Session O-1-1 at Room a Program Chairperson

Home , Murasaki (crater), Reimei, Sohla, Yoshikawa (crater)

June/6th (Tue) AM(1) Session o-1-1 at Room A Session d-1 at Room B Session b-1 at Room C Program Orbital Mechanics Microthrusters

Chairperson :M. Koyama (JAXA) Chairperson :K. Tsuchiya (Kyoto Univ.) Chairperson :M. Nakano (Tokyo Met. College) M. Zell (ESA) O. Montenbruck (DLR) H. Koizumi (Tokyo Univ.)

09:00-9:30 2006-o-1-01v 09:00-9:20 2006-d-01 09:20-9:40 2006-b-01 Potential International Cooperation on Explo- Perturbation Analysis of Interplanetary Sun- Eﬀects of Multi-Nozzle Jets on Thrust- ration - an ESA Perspective Synchronous Orbit Performance Improvement of Micro-Arcjets A. Thirkettle (ESA), Netherlands S. Nishimaki, K. Kuroshima (Tokyo Univ.), T. Saiki, K. Onodera, T. Noda, H. Horisawa (Tokai Univ.), I. J. Kawaguchi (JAXA), Japan Kimura (Tokyo Univ.), Japan 09:30-10:00 2006-o-1-03v Development in the Canadian Contribution to 09:20-9:40 2006-d-02 09:40-10:00 2006-b-03 the ISS Program A dynamical systems approach to the design of Characteristics of DDNP Combustion for B. Marcotte (CSA), Canada the science orbit around Europa MEMS Rocket Application M. Lara (Real Observatorio de la Armada), G. Gomez K. Takahashi, T. Okada, T. Ikuta, T. Nishiyama 10:00-10:30 2006-o-1-04v (Universitat de Barcelona), R. Russell (JPL, California (Kyushu Univ.) et.al., Japan Japan’s Kibo and the Future Vision in Space Institute of Technology), Spain Exploration 10:00-10:20 2006-b-04 Y. Hasegawa (JAXA), Japan 09:40-10:00 2006-d-03 Fundamental Investigations of Electrically- Computing long lifetime orbits for the Eoropa Augmented Micro Pulse Detonation Engines 10:30-11:00 2006-o-1-05v observation mission S. Eto, H. Horisawa, Y. Tomioka (Tokai Univ.), Japan HTV Development and the Future Vision M. Lara (Real Observatorio de la Armada), S. Ferrer H. Sasaki (JAXA), Japan (Universidad de Murcia), Spain

10:00-10:20 2006-d-04 Simulation and Characterization of Dynamical Evolution of Binary Asteroid Systems E. Gregory Fahnestock, D. J. Scheeres (Univ. of Michi- gan), USA June/6th (Tue) AM(1) Session a-1 at Room D Session u-1 at Room E Session s-1 at Room F Liquid Rocket I(Liquid Propellant Practical Ways to Practice Space Managements A) Education and Outreach Robotics Chairperson :B. Vieille (CNES) Chairperson :G. Pignolet (Science Sainte Rose) Chairperson :Y. Yoshida (Tohoku Univ.) T. Himeno (Tokyo Univ.) M. Onuki (Advocate, Asia Liaison, T. Kubota (JAXA/ISAS) Space Frontier Foundation) 09:00-9:20 2006-a-01 09:00-9:20 2006-s-01 Dynamic Behavior of Liquid Propellant in Tank 09:00-9:20 2006-u-01 Simultaneous Feedback Stabilization of Space on Upper Stage Engine which have the function Educational Models for Integrated SSP/WPT Robot Attitude of the re-ignition Systems and H2 Technologies T. Hashimoto (Tokyo Metropolitan Institute of Tech- Y. Kano, Y. Kano (IA), T. Mochizuki (ISE), H. Otsuka G. Pignolet (Science Sainte Rose), J. Lan sun luk nology), Japan (IA) et.al., Japan (Univ. of La Reunion), I. Ingar (Arer, La Reunion), France 09:20-9:40 2006-s-02 09:20-9:40 2006-a-02 Fault Detection in Autonomous Assembly by Development and Results of Space Evaluation 09:20-9:40 2006-u-02 Space Robot using Semantic Task Model Test for Vane Type Tank System(VTS) Student Small Science Payload Promotions K. Sawayama (Tokyo Univ.), Japan R. Imai (Research Institute, IHI), Y. Takano, K. Ya- Program for the Rocketplane XP mada (IHI Aerospace), K. Hama (USEF) et.al., Japan C. John Lauer, C. John Lauer (Rocketplane, Ltd.), M. 09:40-10:00 2006-s-03 Onuki (Space Frontier Foundation), USA DEPLOYMET OF ELECTRODYNAMIC 09:40-10:00 2006-a-03 TETHER USING SIMPLE REEL MECHA- Experimental Investigation of the Dynamic 09:40-10:00 2006-u-04 NISM Characteristics of Lateral Sloshing in a Concen- Experimental rocket project in Gifu for launch- T. Ikeda, Y. Yamagiwa (Shizuoka Univ.), S. tric Membrane Tank ing within a campaign organized by French as- Kawamoto, Y. Okawa (Advanced Space Technology K. Komatsu, M. Nishimoto (JAXA), Japan sociation Planete Sciences in La Courtine Research Group, JAXA/IAT) et.al., Japan M. Sasaki (Gifu Univ.), K. Ogimoto, N. Nakano (Space 10:00-10:20 2006-a-04 Club Gifu), A. Ishida (Gifu Univ.) et.al., Japan 10:00-10:20 2006-s-04 Numerical Analysis of Dynamic Behavior of Development of Engineering Test Satellite Free-Surface Flows in Tanks Based on CIP-LSM 10:00-10:20 2006-u-05 STARS-1 for Tethered Space Robot H. Negishi (JAXA’s Engineering Digital Innovation Development Status of the Microsatellite KKS- T. Yamamoto, T. Yamamoto, H. Yoshihara, A. An- Center, JAXA), T. Himeno (Tokyo Univ.), N. Yaman- 1 by the Tokyo Metropolitan College of Tech- datsu (Kagawa Univ.) et.al., Japan ishi (JAXA’s Engineering Digital Innovation Center, nology JAXA), Japan T. Ishikawa, M. Nakano, T. Miyano, R. Wakabayashi 10:20-10:40 2006-s-05 (Tokyo Metropolitan College of Technology), Japan Orbital Transfer of a Tether System Using Pitch 10:20-10:40 2006-a-05 Motion Control through Tether Length Varia- CFD studies of cryogenic propellant manage- tion ment N. Shibata (Kyushu Univ.), Japan J. Lacapere (Air Liquide), France June/6th (Tue) AM(1) Session r-2-1 at Room G Session p-1 at Room H Impact Experiment Space Medicine (1)

Chairperson :P. Harkness (Cranﬁeld Univ.) Chairperson :T. Maruyama (Tokyo Inst. of Tech.) J. Ishizawa (JAXA) T. Hagale (Boeing co.)

09:00-9:20 2006-r-2-01 09:00-9:20 2006-p-01 Properties of Fragments from Low-Velocity Im- Space Scale: Instrument for Astronaut Mass Mea- pacts on Micro Satellite surement Y. Tsuruda, K. Nakashima, T. Hanada (Kyushu Y. Fujii (Gunma Univ.), K. Shimada (JAXA), Japan Univ.), Japan 09:20-9:40 2006-p-02 09:20-9:40 2006-r-2-02 Eﬀect of Centrifuge-induced Artiﬁcial Gravity and Measurement of the Ejector Generated by Erogometric Exercise on Cardiovascular Decondi- the Hypervelocity Impact Experiment on Thin tioning, Myatrophy, and Osteoporosis Induced by Film Materials -6◦ Head-down Bedrest for 20 Days K. Tanaka (JAXA), Y. Saitoh (Tokyo Univ. of Sci- S. Iwase, H. Takada (Aichi Medical Univ.), Y. Watanabe ence), S. Kosyo (Tokai Univ.), S. Sasaki (JAXA), (Nagoya Univ.), K. Ishida (Research Center for Physical Japan Fittness and Sports) et.al., Japan

09:40-10:00 2006-r-2-03 09:40-10:00 2006-p-03 Estimation of Debris Cloud Generated by Countermeasure Development and Optimization Oblique Impacts Using the Bed Rest Model M. Higashide, T. Okumura, O. Hayashi, T. Koura P. D Jost, O. Angerer, P. Sundblad, D. A. Schmitt (ESA), (Kyushu Institute of Technology) et.al., Japan Netherlands

10:00-10:20 2006-r-2-04 10:00-10:20 2006-p-04 New Measurement of Velocity of Debris Cloud Study of the Development of Device to Maintain Using X-ray Radiograph the Skeletal Muscles in the Space T. Okumura, Y. Akahoshi, K. Watanabe, T. Koura N. Shiba (Kurume Univ.), Y. Tagawa (Kyushu Institute (Kyushu Institute of Technology) et.al., Japan of Technology), Y. Umezu, H. Matsuse (Kurume Univ.) et.al., Japan

10:20-10:40 2006-p-05 Vestibular system contributes human blood pressure control upon gravitational changing C. Awazu (Fukui Univ.), K. Tanaka, C. Abe, H. Morita (Gifu Univ.), Japan June/6th (Tue) AM(2) Session o-1-2 at Room A Session d-2 at Room B Session b-2 at Room C Utilization Interplanetary Mission Analysis Laser Microthruster

Chairperson :N. Fukuda (MHI) Chairperson :J. Fertig (ESA/ESOC) Chairperson :K. Takahashi (Kyushu Univ.) B. Marcotte (CSA) Y. Kawakatsu (JAXA/ISAS) H. Shiraishi (Daido Inst. of Tech.)

