GERMANY: SYSTEM ACTIVITIES TODAY, INSTITUTIONS INVOLVED, CHALLENGES COMING UP; Norbert Püttmann and Klaus Ruf, German Aerospace center (DLR) – Space Administration, Koenigswinterer Str. 522-524, D-53227 Bonn, Germany

2013-258: MINIATURIZED HV POWER SUPPLLY; Richard Visee, Martin de Jong, and Jan Timmerman, SystematIC design b.v., Delft, 2623CR, the Netherlands

2013-259: THE PEGASES GRIDDED ION-ION THRUSTER PERFORMANCE AND PREDICTIONS; A. Aanesland, D. Rafalskyi, J. Bredin, P. Grondein, N. Oudini, and P. Chabert, Laboratoire de Physique des Plasmas (LPP), CNRS-Ecole Polytechnique, 91128 Palaiseau Cedex, France, L. Garrigues and G. Hagelaar, LAboratoire PLAsma et Conversion d’Energie-LAPLACE, 31062 Toulouse Cedex 9, France

2013-260: CHARACTERISTICS OF A LASER-ELECTROSTATIC HYBRID PROPULSION SYSTEM; Tatsuro Sakai, Akihiro Osamura, and Hideyuki Horisawa, Tokai University, hiratuka, Kanagawa, 259-1292, Japan

2013-261: THE SMALL-SCALE HIGH-FREQUENCY EXB INSTABILITY AND ITS LINKS TO OBSERVED FEATURES OF THE HALL THRUSTER DISCHARGE; ICARE, Electric Propulsion Team, UPR 3021, CNRS, Orléans, France, Cyrille Honore and Dominique Grésillon, LPP, Ecole Polytechnique, UMR 7648 CNRS, Palaiseau, France, Anne Héron, CPHT, Ecole Polytechnique, UMR 7644 CNRS, Palaiseau, France, Nicolas Lemoine and Jordan Cavalier, IJL UMR 7198 CNRS, Nancy, France

2013-262: MHD AND THERMAL SIMULATIONS OF A RADIATION COOLED SELF-FIELD MPD THRUSTER; Akira Kawasaki, Tokyo Institute of Technology, Yokohama, Kanagawa, 252-8502, Japan, Kenichi Kubota, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan, Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 252-5210, Japan, Yoshihiro Okuno, Tokyo Institute of Technology, Tokohama, Kanagawa, 226-8502, Japan

2013-263: CONCEPTUAL DESIGN OF HIGH EFFICIENCY BREECH-FED ABLATIVE PPT IN TOKYO METROPOLITAN UNIVERSITY; Takahiro Shindo, Shinya Mori, Keisuke Tajiri, Yuya Tamugi, Junichiro Aoyagi, and Haruki Takegahara, Tokyo Metropolitan University, Hino, Tokyo, 191-0065, Japan

2013-264: DEVELOPMENT OF VACUUM ARC THRUSTER FOR NANO SATELLITE; Shingo Fuchikami, Masayoshi Nakamoto, Kazuhiro Toyoda, and Mengu Cho, Kyushu Institute of Technology, Kitakyushu, Fukuoka, Japan

2013-265: IMPROVEMENT OF LASER ELECTROMAGNETIC HYBRID THRUSTER; Yuji Oigawa and Hideyuki Horisawa, Tokai University, Kitakaname, Hiratsuka City, Kanagawa, 259-1292, Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2013-266: LOW FREQUENCY OSCILLATION ANALYSIS OF A HALL THRUSTER USING A ONE-DIMENSIONAL HYBRID-DIRECT KINETIC SIMULATION; Kentaro Hara and Iain D. Boyd, University of Michigan, Ann Arbor, MI 48109-2140

2013-268: SENSITIVITY ANALYSIS ON ION ACCELERATION GRID EROSION IN ION THRUSTERS; Hiroki Watanabe, Ikkoh Funaki, and Ryoji Takaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 252-5210, Japan, Masakatsu Nakano, Tokyo Metropolitan College of Industrial Technology, Arakawa-ku, Tokyo, 116-0003, Japan, Yoshihiro Kajimura, Akashi National College of Technology, Akashi, Hyogo, 674-8501, Japan