11:10-11:40 2006-o-1-06v 10:30-10:50 2006-d-05 10:30-10:50 2006-b-05 NASA Utilization of the International Space BepiColombo - Navigation Challenges on the A laser ignition microthruster for microspace- Station and the Vision for Space Exploration Way to Mercury craft propulsion J. A Robinson, D. A Thomas (NASA), USA D. Garcia yarnoz (GMV at ESA/ESOC), R. Jehn M. Nakano (Tokyo Metropolitan College of Aeronauti- (ESA/ESOC), N. Sanchez (Deimos Space), Germany cal Engineering), H. Koizumi, T. Inoue (Tokyo Univ.), 11:40-12:10 2006-o-1-07v M. Watanabe (Nichiyu Giken Kogyo Co., LTD.) et.al., ESA’s Life and Physical Science Programme - 10:50-11:10 2006-d-06 Japan Achievement and Plans Control Strategies for the Fly-bys of Asteroids M. Zell (ESA), Netherlands Steins and Lutetia during Rosetta Cruise 10:50-11:10 2006-b-06 V. Companys, J. Fertig (ESOC), M. Diaz (GMV at Research and Development of Compact Laser 12:10-12:40 2006-o-1-08v ESOC), Germany Ablative Thrusters for Small Satellites JAXA Utilization and the Future Vision H. Maesato, S. Matsunami, H. Tahara (Osaka Univ.), M. Koyama (JAXA), Japan 11:10-11:30 2006-d-07 Japan Operational experience during orbit insertion of Venus Express - ESA’s second planetary mis- 11:10-11:30 2006-b-07 sion Simple Calculation of Ablation Process and V. Companys, M. Lauer (ESOC), Germany Performance for Laser Ablative Thrusters S. Matsunami, T. Edamitsu, H. Maesato, H. Tahara 11:30-11:50 2006-d-08 (Osaka Univ.), Japan Preliminary Mission Analysis of a Jupiter Entry Probe Mission 11:30-11:50 2006-b-08 M. Khan, P. De pascale (ESA-ESOC), Germany Electromagnetic Acceleration Characteristics of a Laser-Electric Hybrid Thruster 11:50-12:10 2006-d-09 Y. Sasaki, K. Sasaki, H. Horisawa (Tokai Univ.), I. Analysis of operational strategies to achieve Kimura (Tokyo Univ.), Japan long Mars Express mission duration, to provide relay services for future Martian missions V. Companys (ESOC), M. Muller (EDS at ESOC), R. Cramm (ESOC), Germany June/6th (Tue) AM(2) Session a-2 at Room D Session u-2 at Room E Session s-2 at Room F Space Education and Outreach Liquid Rocket II(Liquid Propellant Space Transportation Technology Managements B) Programs for theGeneral Public Chairperson :J. Lacapere (Air-Liquide) Chairperson :J. Souchay (Paris Observatory) Chairperson :H. Taguchi (JAXA) K. Komatsu (JAXA) F. Tanigaki (JAXA) H. Nagata (Hokkaido Univ.)

10:50-11:10 2006-a-06 10:50-11:10 2006-u-06 11:10-11:30 2006-s-07 Development of Numerical Methods for Propel- Space Education for Children with Disability in Aerodynamic Characteristics of vertical landing lant Management Remote Areas rocket vehicle during turn-over T. Himeno, T. Watanabe (Tokyo Univ.), Japan S. Aso (Kyushu Univ.), T. Ebisuzaki (RIKEN), I. Y. Imamura (Tokyo Univ.), S. Nonaka, H. Ogawa, Y. Chikami (Okierabu High school), S. Mitsumori (Insti- Inatani (ISAS/JAXA), Japan 11:10-11:30 2006-a-07 tute for Future Technology) et.al., Japan Liquid Propellant Management in Launcher 11:30-11:50 2006-s-08 Tanks: the COMPERE research program 11:10-11:30 2006-u-07 Coherent Anti-Stokes Raman Spectroscopic B. Vieille, B. Legrand (CNES), France Public Astronomical Observatory Network Measurement of radiation behind Hyperveloc- (PAONET) – A Network for Sharing Digital ity Shock Waves 11:30-11:50 2006-a-08 Contents and Human Resources on Education K. Arimura, K. Miyazaki, B. Suhe, K. Maeno (Chiba Cryogenic Propellant Management of H-IIA of Astronomy – Univ.) et.al., Japan Upper Stage M. Okyudo (Wakayama Univ.), T. Ono, H. Agata O. Kitayama, T. Tokunaga, K. Tanimoto (MHI), H. (National Astronomical Observatory of JAPAN), C. 11:50-12:10 2006-s-10 Taniguchi (JAXA), Japan Yoshizumi (Tokushima Science Museum) et.al., Japan Preliminary Experment of Laser Micro Propul- sion Using Powdered-Propellant 11:50-12:10 2006-a-09 11:30-11:50 2006-u-08 S. Yokoyama, H. Horisawa (Tokai Univ.), I. Funaki, H. BOILING UNDER MICROGRAVITY Outreach Activities of National Astronomical Kuninaka (JAXA), Japan A. Hoornaert, A. Lakhdar, G. Duhar, C. Colin Observatory of Japan (NAOJ) (IMFT), France T. Ono, H. Agata, J. Watanabe, T. Fukushima (Na- tional Astronomical Observatory of Japan), Japan 12:10-12:30 2006-a-10 The eﬀects of gravitational acceleration on cryo- 11:50-12:10 2006-u-09 genic forced convective boiling Academic and Non Academic Teaching of As- O. Kawanami, T. Nishida, I. Honda, Y. Kawashima tronomy in France (Univ. of Hyogo) et.al., Japan J. Souchay (Observatoire de Paris), France

12:10-12:30 2006-u-10 JAXA Education Program related with the ISS F. Tanigaki (JAXA), Japan June/6th (Tue) AM(2) Session r-2-2 at Room G Session p-2 at Room H Space Debris and Measurement and Orbital Estimation (1) Space Medicine (2) Chairperson :D. Alwes (DLR) Chairperson :P. Jost (ESA) Y. Akahoshi (Kyushu Inst. of Tech.) S. Iwase (Aichi Med. Univ.)

10:30-10:50 2006-r-2-05 10:50-11:10 2006-p-06 Space Debris Surveillance Results in TKSC/JAXA Radiation Exposure Management for Japanese Y. Taromaru, C. Hirose (JAXA), M. Kameyama (Fujitsu ISS Crew Members Limited), S. Aoki (Japan Space Forum) et.al., Japan S. Yabe, M. Kyoda, Y. Koike, T. Murai (JAXA) et.al., Japan 10:50-11:10 2006-r-2-06 Collaboration in Radar Observation and Re-entry 11:10-11:30 2006-p-07 Predictions Research and Development of Japanese Resort Y. Taromaru, C. Hirose (JAXA), M. Kameyama (Fujitsu Curry as a Space Food Limited), S. Aoki (Japan Space Forum), Japan A. Kuramoro (Housefoods Corporation), Japan

11:10-11:30 2006-r-2-07 11:30-11:50 2006-p-08 Optical Observations of Space Debris at the Bisei Development of JAXA Space Food Spaceguard Center: Limitting-Magnitude Evalua- T. Nakazawa, S. Tachibana, K. Yanagawa (JAXA), tion and Magnitude Variability Japan S. Okumura, S. Isobe (Japan Spaceguard Association), Japan 11:50-12:10 2006-p-09 New Methodology Applied to JEM Ad hoc 11:30-11:50 2006-r-2-08 Evaluation to Enhance Mission Success GEO Space Debris Optical Observation Technolo- S. Sasaki, T. Nakahara, K. Niitsu (JAXA), Japan gies A. Nakajima (JAXA), H. Kurosaki (JAXA), Japan June/6th (Tue) PM(1) Session o-1-3 at Room A Session d-3 at Room B Session b-3 at Room C Technologies HAYABUSA Flight Results Laser and Microwave Propulsion

Chairperson :Y. Hasegawa (JAXA) Chairperson :L.A. Cangahuala (NASA/JPL) Chairperson :H. Takegahara (Tokyo Met. Univ.) J.A. Robinson (NASA) K. Tsuchiya (Kyoto Univ.) K. Komurasaki (Tokyo Univ.)

14:30-15:00 2006-o-1-09v 14:30-14:50 2006-d-10 14:40-15:00 2006-b-09 Human Engineering for Manned Space Systems Overview of HAYABUSA Astrodynamics Experi- A Multi Pulse Flight Experiment of a C. Harada (JAXA), Japan ments -Asteroid ITOKAWA Transfer ans Landing- Microwave-Beaming Thruster J. Kawaguchi (JAXA), Japan Y. Oda, K. Komurasaki (Tokyo Univ.), K. Takahashi, 15:00-15:30 2006-o-1-10v A. Kasugai (Naka Fusion Institute, Japan Atomic En- Achievements from the Kibo Program and the 14:50-15:10 2006-d-11 ergy Agency) et.al., Japan future eﬀorts HAYABUSA TRAJECTORY SYNTHESIS AND N. Fukuda, H. Yamaguchi (MHI), Japan RESULTS - ION ENGINE CRUISE TO ITOKAWA 15:00-15:20 2006-b-10 M. Matsuoka, T. Kominato (NEC Aerospace Sys- Induction Phenomena in a Laser-Augmented 15:30-16:00 2006-o-1-11v tems,Co.Ltd), J. Kawaguchi (ISAS/JAXA), Japan Scramjet Future Plans for JEM Exposed System Appli- J. Yonehara, S. Isimoto, H. Horisawa (Tokai Univ.), I. 15:10-15:30 2006-d-12 cations Kimura (Tokyo Univ.), Japan HAYABUSA Orbit Determination just before the M. Akiyama (IHI Aerospace Co,.Ltd), Japan Rendezvous with Itokawa 15:20-15:40 2006-b-11 T. Ohnishi (Fujitsu Ltd.), M. Yoshikawa, T. Kato, T. 16:00-16:30 2006-o-1-12v Numerical Analysis on Ignition and Forma- Ichikawa (JAXA), Japan Future Space Robotics Based on JEMRMS De- tion of Laser-Supported Detonation Wave in velopment 15:30-15:50 2006-d-13 Axisymmetric Nozzle Using Thermal Non- F. Kuwao (NEC Toshiba Space Systems, Ltd), Japan OPTICAL HYBRID NAVIGATION AND GUID- equilibrium Model ANCE IN HAYABUSA - APPROACH, STATION H. Shiraishi (Daido Institute of Technology), Japan 16:30-17:00 2006-o-1-13v KEEPING & HOVERING Conceptual Study on an Orbital Hotel Attached T. Kominato, M. Matsuoka (NEC Aerospace Systems, Ltd.), 15:40-16:00 2006-b-12 to the ISS M. Uo (NEC/Toshiba Space Systems, Ltd.), J. Kawaguchi Numarical analysis of energy conversion process T. Yoshida (Shimizu Corporation), H. Lorenzo (Msc- (JAXA/ISAS.) et.al., Japan in the one dimensional laser supported deto- Industrial Designer), Japan nation wave driven by a linearly focused laser 15:50-16:10 2006-d-14 beam HAYABUSA NAVIGATION PRIOR TO FINAL K. Kawamura, M. Ushio, H. Katsurayama, K. Ko- DESCENT WITH LANDMARK TRACKING murasaki (Tokyo Univ.) et.al., Japan K. Shirakawa, H. Morita (NEC Aerospace Systems, Ltd.), M. Uo (NEC TOSHIBA Space Systems, Ltd.), T. Hasimoto (ISAS/JAXA) et.al., Japan 16:10-16:30 2006-d-15 HAYABUSA GUIDANCE AND NAVIGATION FOR AUTONOMOUS FINAL DESCENT AND TOUCHDOWN M. Uo (NEC TOSHIBA Space Systems, Ltd.), K. Shirakawa (NEC Aerospace Systems, Ltd.), T. Hasimoto, T. Kubota (ISAS/JAXA) et.al., Japan June/6th (Tue) PM(1) Session a-3 at Room D Session u-3 at Room E Session s-3 at Room F Liquid Rocket III (Injector, Unique Examples of Space Education Combustion) and Outreach Small Satellite Chairperson :M. Nosaka (JAXA) Chairperson :M. Yoshikawa (JAXA) Chairperson :S. Aso (Kyushu Univ.) M. Atsumi (MHI) L. Scatteia (CIRA) M. Miyazaki (Nihon Univ.)

14:30-14:50 2006-a-11 14:30-14:50 2006-u-11 14:30-14:50 2006-s-11 Characteristics of Fuel Mixers of Liquid Rocket On The Use of Serious Videogames To Promote Development of Micro Satellite in Kyushu Univer- Engines Under Supercritical Pressure Condi- Space and Educate on Space Sciences sity tions L. Scatteia (CIRA - Italian Aerospace Research Cen- I. Kim, H. Hirayama, T. Hanada, T. Yasaka (Kyushu T. Onodera, M. Takahashi, M. Sasaki, H. Sakamoto tre), Italy Univ.), Japan (JAXA) et.al., Japan 14:50-15:10 2006-u-12 14:50-15:10 2006-s-12 14:50-15:10 2006-a-12 STUDIO PROGRAM OF SPACE ARCHI- Analysis of the plasma environment in polar earth LE-7A Sub Scale Combustion tests to Clarify TECTURE ON UNIVERSITY orbit using data of Defense Meteorological Satellite Causes of Severe Side-loads in the Nozzle Y. Ikeda (Keio Univ.), Japan T. Hamanaga, S. Hatta, M. Cho (Kyushu Institute of Tech- T. Tomita, M. Sasaki, M. Takahashi, H. Sakamoto nology), Japan (JAXA) et.al., Japan 15:10-15:30 2006-u-13 Orbital Motion by Computer Graphics for Ed- 15:10-15:30 2006-s-13 15:10-15:30 2006-a-13 ucational Use Demonstration satellite of aerobrake around Earth Characteristics of Flows and Discharge Coeffi- M. Yoshikawa (JAXA), K. Nishiyama (Japan Space- for aerocapture around Jupiter cients in Coaxial Injectors with Cold Flow Tests guard Association), D. Kuroda (National Astronomical K. Yotsumoto, H. Hirayama, T. Hanada (Kyushu Univ.), Y. Nunome, H. Sakamoto, T. Onodera, H. Tamura Observatory), Japan T. Yasaka (Institute for Q-shu Pioneers of Space), Japan (JAXA) et.al., Japan 15:30-15:50 2006-u-14 15:30-15:50 2006-s-14 15:30-15:50 2006-a-14 Web-based education activity in space develop- The Design of the Attitude Determination System Mechanisms of Soot Emission Control of Hydro- ment field for the Hokkaido Satellite carbon Diffusion Flames by Low-Power Corona J. Terazono, J. Terazono (JAXA), N. Wakabayashi, H. D. Igarashi (Hokkaido Univ.), Japan Discharges Kurose (Tokyo Univ. of Technology) et.al., Japan N. Tujimura, H. Horisawa (Tokai Univ.), I. Kimura 15:50-16:10 2006-s-15 (Tokyo Univ.), Japan 15:50-16:10 2006-u-15 APPLYING A SIMPLE CONTOL LAW TO DE- SPACE EDUCATION IN THE INTERNA- PLOY SPACE TETHER ON A MICRO TETH- 15:50-16:10 2006-a-15 TIONAL SPACE UNIV ERED SATELLITE MB-XX Cryogenic Upper Stage Engine De- T. Ito (JAXA), Japan T. Imazu, Y. Tanaka, H. Hirayama, T. Hanada (Kyushu velopment Progress and Demonstrator Engine Univ.), Japan Hot-Fire Testing M. Atsumi, A. Ogawara, H. Nakanishi (MHI), W. F. 16:10-16:30 2006-s-16 Sack (Pratt & Whitney) et.al., Japan Design of Deep Space Explorer Propelled by Mag- netoplasma Sail T. Kimura (Tokai Univ.), I. Funaki, H. Yamakawa (JAXA), H. Horisawa (Tokai Univ.), Japan June/6th (Tue) PM(1) Session r-2-3 at Room G Session p-3 at Room H Space Debris and Measurement and Orbital Estimation (2) Human Space Tehonology Chairperson :S. Mirmina (NASA) Chairperson :S. Tachibana (JAXA) T. Hanada (Kyushu Univ.) S.Murase (Shinshu Univ.)

14:50-15:10 2006-r-2-09 14:30-14:50 2006-p-10 Destruction and Microwave Emission due to Hyperve- Telemedicine in Japan and to Space locity Impacts onto External Wall of Spacecraft S. Murase, N. Sakata (Shinshu Univ.), H. Ohshima, A. Kozaki E. Soma, K. Ishii (Tokyo Univ. of Science), H. Ohnishi, S. (JAXA) et.al., Japan Chiba (Tokyo Univ.) et.al., Japan 14:50-15:10 2006-p-11 15:10-15:30 2006-r-2-10 Telemedicine in Space and its Advancement Utilizing LONG-TERM EVOLUTION OF GEOSYN- Commercial Devices CHRONOUS ORBITAL DEBRIS WITH HIGH C. Mukai, N. Inoue (JAXA), Japan AREA-TO-MASS RATIOS L. Anselmo, C. Pardini (ISTI/CNR), Italy 15:10-15:30 2006-p-12 IVA Veriﬁcation Using Human Modeling Analysis 15:30-15:50 2006-r-2-11 T. J. Hagale (The Boeing Company), USA Current Status of Low Earth Orbital Debris Modeling in Japan 15:30-15:50 2006-p-13 T. Narumi (Kyushu Univ.), T. Hanada (Space Environment Design of a New Space Suit Research Center, Kyushu Univ.), S. Kawamoto, S. Kibe A. V. Gubarevich, T. Maruyama, O. Odawara (Tokyo Institute (JAXA), Japan of Technology), Japan

15:50-16:10 2006-r-2-12 15:50-16:10 2006-p-14 LEO debris motion estimation Future Space Suit Development H. Kurosaki, A. Nakajima (JAXA), T. Kuribayashi (Nippon M. Mohri, K. Yanagawa, T. Yamaguchi, K. Yamagata (JAXA), Institute of Technology), Japan Japan

16:10-16:30 2006-r-2-13 16:10-16:30 2006-p-15 Trends in Reorbiting of Geostationary Satellites Physiological Eﬀects of Mechanical Counter Pressure R. Jehn, H. Klinkrad (ESA/ESOC), Germany Glove and Sleeve for Extravehicular Activity. K. Tanaka, C. Abe, C. Awazu, H. Morita (Gifu Univ.) et.al., 16:30-16:50 2006-r-2-14 Japan A new method of danger debris ﬁlter for collision risk assessment 16:30-16:50 2006-p-16 S. Hu, G. Tang, C. Li (Beijing Aerospace Flight Control Cen- WETS EVA Underwater Demonstration ter), China Y. Sone, Y. Saito, S. Ishida, K. Yamagata (JAXA) et.al., Japan June/6th (Tue) PM(2) Session d-4 at Room B Session b-4 at Room C Session a-4 at Room D Space Robotics Pulsed Plasma Thrusters Liquid Rocket IV (Turbopump,Nozzle)