2013-269: PARAMETRIC STUDY OF HEMP-THRUSTER DOWNSCALING TO µN THRUST LEVELS; Andreas Keller, Franz Georg Hey, Dennis, Weise, and Ulrich Johann, Astrium GmbH – Satellites, Friedrichshafen, Germany, Justus-Liebig-University Gieben, I. Physikalisches Institut, Germany, Peter Kohler, Justus-Liebig-University Gieben, I. Physikalisches Institut, Germany, Marcel Berger, Astrium GmbH – Space Transportation, Bremen, Germany, Claus Braxmaier, Unviersity of Bremen, ZARM Center for Applied Space Technology and Microgravity, DLR German Aerospance Center, Institute of Space Systsems, Bremen, Davar Feilli, University of Southampton, Faculty of Engineering and the Environment, United Kingdom

2013-270: PLASMA DIANOSTICS OF THE µ10 ECR ION THRUSTER USING OPTICAL FIBER PROBES; Ryudo Tsukizaki, Japan Aerospace Exploration Agency, Sagmihara, Kanagawa, 252-5210, Japan, Toshiyuki Ise and Hiroyuki Koizumi, The Universrity of Tokyo, Bunkyo-ku, Tokyo, 113-8656, Japan, Hiroyoshi Togo, Nippon Telegraph and Telephone Corporation, Atsugi, Kanagawa, 243-0198, Japan, and Kazutaka Nishiyama and Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 252-5210, Japan

2013-272: ELECTRON TEMPERATURE AND PLASMA POTENTIAL MEASUREMENTS IN A RADIAL PLASMA SOURCE; Gennady Makrinich, D. Zoler, and A. Fructhtman, H.I.T. – Holon Institute of Technology, Holon, 58102, Israel

2013-273: SPACE MISSIONS POTENTIALLY BENEFIT OR ENABLED BY THE PROSPECTIVE USE OF HELICON PLASMA THRUSTERS; M. Ruiz, I. urdampilleta, and J. M. del Cura, SENER Ingeniería y Sistemas, Tres Cantos, Madrid, Spain, E. Ahedo, Universidad Carlos III de Madrid, Madrid, Spain, J. Navarro-Cavallé, Universidad Politécnica de Madrid, Madrid, Spain

2013-274: PROGRESS IN TESTING OF QM AND FM HEMP THRUSTER MODULES; A. Lazurenko, A. Genovese, B. van Reijen, J. Haderspeck, S. Weis, and P. Holtmann, Thales Electronic Systems GmbH, Ulm, 89077, Germany, M. Schirra, Kempten University of Applied Sciences, K. Ruf and N. Püttmann, Deutsches Zentrum für Luft-und Raumfahrt e. V. (DLR) – Raumfahrtmanagement, Bonn, 53227, Germany

2013-275 a: ESA PROPULSION LABORATORY; A Bulit and J. Gonzalez Del Amo, ESA/ESTEC, Keplerlaan1, 2200 AG Noordwijk ZH, The Netherlands

2013-276: CONDUCTIN WALL HALL THRUSTERS; Dan M. Goebel, Richard R. Hofer, Ioannis G. Mikellides, Ira Katz, James E. Polk, and Brandon Dotson, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2013-275 b: DEVELOPMENT OF A HIGHLY PRECISE MICRO-NEWTON THRUST BALANCE; Franz Georg Hey, Astrium GmgH – Satellites, Friedrichshafen, Germany, Technische Universität Dresden, Germany, Andreas Keller, Astrium GmbH – Satellites, Friedrichshafen, Germany, Justus-Liebig, University Gießen, I. Physikalisches Institut, Germany, Dirk Papendorf, Astrium GmbH – Satellites, Friedrichshafen, Germany, Claus Braxmaier, University of Bremen, ZARM Center of Applied Space Technology and Microgravity, DLR German Aerospace Center, Institute of Space Systems, Bremen, Martin Tajmar, Technische Universität Dresden, Germany, Ulirch Johann and Dennis Weise, Astrium GmbH – Satellites, Friedrichshafen, Germany