Chairperson :K. Yoshida (Tohoku Univ.) Chairperson :H. Nakashima (Kyushu Univ.) Chairperson :W.F. Sack (PWR) S. Nakasuka (Tokyo Univ.) H. Horisawa (Tokai Univ.) M. Atsumi (MHI) 16:10-16:30 2006-b-13 16:40-17:00 2006-d-16 16:20-16:40 2006-a-16 Research and Development of High-Impulse Elec- An Effective Modeling Method of Contact Dy- Thermodynamic Effect of Cavitating Inducer in trothermal Pulsed Plasma Thrusters namics for Satellite Capturing a Hydrogen Rocket Turbopump T. Edamitsu, H. Tahara (Osaka Univ.), Japan N. Inaba, H. Sawada (JAXA), Y. Funaki (Tokyo Insti- K. Kinefuchi, M. Uchiumi, H. Yamada (JAXA), Japan tute of Technology), S. Ueda (JAXA), Japan 16:30-16:50 2006-b-14 R&D on Pulsed Plasma Thruster with Wide Thrust 16:40-17:00 2006-a-17 17:00-17:20 2006-d-17 Performance Evaluation of Durability of Hybrid Ceramic Angular Velocity Control of an Asymmetrical Y. Kamishima, J. Iio, J. Uezu, M. Mukai (Tokyo Metropoli- Ball Bearings in Liquid Hydrogen at 3 Million Rigid Spacecraft Using Two Constant Torque tan Univ.) et.al., Japan DN(120,000 rpm) H. Kojima (Tokyo Metropolitan Univ.), Japan M. Nosaka, S. Takada, M. Kikuchi, T. Sudo (JAXA) 16:50-17:10 2006-b-15 et.al., Japan Effects of Nozzle and Cavity Configuration on an 17:20-17:40 2006-d-18 Electrothermal Pulsed Plasma Thruster Analysis and Design of Dynamics and Control 17:00-17:20 2006-a-18 W. Matsuura, T. Edamitsu, H. Tahara (Osaka Univ.), Japan to Recover from Incomplete Grasping of Dock- Performance evaluations of the methane fueled ing Mechanism for Nanosatellite 17:10-17:30 2006-b-16 rocket nozzles under high altitude conditions K. Ui (JAXA), S. Matunaga (Tokyo Institute of Tech- Use of Solid Chemical Propellants for Coaxial Pulsed T. Ito, A. Kumakawa, K. Hasegawa, M. Sato (JAXA) nology), Japan Plasma Thrusters et.al., Japan H. Mashidori, T. Tachibana (Kyushu Institute of Technol- 17:40-18:00 2006-d-19 ogy), Japan 17:20-17:40 2006-a-19 Robust Skills for Assembly Task Found by Au- Effect of Nozzle Deployment Position on Dy- 17:30-17:50 2006-b-17 tonomous Learning Space Robot namic Characteristics of an Extendible Nozzle Performance Characteristics of an Electrothermal K. Senda, S. Fujii (Kanazawa Univ.), Japan M. Sato, S. Moriya, M. Tadano, M. Sato (JAXA) et.al., Pulsed Plasma Thruster with Teflon-Alternative Japan Propellants 18:00-18:20 2006-d-20 H. Asakura, T. Edamitsu, H. Tahara (Osaka Univ.), Japan Tethered Recovery and Its Behavior of Tethered 17:40-18:00 2006-a-20 Sampling for Deep Space Minorbody Exploration 17:50-18:10 2006-b-18 FLOW SEPARATION AND THE ASSOCI- S. Matunaga (Tokyo Institute of Technology), O. Mori, Performance Characteristics of an Electrothermal ATED SIDE-LOAD ORIGIN IN A THRUST K. Nakaya (ISAS/JAXA), S. Masumoto (Tokyo Institute Pulsed Plasma Thruster with an Insulator-Rod- OPTIMIZED PARABOLIC NOZZLE of Technology) et.al., Japan Arranged Cavity S. Bhushan Verma (NAL Bangalore), O. Haidn (DLR H. Sugihara, T. Edamitsu, H. Tahara (Osaka Univ.), Japan Lampoldshausen, Germany), India 18:20-18:40 2006-d-21 18:10-18:30 2006-b-19 System configuration of tethered spinning solar A Preliminary Study on an Active-controlled Thrust 18:00-18:20 2006-a-21 sail for orbital experiment Numerical simulation Stand for Thrust Variation Measurement Volvo Aero Technologies for Advanced Rocket and ground experiment A. Kakami (National Institute of Advanced Industrial Sci- Nozzles S. Masumoto, K. Omagari, T. Yamanaka, S. Matunaga ence and Technology), R. Hiyamizu, S. Masaki, T. Tachibana R. Ryden (Volvo Aero Corporation), Sweden (Tokyo Institute of Technology), Japan (Kyushu Institute of Technology), Japan June/6th (Tue) PM(2) Session s-4 at Room F Session r-2-4 at Room G Ground Testing Space Debris Mitigation

Chairperson :P.M. Bainum (Howard Univ.) Chairperson :S. Aoki (Keio Univ.) K. Suzuki (Tokyo Univ.) R. Jehn (ESOC)

16:40-17:00 2006-s-17 17:00-17:20 2006-r-2-15 ESD Tests on Cu(In,Ga)Se2 thin-ﬁlm solar cell in sim- ISO STANDARDS: THE NEXT STEP FOR ulated LEO Plasma Environment ORBITAL DEBRIS MITIGATION T. Okumura, S. Hosoda, J. Kim, K. Toyoda (Kyushu Institute J. R Davey (BNSC), E. A. Taylor (Consultant to of Technology) et.al., Japan BNSC), Y. Kitazawa (IHI), T. Goka (JAXA), UK

17:00-17:20 2006-s-18 17:20-17:40 2006-r-2-16 Environmental Eﬀects on Electron Emission Charac- Drag Sail Optimisation for the Safe and Rapid teristics of Carbon Nanotube Cathodes Disposal of Spacecraft from Low Earth Orbit Y. Nakamura, Y. Yamagiwa (Shizuoka Univ.), Y. Okawa, S. P. G Harkness, P. C e Roberts (Cranﬁeld Univ.), UK Kawamoto (JAXA) et.al., Japan 17:40-18:00 2006-r-2-17 17:20-17:40 2006-s-19 DEBRIS MITIGATION WITH SELF BAL- Development of an electron beam source for spacecraft ANCED ELECTRODYNAMIC TETHERS charging study J. Pelaez, M. Sanjurjo (Technical Univ. of Madrid K. Odahara, S. Hosoda, K. Toyoda, M. Cho (Kyushu Institute (UPM)), Spain of Technology), Japan 18:00-18:20 2006-r-2-18 17:40-18:00 2006-s-20 Survivability of Electrodynamic Tether until Simulation of Plasma Environment around a Bare Atmospheric Reentry Tether H. Hirayama, A. Oishi, T. Hanada (Kyushu Univ.), K. Kashihara, D. Qu, T. Muranaka, M. Cho (Kyushu Institute Japan of Technology) et.al., Japan 18:20-18:40 2006-r-2-19 18:00-18:20 2006-s-21 Dynamic of a Crawler Mass of Space Tether Emission spectroscopy of arc plasma on solar array in System GEO environment H. A. Fujii, T. Watanabe, T. Kusagaya, M. Ohta T. Ose, Y. Sanmaru, T. Kitamura, T. Kawasaki (Kyushu In- (TMU) et.al., Japan stitute of Technology) et.al., Japan

18:20-18:40 2006-s-22 Plasma measurements for code validation of Multi- Utility Spacecraft Charging Analysis Tool N. Kurahara, T. Muranaka, S. Hatta, J. Kim (Kyushu Institute of Technology) et.al., Japan June/7th (Wed) AM(1) Session o-2-1 at Room A Session d-5 at Room B Session b-5 at Room C Investigations of the Teritory Reentry and Landing Ion Thrusters (1)

Chairperson :J. Kawaguchi (JAXA/ISAS) Chairperson :F. Terui (JAXA/IAT) Chairperson :M. Cho (Kyushu Inst. of Tech.) G. Schwehm (ESA/ESTEC) N. M. Ivanov (RMCC) Y. Yamagiwa (Shizuoka Univ.)

09:00-9:30 2006-o-2-01v 09:00-9:20 2006-d-22 09:00-9:20 2006-b-20 Two Mars Years of Science Operations: Results Analytical Solution of Guidance Law for Verti- HAYABUSA Explorer Ion-Driven in Deep from the Mars Odyssey Mission cal Landing Vehicles with Input Constraint Space D. A Senske, J. J. Plaut (JPL), USA K. Uchiyama, Y. Shimada (Nihon Univ.), Japan H. Kuninaka, K. Nishiyama, I. Funaki, T. Yamada (ISAS/JAXA) et.al., Japan 09:30-10:00 2006-o-2-02v 09:20-9:40 2006-d-23 Phoenix :The First Mars Scout Mission (A Mid- A Perturbation Approach in Determination of 09:20-9:40 2006-b-21 Term Report) Closed-Loop Optimal-Fuzzy Control Policy for Result of 16,000 hours Endurance Test on B. G Goldstein (JPL), USA Lunar Lander 20mN class Xenon Ion Thruster for ETS-VIII S. H. Pourtakdoust, A. B. Novonzadeh (Sharif Univ. T. Ozaki, Y. Inanaga, Y. Kasai, T. Nakagawa 10:00-10:30 2006-o-2-03v of Technology), Iran (MELCO) et.al., Japan The ExoMars mission and the European Space Exploration Programme ”Aurora” 09:40-10:00 2006-d-24 09:40-10:00 2006-b-22 P. Messina, B. Gardini (ESA), France Rosetta mission: Simulation of landing on a Overview and research status of the JAXA 150- rubble pile model of comet 67 P/Churyumov mN Ion Engine 10:30-11:00 2006-o-2-04v Gerasimenko Y. Ohkawa, Y. Hayakawa, H. Yoshida, K. Miyazaki The Venus Express Mission R. Garmier, T. Ceolin (CS), France (JAXA) et.al., Japan H. Svedhem, O. Witasse, G. Schwehm (ESA/ESTEC), D. Titov (Max Planck Institute for Solar System Re- 10:00-10:20 2006-d-25 10:00-10:20 2006-b-23 search), Netherlands Three-Dimensional Entry Guidance Using Ex- Geospace Environment Simulator and the Ap- act Linearization plication to the Analysis of Plasma Emission 11:00-11:30 2006-o-2-05v A. Abe, Y. Shimada, K. Uchiyama (Nihon Univ.), from Ion Propulsion Engine PLANET-C: Venus Climate Orbiter mission of Japan H. Usui (Kyoto Univ.), M. Okada (Nationa Institute Japan for Polar Research), Y. Omura (Kyoto Univ.), T. Mu- T. Imamura, M. Nakamura, T. Abe, N. Ishii (JAXA) 10:20-10:40 2006-d-26 rata (Ehime Univ.) et.al., Japan et.al., Japan Flight Test Result and Dynamic Motion of Glid- ing Parachute Recovery Demonstrator Vehicle 10:20-10:40 2006-b-24 11:30-12:00 2006-o-2-06v (GPRDV) Eﬀects of Environmental Conditions to Dis- AN OVERVIEW OF THE JUNO MISSION H. Ohtsuka, H. Ohtsuka, N. Sano (IHI Aerospace), Y. charge Characteristics of Hollow Cathode TO JUPITER Tsuda (JAXA) et.al., Japan T. Katayama (Tokyo Metropolitan Univ.), J. Mat- R. Grammier (JPL), USA suyama, T. Naka (Tokyo Metropolitan Institute of Technology), H. Ishikawa (Tokyo Metropolitan Univ.) et.al., Japan June/7th (Wed) AM(1) Session a-5 at Room D Session c-1 at Room E Session n-1 at Room F Solid Rocket I(Failures, Performance, Mechanical Design Data Processing Aluminum Combustion) with AIAA SRTC Chairperson :H. Furuya (Tokyo Inst. of Tech) Chairperson :W. Takeuchi (Tokyo Univ.) Chairperson :W.A. Dick (Univ. of Illinois) S. Ozawa (JAXA) M. Tokunaga (Kanazawa Inst. of K. Hori (JAXA) Tech.) 09:00-9:20 2006-c-01 09:00-9:20 2006-a-22 Development of Rotor Mechanism Assembly for 09:00-9:20 2006-n-01 Survey of U.S. Small Launch Vehicle Failures Centrifuge Rotor Geometric Correction for Satellite Images Us- E. J. Tomei, I. Chang (The Aeroapace Corporation), M. Tabata (NEC TOSHIBA Space Systems, Ltd.), N. ing Mutual Information USA Sato, T. Nakano (JAXA), T. Murata (NEC TOSHIBA M. Motohashi, A. Iwasaki (Tokyo Univ. ), Japan Space Systems, Ltd.) et.al., Japan 09:20-9:40 2006-a-23 09:20-9:40 2006-n-02 Survey of Non-U.S. Small Launch Vehicle Fail- 09:20-9:40 2006-c-02 Extraction of Flood Area for Arsenic Soil Con- ures Bearing Failure Mode Test for Centrifuge Rotor tamination Analysis I. Chang, E. Joe Tomei (The Aerospace Corporation), T. Takegai (NEC TOSHIBA Space Systems, Ltd.), S. Masuda, M. Tokunaga (Kanazawa Institute of Tech- USA N. Sato, T. Nakano (JAXA), O. Kawamoto (NEC nology), Japan TOSHIBA Space Systems, Ltd.) et.al., Japan 09:40-10:00 2006-a-24 09:40-10:00 2006-n-03 Performance Reconstruction and Prediction 09:40-10:00 2006-c-03 Correction of Terra Spacecraft Attitude Fluc- Method for Space-Ignited Solid Rocket Motors Experimental study of an etching method as tuation using ASTER Image A. J. Posada (United States Air Force), S. A. Frolik a fabrication technique of cooling passages for Y. Teshima, A. Iwasaki (Tokyo Univ.), Japan (The Aerospace Corporation), USA combined cycle engine wall structure T. Saito, S. Ueda (JAXA), T. Yamamura (Tohoku 10:00-10:20 2006-n-04 10:00-10:20 2006-a-25 Univ.), Japan A digital mosaic processing for CORONA/KH- A Summary of Aluminum Combustion 4 imageries M. W. Beckstead (Brigham Young Univ.), USA 10:00-10:20 2006-c-04 T. Sugimura, S. Tanaka (RESTEC), S. Yamaguchi, Y. Fundamental Study on Cooling Structures of Nakayama (Nihon Univ.), Japan 10:20-10:40 2006-a-26 C/C Composite Material with a Metallic Tube Recent Progress in Modeling Solid Propellant M. Takegoshi, S. Ueda (JAXA), Japan 10:20-10:40 2006-n-05 Ingredients Using Detailed Kinetics Destriping MODIS Data by Facet Model and M. W. Beckstead, K. Pudappakkam (Brigham Young Histogram Matching Univ.), USA P. Rakwatin, W. Takeuchi, Y. Yasuoka (Tokyo Univ.), Japan June/7th (Wed) AM(1) Session s-5 at Room G Session h-1 at Room H Spacecraft Equipment Space Crafts and Microgravity Experiments

Chairperson :K. Tahara (Osaka Univ.) Chairperson :T. Nakamura (JAXA) H. Akahoshi (Kyushu Inst. of Tech.) O. Norberg (Swedish Space Corporation)

09:00-9:20 2006-s-23 09:00-9:20 2006-h-01 The dependence of degradation on ultraviolet light International Space Station applied research center pro- source for ground test of space materials motion program D. Kumagai, M. Iwata, M. Cho (Kyushu institute of tech- S. Sano, N. Kosihikawa, M. Sato, T. Kobayashi (JAXA), Japan nology), S. Kawakita (JAXA), Japan 09:20-9:40 2006-h-02 09:20-9:40 2006-s-24 JAXA’s Space Utilization Experiments Onboard the Physical properties evaluation of spacecraft glass Service Module of ISS materials and surface modiﬁcation C. Saito, M. Kato, K. Arakane, T. Nakamura (JAXA), Japan Y. Haraguchi, S. Hosoda, M. Iwata, K. Toyoda (Kyushu Institute of Technology) et.al., Japan 09:40-10:00 2006-h-03 STUDY OF POSSIBILITY TO USE THE PROGRESS 09:40-10:00 2006-s-25 VEHICLE FOR MICROGRAVITY RESEARCH DUR- Analysis of the reaction wheel disturbance with Air ING ITS AUTONOMOUS FLIGHT Floating Disturbance Detector M. Yu. Beliaev, E. V. Babkin, N. A. Bruykhanov, T. V. Y. Hatsutori (Tokyo Univ.), S. Taniwaki (Keio Univ.), Y. Matveeva (RSC ENERGIA) et.al., Russia Ohkami (JAXA), Japan 10:00-10:20 2006-h-04 10:00-10:20 2006-s-26 Micro-gravity test system using free-fall capsule from The Basic study of rolling mechanism for liquid high altitude balloon wheel using Lorentz force T. Hashimoto, S. Sawai, Y. Saito, H. Inatomi (JAXA) et.al., A. Iwakura (Tokai Univ.), Japan Japan

10:20-10:40 2006-h-05 Parameters Optimization of Attitude Determination System of Micro-core J. Sun, W. Zhao Sun, Y. Zhao (Harbin Institute of Technology), China

10:40-11:00 2006-h-06 The MASER Microgravity Missions and Sounding Rocket Operations at Esrange O. Norberg, S. Kemi, C. Lockowandt, K. Loth (Swedish Space Corporation) et.al., Sweden June/7th (Wed) AM(2) Session d-6 at Room B Session b-6 at Room C Session a-6 at Room D Mission Analysis Spacecraft and Plasma Interactions Solid Rocket II(Simulation, Gas Generator, Micro Thruster) with AIAA SRTC Chairperson :K. Yoshida (Tohoku Univ.) Chairperson :H. Usui (Kyoto Univ.) J. Foliard (CNES) Y. Takao (Oita National College Chairperson :I-Shih Chang (Aerospace Corp.) of Tech.) H. Nagata (Hokkaido Univ.) 10:50-11:10 2006-d-27 FORMATION FLYING OF MICROSATEL- 11:10-11:30 2006-b-26 10:50-11:10 2006-a-27 LITES INTO A GTO ORBIT Effect of substrate on sustained arc between High-fidelity Simulation of Solid Propellant F. Bonaventure, F. Raballand, L. Boulogne (EADS electrodes Rockets ASTRIUM), France K. Toyoda (Chiba Univ.), L. Levy (ONERA), Japan W. A. Dick, M. T. Heath, R. A Fiedler (Univ. of Illi- nois), USA 11:10-11:30 2006-d-28 11:30-11:50 2006-b-27 MSG-2 MISSION AND FLIGHT DYNAMICS GROUND-BASED EXPERIMENT OF HIGH- 11:10-11:30 2006-a-28 OPERATIONS VOLTAGE ELECTRIC BREAKDOWN OF SP Rocket Simulations at CSAR R. Mugellesi dow, A. Schuetz, D. Hocken SPACECRAFT INSULATOR SURFACE IN W. A. Dick, M. T. Heath (Univ. of Illinois), USA (ESOC/ESA), J. De juana gamo (SES ASTRA) AMBIENT PLASMA ENVIRONMENT et.al., Germany K. Horikawa, H. Tahara (Osaka Univ.), Japan 11:30-11:50 2006-a-29 University-Industry-Government Partnerships 11:30-11:50 2006-d-29 11:50-12:10 2006-b-28 in Solid Propellant Rocket Research HALO GEO Collocation Method Analysis Application of NuSPACE to the Spacecraft En- W. A. Dick (Univ. of Illinois), USA M. Molina, A. Perez, D. Cano (GMV SA), Spain vironment Analysis M. Okada (National Institute of Polar Research), H. 11:50-12:10 2006-a-30 11:50-12:10 2006-d-30 Usui, Y. Omura (Kyoto Univ.), H. O. Ueda (JAXA) Development of a Variable Flow Solid Propel- EUROSTAR 3000 : INCLINED ORBIT MIS- et.al., Japan lant Gas Generator using 3D Carbon/Carbon SION : LIFETIME OPTIMISATION AND Composite Cylindrical Valve PLASMIC PROPULSION IN FLIGHT EXPE- I. Yamaguchi, Y. Suzuki, S. Kanaizumi, M. Sugimine RIENCE (IHI Aerospace Co,.Ltd) et.al., Japan F. Raballand, T. Ha, A. Gicquel, F. Bonaventure (EADS ASTRIUM), France 12:10-12:30 2006-a-31 Ignition and combustion characteristics of Mi- 12:10-12:30 2006-d-31 cro Solid Rocket Array Thruster in Vacuum Lunar Transfer Orbit for SELENE H. Habu, S. Tokudome, K. Hori (JAXA), K. Kondo S. Matsumoto, Y. Takizawa, H. Konishi, M. Yamamoto (Tohoku Univ.) et.al., Japan (JAXA) et.al., Japan June/7th (Wed) AM(2) Session c-2 at Room E Session n-2 at Room F Session h-2 at Room H Facilities and Apparatus for Control & Identification Disaster Microgravity Experiments Chairperson :T. Iwata (AIST) Chairperson :S. Takeuchi (Hiroshima Inst. of Chairperson :T. Numazawa (National Institute H. Fukunaga (Tohoku Univ.) Tech.) for Material Science) M. Tokunaga (Kanazawa Inst. of I. Yoshizaki (JAXA) 10:30-10:50 2006-c-05 Tech.) Sound Attenuation to Minimize Transmission 11:10-11:30 2006-h-07 into Rocket Faring 10:50-11:10 2006-n-06 JAXA Life science experiment system for ISS K. Makihara (ISAS/JAXA), T. Miyakawa (Tokyo Feature Extraction of Volcanic Eruption Based S. Yano, M. Masukawa, A. Nagamatsu, W. Nishikawa Univ.), J. Onoda (ISAS/JAXA), Japan on Microwave Radiometer (AMSR-E) Observa- (JAXA) et.al., Japan tion 10:50-11:10 2006-c-06 T. Maeda (Tokyo Univ.), T. Takano (ISAS/JAXA), K. 11:30-11:50 2006-h-08 The Control of a Large Planar Structure Sus- Imaoka (EORC, JAXA), Japan JAXA Ryutai rack for material science re- pended by Multi-Tethers searches on Kibo K. Ishimura (Hokkaido Univ.), Japan 11:10-11:30 2006-n-07 M. Kunihiro, M. Keiji, K. Takuya, N. Tai (JAXA), A conceptual study of small satellite constella- Japan 11:10-11:30 2006-c-07 tion system for disaster and risk management Vibration analysis and vibratory control of A. Noda, M. Utashima, A. Tsuiki, A. Ogawa (JAXA), 11:50-12:10 2006-h-09 Space Solar Power Satellite Japan Development of continuous ADR system for M. Tanemura, H. A Fujii, Y. Koga, T. Watanabe weak gravity missions (Tokyo Metropolitan Univ.), Japan 11:30-11:50 2006-n-08 T. Numazawa, K. Kamiya (National Institute for Ma- JAXA Disaster/Crisis management program terials Science), P. Shirron, M. Dipirro (NASA God- 11:30-11:50 2006-c-08 T. Fukuda (JAXA), Japan dard Space Flight Center) et.al., Japan Thermal Model Identification of Multibeam Antenna System on WINDS Communication 11:50-12:10 2006-n-09 12:10-12:30 2006-h-10 Satellite Space-based Disaster Management High Definition Television Real-time Downkink S. Ozawa (JAXA), T. Kasuya, A. Kobayashi (NEC Y. Koizumi, S. Obi (NEC), K. Hiraishi (NEC System from International Space Station with TOSHIBA Space Systems, Ltd.), T. Maeda (JAXA) Aerospace Systems, Ltd), Japan Consumer Camcorder et.al., Japan J. Yoshikawa, M. Keiji, M. Kunihiro, N. Tai (JAXA) et.al., Japan 11:50-12:10 2006-c-09 Adaptive Noise Filtering with Variable Struc- tural Parameters for Flexible Structures A. Senba, H. Furuya (Tokyo Institute of Technology), Japan June/7th (Wed) PM(1) Session o-2-2 at Room A Session d-7 at Room B Session b-7 at Room C Explorations of the Fronteer Attitude Determination Ion Thrusters (2)