2013-278: A DIRECT DRIVE SYSTEM APPLICATION FOR HALL EFFECT THRUSTERS; Alessio Pampaloni and Mirko Trisolini, University of Pisa, Pisa, 56122, Italy; Tommaso Misuri, Alta S.p.A., Ospedaletto, Pisa, 56121, Italy; Mariano Andrenucci, Alta S.p.A., Ospedaletto, Pisa, 56121, Italy

2013-279: HT5K HALL THRUSTER TO IMPROVE SMALL LAUNCHER CAPABILITIES; Tommaso Misuri Pierpaolo Pergola, Alta S.p.A. Ospedaletto, Pisa, 56121, Italy, Mariano Andrenucci, Alta S.p.A. Ospedaletto, Pisa, 56121, Italy

2013-280: VERIFICATION OF A FLOW CONTROL UNIT WITH GAS PURIFIER AND INTEGRATION INTO THE HEMP THRUSTER MODULE; J. Haderspeck, S. Weis, B. van Reijen, A. Lazurenko, A. Genovese, and P. Holtmann, Thales Electronic Systems GmbH, Ulm, 89077, Germany, K. Ruf and N. Püttmann, Deutsches Zentrum für Luft-und Raumfahrt e. V. (DLR) – Raumfahrt-Agentur, Bonn, 53227, Germany, M. schirra, Hochschule für angewandte Wissenschaften, Kempten, 87435, Germany, J. Kuiper, MOOG Bradford heerle, 4726 TG, The Netherlands

2013-281: HIGH SPECIFIC IMPULSE SOLUTIONS FOR ORBIT RAISING, ORBIT TOPPING AND STATION KEEPING WITH THE HEMP-T ELECTRIC PROPULSION SYSTEM; B. van Reijen, S. Weis, J. Haderspeck, A. Lazurenko, A. Genovese, and P. Holtmann, Thales Air Systems & Electron Devices GmbH, Ulm, 89077, Germany, M. Schirra, Kempten University of Applied Sciences, K. Ruf and N. Püttmann, Deutsches Zentrum für Luft-und Raumfahrt e. V. (DLR) – Raumfahrt-Agentur, Bonn, 53227, Germany

2013-282: ENVIRONMENTAL AND OPERATIONAL QUALIFICATION OF THE THALES MIXED METAL HOLLOW CATHODE NEUTRALIZER FOR THE HEMP-T BASED ION PROPULSION SYSTEM; B. van Reijen, A. Genovese, A. Lazurenko, S. Weis, J. Haderspeck, and P. Holtmann, Thales Electronic Systems GmbH, Ulm, 89077, Germany, M. Schirra, Hochschule für angewandte Wissenschaften, Kempten, 87435, Germany, K. Ruf and N. Püttmann, Zentrum für Luft-und Raumfahrt e. V. (DLR) – Raumfahrt-Agentur, Bonn, 53227, Germany

2013-283: PERFORMANCE MEASUREMENTS OF A HIGH POWERED QUAD CONFINEMENT THRUSTER; Thomas Harle, Aaron Knoll, and Vaios J. Lappas, Unversity of Surrey, Guildford, GU2 7XH, United Kingdom; Paolo Bianco, Astrium Ltd, Anchorage Road, Portsmouth, PO3 5PU, United Kingdom

2013-284: HIGH PRECISION THRUST VECTOR DETERMINATION THROUGH FULL HEMISPHERICAL RPA MEASUREMENTS ASSISTED BY ANGULAR MAPPING OF ION ENERGY CHARGE STATE DISTRIBUTION; B. van Reijen, S. Weis, A. Lazurenko, J. Haderspeck, A. Genovese, and P. Holtmann, Thales Electronic Sytstems GmbH, Ulm, 89077, Germany; K. Ruf and N. Püttmann, Deutsches Zentrum für Luft-und Raumfahrt e. V. (DLR) – Raumfahrt-Agentur, Bonn, 53227, Germany