Chairperson :D. Senske (NASA/JPL) Chairperson :J. O’Donnel (NASA/GSFC) Chairperson :A. Ando (Tohoku Univ.) H. Yano (JAXA/ISAS) T. Hashimoto (JAXA/ISAS) T. Ozaki (Mitsubishi Electric co.)

14:30-15:00 2006-o-2-07v 14:30-14:50 2006-d-32 14:40-15:00 2006-b-29 HAYABUSA - A New Solar System Cruiser - Ground-Based Precision Attitude Determina- Effects of magnetic field and antenna config- J. Kawaguchi (JAXA), Japan tion for the Advanced Land Observing Satellite urations on thrust performance of microwave (ALOS) discharge ion engines with multi mono-pole an- 15:00-15:30 2006-o-2-08v T. Iwata, T. Iwata (JAXA), M. Uo, T. Kawahara tenna system Rosetta Mission (NTSpace) et.al., Japan N. Munesada, K. Shinyashiki, M. Miyoshi, T. G. Schwehm (ESA/ESTEC), Netherlands Miyamoto (Kyushu Univ.) et.al., Japan 14:50-15:10 2006-d-33 15:30-16:00 2006-o-2-09v Orbit/Attitude Determination for MTSAT 15:00-15:20 2006-b-30 MESSENGER OPERATIONS AND CRITI- through automated Landmark and Earth Edge Magnetic Field Configuration Effects on CAL EVENTS Detection Thruster Performance of Miniature Microwave J. C Leary (Johns Hopkins Univ. Applied Physics Lab- M. D Milnes (LogicaCMG), UK Discharge Ion Engine oratory), R. W. Farquhar, M. E. Holdridge, R. E. Gold T. Chikaoka, S. Kondou, N. Yamamoto, H. Nakashima (Johns Hopkins Univ. Applied Physics Laboratory) 15:10-15:30 2006-d-34 (Kyushu Univ.), Japan et.al., USA Pleiades HR: On-ground attitude estimation J. Montel (CNES), France 15:20-15:40 2006-b-31 16:00-16:30 2006-o-2-10v Numerical Analysis of Microwave Discharge BepiColombo - The Mercury Challenge 15:30-15:50 2006-d-35 Plasma Source using Antennas for Propulsion J. Van casteren, J. Benkhoff, R. Carli, B. Gramkow TRMM On-Orbit Performance Reassessed Af- T. Kasa, T. Kanagawa, K. Izumi, H. Masui (Kyushu (ESA/ESTEC) et.al., Netherlands ter Control Change Univ.) et.al., Japan S. Bilanow (SAIC), S. Slojkowski (a.i. solutions, Inc), 16:30-17:00 2006-o-2-11v USA 15:40-16:00 2006-b-32 New Horizons, the first mission to the third Performance Improvement of the Microwave zone of the Solar System 15:50-16:10 2006-d-36 Discharge Ion Thruster µ20 G. Fountain (Johns Hopkins Univ. Applied Physics Calibration of Gimbaled Platforms: The Solar T. Nakai (Tokyo Univ.), K. Nishiyama, H. Kuninaka Laboratory), USA Dynamics Observatory High Gain Antennas (JAXA), Japan J. A Hashmall (a.i.solutions, Inc.), USA 16:00-16:20 2006-b-33 16:10-16:30 2006-d-37 Experimental Demonstration of Microwave Dis- Attitude Change Rate Estimation from Star charge Ion Engine with 10,000sec Isp Sensor Images in Frequency Domain H. Hayashi, M. Cho (Kyushu Institute of Technology), K. Nishiguchi, S. Yoshikawa (Mitsubishi Electric Cor- H. Kuninaka (ISAS/JAXA), Japan poration), Japan June/7th (Wed) PM(1) Session a-7 at Room D Session c-3 at Room E Session n-3 at Room F Thruster Membrane Structures GPS, Fusion

Chairperson :E.J. Tomei (Aerospace Corp.) Chairperson :Y. Miyazaki (Nihon Univ.) Chairperson :M. Nagai (Tokyo Univ.) S. Tomioka (JAXA) K. Ishimura (Hokkaido Univ.) M. Tokunaga (Kanazawa Inst. of Tech.) 14:30-14:50 2006-a-32 14:30-14:50 2006-c-10 Propulsion System on Hydrogen Peroxide Mono- Construction of Solar Power Satellites Using 14:30-14:50 2006-n-10 Propellant for Panel ExTension SATellite (PETSAT) Small Satellites and Large-scale Deployable Universal Map by Collaboration of Remote H. Sahara, S. Nakasuka, Y. Sugawara (Tokyo Univ.), C. Structures Sensing, GPS and GIS Kobayashi (SOHLA), Japan T. Iwata, H. Murakami (AIST), Japan M. Shikada, S. Shimano (Kanazawa Institute of Tech- nology), A. Okuno (Kokusai Kogyo Co.,LTD.), Japan 14:50-15:10 2006-a-33 14:50-15:10 2006-c-11 Experimental Results of Precision Thrust Controlled Particle System Approximation for Dynamic 14:50-15:10 2006-n-11 Supersonic Cold-Gas and Warm-Gas Microthruster Behavior of Membranes Improvements on Ionospheric Parameters Op- G. Manzoni (Microspace), S. Heisig, S. Matsumoto, R. Maeda M. Natori (ISAS/JAXA), F. Nakamura (Tokyo Univ.), timized by Regional Limitation (AIST - MEMS Group), Italy N. Okuizumi (ISAS/JAXA), Japan M. Sato (Space Engineering Development Co.,Ltd.), M. Sawabe, I. Kawano, S. Kogure (JAXA) et.al., Japan 15:10-15:30 2006-a-34 15:10-15:30 2006-c-12 Flow Simulation Of Film-Cooled Bipropellant Development of Inflatable Truss Structure for 15:10-15:30 2006-n-12 Thruster Space Solar Power System Robust Trajectory Tracking by Combining K. Ohminami (Sokendai Univ. / ISAS), K. T Uesugi, H. K. Anma, T. Kozasa, A. Tukahara, F. Takeda (MHI) GPS/IMU and Continual CCD Images Ogawa (ISAS/JAXA), Japan et.al., Japan M. Nagai, R. Shibasaki (Tokyo Univ.), Japan 15:30-15:50 2006-a-35 15:30-15:50 2006-c-13 DESIGN, DEVELOPMENT AND MANUFACTUR- 15:30-15:50 2006-n-13 Deployment Analysis on Membrane Structures ING OF A HIGH PERFORMANCE GREEN PRO- Analysis on Topographical Aspect in Urban Combined with Inflatable Tubes PELLANT THRUSTER USING ADN Growth by Combining Satellite Remote Sens- N. Kishimoto (ISAS/JAXA), M. Hashimoto (Tokyo N. Boman, R. Nedar, U. Palmnas (Volvo Aero Corpora- ing Images with DEM Univ.), Y. Miyazaki (Nihon Univ.), M. Natori tion/ECAPS), K. Anflo (Swedish Space Corporation/ECAPS,) S. Takeuchi, Y. Oguro (Hiroshima Institute of Tech- (ISAS/JAXA), Japan et.al., Sweden nology(HIT)), Japan

15:50-16:10 2006-a-36 15:50-16:10 2006-c-14 Evaluation on Hydrogen Peroxide Decomposition with Wrinkling and Reﬂection Characteristics of Discharge Plasma Membrane Solar Reﬂectors of REIMEI Space- J. Aoyagi, Y. Kotake (Tokyo Metropolitan Institute of Tech- craft nology), H. Takegahara, K. Kuriki (Tokyo Metropolitan N. Okuizumi, H. Saito, K. Tanaka, K. Higuchi Univ.), Japan (ISAS/JAXA), Japan

16:10-16:30 2006-a-37 16:10-16:30 2006-c-15 COMBUSTION CHARACTERISTICS OF HAN- A Concept of Retractable Inﬂatable Tubes BASED LIQUID MONOPROPELLANT H. Furuya, M. Nakahara (Tokyo Institute of Technol- T. Katsumi (Tokai Univ.), H. Shibamoto (Hosoya Kako. CO. ogy), Japan LTD.), K. Hori (ISAS/JAXA), Japan June/7th (Wed) PM(1) Session r-2-5 at Room G Session h-3 at Room H Space Environment Simulation Fluid and Bubble Dynamics

Chairperson :Y. Kimoto (JAXA) Chairperson :M. Watanabe (Gakushuin Univ.) M. Akioka (NICT) S. Matsumoto (JAXA)

14:30-14:50 2006-r-2-20 14:30-14:50 2006-h-11 Development of MUSCAT (Multi-Utility Large-amplitude Oscillation of Droplet Levi- Spacecraft Charging Analysis Tool): Part of tated by Electrostatic Force GUI Spacecraft Modeling S. Awazu (Univ. of Tsukuba), S. Matsumoto, T. K. Jeong Ho, K. Jeong Ho, S. Hatta, T. Muranaka Ishikawa, S. Yoda (JAXA) et.al., Japan (Kyushu Institute of Technology) et.al., Japan 14:50-15:10 2006-h-27 14:50-15:10 2006-r-2-21 Synergistic Effect of Hyperthermal Atomic Midterm Development Report of Multi-Utility Oxygen Beam and Vacuum Ultraviolet Radia- Spacecraft Charging Analysis Tool (MUSCAT) tion Exposures on the Mechanical Degradation T. Muranaka, S. Hosoda, J. Kim, S. Hatta ((La- of High-Modulus Aramid Fibers SEINE), Kyushu Institute of Technol) et.al., Japan L. Ghosh, H. Kinoshita, N. Ohmae (Kobe Univ.), Japan 15:10-15:30 2006-r-2-22 Toward the Radiation Belt Forecast in Japan 15:10-15:30 2006-h-13 T. Obara (NICT), K. Koga, T. Goka (JAXA), Japan Multiple bubble oscillation under ultrasonic vibration 15:30-15:50 2006-r-2-23 T. Kojo, I. Ueno (Tokyo Univ. of Science), Japan Experimental Demonstration on Remote Sens- ing of Atomic Oxygen in the Upper Atmosphere 15:30-15:50 2006-h-14 using Artificial Ion Beam Existing length of precursor film ahead advanc- Y. Sakamoto (Tokyo Univ.), H. Kuninaka (JAXA), ing droplet on solid substrate Japan T. Watanabe, I. Ueno (Tokyo Univ. of Science), Japan June/7th (Wed) PM(2) Session d-8 at Room B Session b-8 at Room C Session a-8 at Room D Formation Flight New Propulsion System (Hybrid Hall Thrusters Propulsion System, Propellant) Chairperson :T. Iwata (JAXA/IAT) Chairperson :K. Nishiyama (JAXA) Chairperson :S.A. Frolik (Aerospace Corp.) T. Hashimoto (JAXA/ISAS) N. Yamamoto (Kyushu Univ.) H. Taguchi (JAXA)

16:40-17:00 2006-d-38 16:30-16:50 2006-b-34 16:40-17:00 2006-a-38 CONFIGURATION, ORBIT DESIGN OF INTER- Development Status of High Power Xenon Hall LiH as Fuel for Aerospace Propulsion FEROMETRIC SAR FORMATION BASED ON Thruster of MELCO D. Simone, C. Bruno (Univ. of Rome ”La Sapienza”), MEAN ELEMENTS T. Ozaki, Y. Inanaga, T. Nakagawa, Y. Kasai Italy X. Cao, J. Zhang, F. Wang (Harbin Institute of Technology), (MELCO), Japan China 17:00-17:20 2006-a-39 16:50-17:10 2006-b-35 Rocket Engine with Film/Trimming 17:00-17:20 2006-d-39 Thrust Performance of a 1-kW class SPT-type V. Leudiere, P. Fortunier (CNES), France An Optimal Formation Design Method for dual- Hall thruster Satellite Formation Y. Saeki, S. Yuge, H. Tahara (Osaka University), Japan 17:20-17:40 2006-a-40 X. Cao, B. Wu, D. He, F. Liu (Harbin institute of technology), Development of CEES Rocket using Liquid Ni- China 17:10-17:30 2006-b-36 trogen and Water Inﬂuence of magnetic ﬁeld topography and dis- T. Hiejima, K. Maruyama, H. Azuma (Osaka Prefec- 17:20-17:40 2006-d-40 charge channel structure on performance of an ture Univ.), O. Kawanami (Univ. of Hyogo), Japan Numerical Approach for Designing and Deploying anode-layer Hall thruster Satellite Formations S. Yuge, H. Tahara (Osaka Univ.), Japan 17:40-18:00 2006-a-41 P. Williams, P. Trivailo (RMIT Univ.), Australia COMBUSTION MECHANISM OF TETRA- 17:30-17:50 2006-b-37 OL Glycidyl Azide Polymer 17:40-18:00 2006-d-41 The Fluctuation of Electron Density Distribu- Y. Wada (Tokai Univ.), M. Nishioka (Univ. of On Elliptic Formation Control of Spinning Tethered tion Inside a Hollow Anode ina an Anode-layer Tsukuba), K. Hori (ISAS/JAXA), Japan Formation Flying Hall Thruster K. Nakaya (JAXA/ISAS), S. Matunaga (Tokyo Institute of S. Yokota, K. Komurasaki, Y. Arakawa (Tokyo Univ.), Technology), Japan Japan

18:00-18:20 2006-d-42 17:50-18:10 2006-b-38 Satellite Formation Keeping Using Robust Con- Eﬀect of Magnetic Field Conﬁguration in Hall strained MPC in Elliptical Orbits Thrusters with Circular Cross-sectional Dis- B. Wu (Harbin institute of technology), X. Cao (Harbin insti- charge Chambers tute of technology), G. Wu (Harbin institute of technology ), A. Shirasaki, H. Tahara (Osaka Univ.), Japan China

18:20-18:40 2006-d-43 Proximity Maneuver and Obstacle Avoidance Control Using Potential Function Guidance Method Y. Shimada, K. Uchiyama, Y. Yokota (Nihon Univ.), G. Radice (Univ. of Glasgow, ) et.al., Japan June/7th (Wed) PM(2) Session c-4 at Room E Session n-4 at Room F Session r-2-6 at Room G Analysis & Simulation Sensor, Observation System Space Environment Eﬀect on Space Material

Chairperson :N. Hu (Tohoku Univ.) Chairperson :M. Shikada (Kanazawa Inst. of Chairperson :E.A. Taylor (ISO/TC20/SC14/ N. Okuizumi (JAXA) Tech) ODCWG) M. Tokunaga (Kanazawa Inst. of T. Goka (JAXA) 16:40-17:00 2006-c-16 Tech) Study on 3-dimensional finite element analysis 16:00-16:20 2006-r-2-24 for the insulation tile considering heat radiation 16:00-16:20 2006-n-14 Damage Evaluation of Solar Panel Impacted by Debris and conduction coupling Satellite-borne Small Compound Camera Con- Y. Machida, Y. Akahoshi, S. Fukushige (Kyushu Institute of M. Takagaki (Institute of Industrial Science, Tokyo figuration for High-Resolution Earth Images Technology), T. Hanada (Kyushu Univ.) et.al., Japan Univ.), Y. Sato, T. Nakamura, T. Kai (JAXA), Japan and its Data Processing A. Enokuchi, S. Nakasuka (Tokyo Univ.), Japan 16:20-16:40 2006-r-2-25 17:00-17:20 2006-c-17 Hypervelocity Impact Test to Solar Array for Evalua- P-finite elements and an analysis system for a 16:20-16:40 2006-n-15 tion of Possibility of Sustained Arc simple numerical model of thermal structures Camera Pointing Mechanism for a Two- S. Fukushige, Y. Akahoshi, K. Watanabe, T. Harano (Kyushu K. Takasaki, T. Kai (JAXA), S. Arashi (JST), Japan dimensional Spectroscopic Observation of the Institute of Technology) et.al., Japan Vapor Transfer with an S-520 Sounding Rocket 17:20-17:40 2006-c-18 Y. Shoji, K. Yoshida, H. Nakanishi, J. Shimasaki (To- 16:40-17:00 2006-r-2-26 A Novel Non-equilibrium Molecular Dynam- hoku Univ.) et.al., Japan SPACE ENVIRONMENT EFFECT OF MPAC & ics Simulation of the Thermal Conductivity of SEED MISSION IN ISS Crystals Ar Film 16:40-17:00 2006-n-16 Y. Kimoto, T. Inoue, K. Yano, J. Ishizawa (JAXA) et.al., B. Shao, Z. Sun, G. Wu (the Research Institute of New development of infrared detectors for Japan Satellite Technology, Harbin Institute of Technology), space activity at Sofradir China P. Chorier, M. Vuillermet, P. Tribolet (Sofradir), 17:00-17:20 2006-r-2-27 France Passive Measurement of Dust Particles on the ISS 17:40-18:00 2006-c-19 (MPAC): Third Report on Aerogel Dust Collectors Molecular Dynamics Simulation on The out-of 17:00-17:20 2006-n-17 Y. Kitazawa (IHI), M. J. Neish (AES), T. Noguchi (Ibaraki Plane Thermal Conductivity of Single-Crystal ASSIMILATION of IMAGES for GEOPHYSI- Univ.), I. Yamagata (JAXA) et.al., Japan Carbon Thin Films CAL FLUIDS G. Wu, X. Kong, Z. Sun, D. Zhao (Harbin Institute F. L. Le dimet (Universite Joseph Fourier and INRIA), 17:20-17:40 2006-r-2-28 Technology Research Center of Satellite Technology), France Evaluation and Analysis of the Second-Retrieved China Unit of the Space Environment Exposure Device (SM/MPAC&SEED) J. Ishizawa, I. Yamagata, K. Yugo, N. Baba (JAXA) et.al., Japan

17:40-18:00 2006-r-2-29 Characterization of lubricative coating after exposure test in orbit M. Tosa, A. Kasahara, M. Goto (NIMS), T. Inoue (JAXA) et.al., Japan June/7th (Wed) PM(2) Session h-4 at Room H Marangoni Convection

Chairperson :I. Ueno (Tokyo Univ. of Science) K. Kinoshita (JAXA)

16:00-16:20 2006-h-15 Development of Flow Visualization System by Ultrasonic wave for Thermocapillary Convec- tion of Low Prandtl Number Fluid H. Sasaki (Chiba Institute of Technology), S. Mat- sumoto, T. Mashiko, H. Ohira (JAXA) et.al., Japan

16:20-16:40 2006-h-16 Initial Results from a Ground Experiment for Elucidating Marangoni Convection T. Mashiko, S. Matsumoto, H. Ohira (JAXA), Y. Kamotani (Case Western Reserve Univ.) et.al., Japan

16:40-17:00 2006-h-17 Numerical analysis of thermocapillary ﬂows in a cylindrical container H. Ohira, S. Matsumoto, T. Mashiko, S. Yoda (JAXA) et.al., Japan