2013-286: QUASINEUTRAL PIC ELECTRON GUIDING CENTER MODELING IN THE PRESENCE OF SLOW CROSS-FIELD ELECTRON TRANSPORT IN A HALL THRUSTER; Dariusz Danitko and Serge Barral, Institute of Plasma Physics and Laser Microfusion, Hery 23, 01-497 Warsaw, Poland, Stéphan Zurback, Snecma, Safran Group, 27208 Vernon, France

2013-289: EXPERIMENTAL DISCHARGE CHARACTERIZATION AND SCALING OF IEC PLASMA DEVICES; Constanze Syring and Greg Herdrich, University of Stuttgart, Stuttgart, 70567, Germany

2013-291: DEVELOPMENT STATUS OF AN OPEN CAPILLARY PULSED PLASMA THRUSTER WITH NON-VOLATILE LIQUID PROPELLANT; S. Barral and J. Kurzyna, Institute of Plasma Physics and Laser Microfusion, 01497 Warsaw, Poland, E. Remírez and R. Martin, JMP Ingenieros, 26371 Sotés (la Rioja), Spain, S. Bottinelli and Y. Mabillard, Mecartex, 6933 Muzzano, Switzerland, A. Zaldívar and P. Rangsten, NanoSpace AB, Uppsala Science Park, SE-751 83 Uppsala, Sweden, and C. R. Koppel, KopooS Consulting Ind., 75008 Paris, France

2013-292: DEVELOPMENT OF LONG-LIFE LIGHTWEIGHT ARCJETS; Daisuke Nakata, Muroran Institute of Technology, 27-1, Mizumoto-cho, Muroran-shi, Hokkaido 050-8585, Japan, Kiyoshi Kinefuchi, Japan Aerospace Exploration Agency, 2-1-1, Sengen, Tsukuba-shi, Ibaraki 305-8505, Japan, Masahiro Kinoshita, The University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan, Satoshi Hosoda, Aerospace Exploration Agency, 3-1-1, Yoshinodai, Chuoku, Sagamihara-shi, Kanagawa 252-5210, Japan, Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya Asahi-Ku, Osaka 535-8585, Japan, Hitoshi Kuninaka, Aerospace Exploration Agency, 3-1-1, Yoshinodai, Chuoku, Sagamihara-shi, Kanagawa 252-5210, Japan

2013-294: 2D AXISYMMETRIC FLUID AND ELECTROMAGNETIC MODELS FOR INDUCTIVELY COUPLED PLASMA (ICP) NI RF ION THRUSTERS; Emre Turkoz and Murat Celik, Bogazici University, Istanbul, Turkey

2013-295: PLASMADIAGNOSTICS IN THE PLUME OF A RADIOFREQUENCY ION THRUSTER; Christoph Eichhorn, Frank Scholze, Carsten Bundesmann, and Horst Neumann, Leibniz-Institute of Surface Modification (IOM), Permoserstrasse 15, D-04318 Leipzig, Germany

2013-296: DIRECT FUSION DRIVE ROCKET FOR ASTEROID DEFLECTION; Joseph B. Mueller, Yosef S. Razin, Michael A. Paluszek, Amanda J. Knutson, and Gary Pajer, Princeton Satellite Systems, 6 Market St., Suite 926, Plainsboro, NJ, 08536, USA; Samuel A. Cohen, Plasma Physics Laboratory, 100 Stellarator Road, Princeton, NJ, 08540; and Allen H. Glasser, University of Washington, Department of Aeronautics and Astronautics, Guggenheim Hall, Seattle, WA 98195

20123-297: BEAM DIAGNOSTICS FOR MINI ION ENGINES; Peter E. Köhler and Bruno K. Meyer, University of Giessen, 1. Physikalisches Insitut, 35392 Griessen, Germany

2013-298: 3D THERMAL SIMULATION OF A µN-RIT; Waldemar Gärtner, Benjamin Lotz, and Bruno K. Meyer, Justus-Liebig-University Giessen, I. Physikalisches Institut, Giessen, hessen, 35392, Germany

2013-299: OVERVIEW, QUALIFICATION AND DELIVERY STATUS OF THE HEMPT BASED ION PROPULSION SYSTEM FOR SMALLGEO; Stefan Weis, Alexey Lazurenko, Benjamin van Reijen, Jens Haderspeck, Angelo Genovese, and Peter Holtmann, Thales Electronic Systems GmbH, Soeflinger Str. 100, D-89077 Ulm, Germany; Klaus Ruf and Norbert Püttmann, Deutsches Zentrum Für Luft- und Raumfahrt e. V. (DLR) – Raumfahrt-Agentur, Königswinterer Strasse 522-524, 53227 Bonn; Martin Schirra, Hochschule für angewandte Wissenschaften Kempten, Bahnhofstraße 61, 87435 Kempten, Germany

2013-300: ELECTROSTATIC ANALYZERS WITH APPLICATION TO ELECTRIC PROPULSION TESTING; Casey C. Farnell and Cody C. Farnell, Colorado State University, Fort Collins, CO 80523, USA, Shawn C. Farnell, Kenyon College, Gambier, OH 43022, USA, Plasma Controls, LLC, Fort Collins, CO 80526, USA, and John D. Williams, Colorado State University, Fort Collins, CO 80523, USA, Plasma Controls, LLC, Fort Collins, CO 80526, USA

2013-301: THREE DIMENSIONAL SIMULATION OF MICRO NEWTON RITS; Robert Henrich and Christian Heiliger, Justus-Liebig-University, Giessen, 35392, Germany

2013-304: GLOBAL STABILITY ANALYSIS OF AZIMUTHAL OSCILLATIONS IN HALL THRUSTERS; Diego Escobar, Universidad Politecnica de Madrid (UPM), Madrid, 28040, Spain, Eduardo Ahedo, Universidad Carlos III de Madris (UC3M), Leganes, 28911, Spain

2013-305: INSTANT START ELECTRIDE HOLLOW CATHODE; Lauren P. Rand and John D. Williams, Colorado State University, Fort Collins, CO, 80523, USA

2013-306: INNOVATIVE VACUUM ARC THRUSTER FOR CUBESAT CONSTELLATIONS; Mathias Pietzka, Marina Kuhn-Kauffeldt, and Jochen Schein, University of the Federal Armed Forces Munchen, Werner-Heisenberg-Weg 39, 85577 Neubiberg, Germany, Igal Kronhaus and Klaus Schilling, Justus-Maximilians-Universitat Wurzburg, Am Hubland, 97074, Wurzburg, Germany, Toni Mai and Anton Lebeda, Apcon AeroSpace & Defense GmbH, Prof.-Messerschmidt-Str. 4, 85577 Neubiberg, Germany

2013-307: 3D SIMULATION OF THE ROTATING SPOKE IN A HALL THRUSTER; K. Matyash and R. Schneider, Greifswald University, Greifswald, D-17487, Germanhy, S. Mazouffre and S. Tsikata, ICARE, Centre National de la Recherche Scientifique, 45071 Orleans, France, Y. Raitses and A. Diallo, Princeton Plasma Physics Laboratory, Princeton, New Jersey 08543, USA

2013-311: IODINE PROPELLANT SPACE PROPULSION; James Szabo, Mike Robin, Surjeet Paintal, Bruce Pote, Vlad Hruby, Chas Freeman, Busek Co. Inc. Natick, MA, 01760, USA

2013-313: ACCURATELY DETERMINING THE PLASMA POTENTIAL USING EMISSIVE PROBES; J. P. Sheehan, University of Michigan, Ann Arbor, MI, 48103, USA, Yevgeny Raitses, Princeton Plasma Physics Laboratory, Princeton, NJ, 08543, USA, Noah Hershkowitz, University of Wisconsin – Madison, Madison, WI, 53706, USA

2013-315: INSIGHT INTO PERFORMANCE IMPROVEMENT OF ECR NEUTRALIZER; W. Ohmichi, The University of Tokyo, Bunkyo, Tokyo, 113-8656, Japan, H. Kuninaka, The Institute of Space and Astronautical Science, Sagamihara, Kanagawa, 252-5210, Japan

2013-317: EIGHT KILOWATT HALL THRUSTER SYSTEM CHARACTERIZATION; James Szabo, Bruce Pote, Lawrence Byrne, Surjeet Paintal, Vlad Hruby, Rachel Tedrake, George Kolencik, and Chas Freeman, Busek Co. Inc, Natick, MA, 01760, USA; Nikolaos Gatsonis, Worchester Polytechnic Institute, Worcester, MA 01609, USA

2013-318: PROGRESS ON THE DEVELOPMENT OF A PULSED PLASMA THRUSTER FOR THE ASTER MISSION; Fin Paula and Intini Marques, R., INPE – The Brazilian National Institute for Space Research, LCP – Combustion and Propulsion Laboratory – Cachoeira Paulista – Sao Paulo State, Brazil

2013-319: IONIC LIQUID FERROFLUID ELECTROSPRAY WITH EMIM-NTf2 AND FERROFLUID MODE STUDIES WITH FERROTEC-EFH-1 IN A NON-UNIFORM MAGNETIC FIELD; Edmond J. Meyer IV and Lyon B. King, Michigan Technological University, Houghton, MI 49931, USA; Nirmesh Jain and Brian s. Hawkett, University of Sydney, NSW, 2006, Australia

2013-320: APPLICATION OF AUGER SPECTROSCOPY FOR MEASUREMENT OF SECONDARY ELECTRON EMISSION FROM CONDUCTING MATERIAL FOR ELECTRIC PROPULSIOIN DEVICES; Marlene I. Patino, University of California, Los Angeles, CA, 90095, USA, Yevgeny Raitses, Princeton Plasma Physics Laboratory, Princeton, NJ, 08540, USA, and Richard E. Wirz, University of California, Los Angeles, CA 90095, USA

2013-321: OVERVIEW OF MISSION DESIGN FOR NASA ASTEROID REDIRECT ROBOTIC MISSION CONCEPT; Nathan Strange, Damon Landau, Timothy McElrath, Gregory Lantoine and Try Lam, Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Dr., Pasadena, CA, 91109; Melissa McGuire, Laura Burke, and Michael Martini, NASA Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH, 44135; and John Dankanich, NASA Marshall Space Flight Center, Huntsville, AL, 35812

2013-324: MODELING OF A DC-RF PLASMATHRUSTER WITH THE NAVIER-STOKES CODE SINA; U. Bauder and G. Herdrich and S. Fasoulas, Institute of Space Systems (IRS), University of Stuttgart, 70569 Stuttgart, Germany; M. Auweter-Kurtz, German Aerospace Academy ASA, 71304 Böblingen, Germany

2013-325: IS THERE A FUTURE FOR FISSION NUCLEAR ELECTRIC PROPULSION; Richard Blott, Director, Space Enterprise Partnerships Ltd, Eastergate, West Sussex, PO20 3SJ, UK, Christophe Koppel, KopooS Consulting Ind, Paris, 75008, France, Dr. Dominique Valentian, ITG, Paris, 75008, France, Dr. Frank Jansen, DLR, Bremen, 28359, Germany, Prof. Claudio Ferrari, ISIS R&D, Rome, 00146, Italy, Prof. Claudio Bruno, c/o ISIS R&D, Rome, 00146, Italy, Priv. Doz. Dr., Adj. Assoc, Prof/Baylor Georg Herdrich, IRS Stuttgart, Stuttgart, Stuttgart 70714, Germany, Dipl.-Ing. Roland Gabrielli, IRS Stuttgart, Stuttgart 70714, Germany

2013-327: NEAR ANODE PLASMA IN THE PLASMA INTERACTION FACILITY AT UCLA; Taylor S. Matlock, Dan M. Goebel, and Richard E. Wirz, University of California Los Angeles, Los Angeles, CA, 90095, USA

2013-329: EXPERIMENTAL INVESTIGATION OF MOMENTUM TRANSFER TO SOLID SURFACES BY THE IMPACT OF ENERGETIC IONS AND ATOMS; Thomas Trottenberg, Jakob Rutscher, and Holger Kersten, Institute of Experimental and Applied Physics, University of Kiel, 24098 Kiel, Germany

Index Continued (331-459; N)