17:00-17:20 2006-h-18 Reconstruction of relative particle behavior in formation and collapse processes of particle ac- cumulation structure (PAS) in half-zone liquid bridge by 3-D PTV I. Ueno, Y. Abe, K. Noguchi, S. Tanaka (Tokyo Univ. of Science) et.al., Japan June/7th (Wed) PM(3) Session n-5 at Room F Session h-5 at Room H Levitation Techniques and their Satellite System Applications Chairperson :M. Tokunaga (Kanazawa Inst. of Tech.) Chairperson :T. Ishikawa (JAXA) W. Takeuchi (Kanazawa Inst. of Tech.) P-F. Paradis (JAXA)

17:30-17:50 2006-n-18 17:30-17:50 2006-h-19 SIDUSS: SAR Interferometry Dual Satellite System Electrostatic Levitation for Space and Ground- T. Kodama (JAXA), Japan based Research: JAXA’s Innovations P. Paradis, T. Ishikawa (JAXA), Japan 17:50-18:10 2006-n-19 ELMOS: Electric and Magnetic ﬁeld Observation 17:50-18:10 2006-h-20 Satellite Development of non-contact electrical resistiv- T. Kodama (JAXA), Japan ity measurement technique in an electrostatic levitator 18:10-18:30 2006-n-20 T. Ishikawa (JAXA), N. Koike (Chiba Institute of High Resolution Extensible Telescope for University Technology), A. Ishikura (Gakushuin Univ.), P. Par- of Tokyo’s Remote Sensing Nano-Satellite adis (JAXA), Japan N. Miyamura, T. Eishima, Y. Nakamura, R. Funase (Tokyo Univ.) et.al., Japan 18:10-18:30 2006-h-21 Thermophysical property measurement of liquid platinum with an electrostatic levitator N. Koike (Chiba Institute of Technology), T. Ishikawa (JAXA), A. Ishikura (Gakushuin Univ.), P. Francois Paradis (JAXA) et.al., Japan

18:30-18:50 2006-h-22 Precise density measurement for electromag- netically levitated liquid combined with the surface oscillation analysis M. Adachi, Y. Miura, K. Higuchi, A. Mizuno (Gakushuin Univ.) et.al., Japan June/8th (Thu) AM(1) Session d-9 at Room B Session b-9 at Room C Session a-9 at Room D Interplanetary Trajectory Design MPD Thrusters and Electromagnetic Plasma Air Breathing Engine I (Turbojet, Accelerators Cycle, Combustion, Fluid Dynamics) Chairperson :J. Fertig (ESA/ESOC) Chairperson :H. Kuninaka (JAXA) Chairperson :TBD J. Kawaguchi (JAXA/ISAS) Y. Ohkawa (JAXA) S. Tomioka (JAXA) 09:00-9:20 2006-b-39 09:00-9:20 2006-d-44 09:00-9:20 2006-a-42 Performance Characterization for Various Electrode Study on Optimal Transfer Trajectories of the Combustion Tests in a Small Hydrogen- Geometries in an Magneto-Plasma-Dynamic Thruster Solar Polar Region Explorers Using Electric Fueled Reversed-Flow Combustor for Hyper- D. Nakata (Tokyo Univ.), K. Toki (Tokyo Univ. of Agriculture Propulsion. sonic Flight Experiments and Technology), I. Funaki, Y. Shimizu (JAXA/ISAS) et.al., R. Maruyama, S. Ueno (Yokohama National Univ.), K. Okai, K. Shimodaira, Y. Kurosawa, H. Taguchi Japan Japan (JAXA) et.al., Japan 09:20-9:40 2006-b-40 09:20-9:40 2006-d-45 Plasma Acceleration by Applying a Magnetic Nozzle 09:20-9:40 2006-a-43 Advances in Global Optimisation for space train a Quasi-Steady MPD Arcjet Design Study on Pre-Cooled Turbojet Engines jectory design Y. Kagaya, H. Tahara, S. Kawano (Osaka Univ.), Japan for Hypersonic Airplanes D. Izzo (ESA), Netherlands H. Taguchi, T. Kojima, K. Fujita, H. Kobayashi 09:40-10:00 2006-b-41 (JAXA) et.al., Japan Performance of an MPD Thruster with a Laval-type 09:40-10:00 2006-d-46 Magnetic Nozzle Low-Thrust Gravity Assist Interplanetary Tra- 09:40-10:00 2006-a-44 K. Hattori, T. Komagome, A. Ando, M. Inutake (Tohoku jectory Optimization Using Evolutionary Neu- A Comparison of Precooled Expander Cycle Jet Univ.), Japan rocontrollers Engines for Space Planes I. Carnelli (ESA), B. Dachwald (DLR), Netherlands 10:00-10:20 2006-b-42 T. Sato, H. Kobayashi (JAXA), M. Hempsell (Univ. of Magnetic Nozzle Acceleration in a Fast-ﬂowing Plasma Bristol), Japan 10:00-10:20 2006-d-48 for the VASIMR Thruster Study on the Lunar Approach Strategies Toler- A. Ando, M. Shibata, Y. Kasashima, K. Hattori (Tohoku 10:00-10:20 2006-a-45 ant of Lunar Orbit Injection Failure Univ.) et.al., Japan Evaluate of Boundary Layer Introduced Y. Kawakatsu (JAXA/ISAS), M. Yamamoto Streamwise Vortices in Scramjet Combustor 10:20-10:40 2006-b-43 (JAXA/ISTA), J. Kawaguchi (JAXA/ISAS), Japan Using Quantitative Schlieren Method A Performance Study of MHD Accelerator with S. Sakaue, T. Arai, T. Morisaki (Osaka Prefecture Chemical Nonequilibrium Air Plasma Univ.), T. Sunami (JAXA) et.al., Japan T. Hardianto, N. Sakamoto, J. Kondo, N. Harada (Nagaoka Univ. of Technology), Japan 10:40-11:00 2006-b-44 Eﬃciency Analysis of a Diagonal MHD Accelerator M. Anwari (Univ. of Tanjungpura), N. Harada (Nagaoka Univ. of Technology), Indonesia 11:00-11:20 2006-b-45 Study of Electrodeless Plasma Production and Elec- tromagnetic Acceleration K. Toki (Tokyo Univ. of Agriculture and Technology), S. Shi- nohara (Kyushu Univ.), T. Tanikawa (Tokai Univ.), T. Hada (Kyushu Univ.) et.al., Japan June/8th (Thu) AM(1) Session c-5 at Room E Session f-1 at Room F Session r-3-1 at Room G Environment Test Small Satellite (1) Space Law and Policy

Chairperson :T. Ogasawara (JAXA) Chairperson :K. Ui (JAXA/ISAS) Chairperson :T. Kosuge (DHW) T. Yokozeki (JAXA) S. Hagino (NEC TOSHIBA M. Sato (JAXA) Space Systems) 09:00-9:20 2006-c-20 10:50-11:10 2006-r-3-01 IN ORBIT TEST RESULT OF SMART RADI- 09:00-9:20 2006-f-01 Study on Legal Implication of JAXAs Long ATION DEVICE On-orbit Performance of the REIMEI Satellite Term Vision (JAXA 2005) Y. Nakamura, A. Okamoto (NEC TOSHIBA with Integrated Computer System and Intro- S. Morikawa (JAXA), Japan Space Systems, Ltd.), S. Tachikawa, A. Ohnishi duction to Its Flexible Operation (ISAS/JAXA) et.al., Japan S. Fukuda, T. Mizuno, S. Sakai, Y. Fukushima 11:10-11:30 2006-r-3-02 (ISAS/JAXA) et.al., Japan Survey on Patent Applications for Medical 09:20-9:40 2006-c-21 Treatment on Space Engineering Field Bearing Test for Mirror Support Mechanism of 09:20-9:40 2006-f-02 Y. Tomioka, A. Naoki, K. Kakehi (Office Tomioka), Space Infrared Telescope - Evaluation of Hy- Development and On-Orbit Results of Minia- I. Nakajima (Tokai Univ. School of Medicine) et.al., brid Ball Bearing Characteristics in Cryogenic ture Space GPS Receiver by means of Japan Environment - Automobile-Navigation Technology M. Haruna, M. Tabata, T. Oshima (MITSUBISHI H. Saito, T. Mizuno, K. Kawahara, K. Shinkai 11:30-11:50 2006-r-3-03 ELECTRIC CORPORATION), T. Onaka (Tokyo (ISAS/JAXA) et.al., Japan GNSS AND SPACE SECURITY Univ.) et.al., Japan Y. Takaya-umehara (IDEST, Paris XI Univ.), Japan 09:40-10:00 2006-f-03 09:40-10:00 2006-c-22 Development and On-Orbit Results of Solar SM/SEED FLIGHT EXPERIMENTAL RE- Concentrated Paddles with Thin Film Reflec- SULTS ON MOLYBDENUM DISULSIDE- tor BASED SOLID LUBRICANTS H. Saito, N. Okuizumi, K. Tanaka, M. Mita M. Tagawa, M. Tagawa, H. Asada, K. Yokota (Kobe (ISAS/JAXA) et.al., Japan Univ.) et.al., Japan 10:00-10:20 2006-f-04 10:00-10:20 2006-c-23 The Flight and Ground Test Data of the Comparative Study of Polyimide and FEP on Lithium-Ion Secondary Battery of ’REIMEI’ the Simultaneous Exposure Effects of Atomic Y. Sone, M. Uno (JAXA), Y. Takeda (Advanced En- Oxygen and Ultraviolet gineering Services), K. Tanaka (JAXA) et.al., Japan K. Yokota, K. Yokota (Kobe Univ.), A. Okamoto (Technology Research Institute of Osaka Prefecture), 10:20-10:40 2006-f-05 M. Tagawa (Kobe Univ.), Japan Magnetic Moment Measurement and Demagne- tization of Piggyback Satellite H. Shirasawa, H. Takahashi, F. Tohyama (Tokai Univ.), T. Mizuno (JAXA) et.al., Japan June/8th (Thu) AM(1) Session k-1 at Room H Lunar & Martian Exploration (1)

Chairperson :H. akiyama (Akita Univ.) A. Toigo (Kobe Univ.)

09:00-9:20 2006-k-01 Low energy charged particle measurement by Japanese lunar orbiter SELENE Y. Saito, S. Yokota, K. Asamura, T. Mukai (ISAS/JAXA), Japan

09:20-9:40 2006-k-02 Gamma-Ray Observation to Globally Map Chemical Composition of the Lunar Surface by SELENE O. Okudaira, N. Hasebe, T. Miyachi, N. Yamashita (Waseda Univ.) et.al., Japan

09:40-10:00 2006-k-03 Simulation toward Development of a New Gamma-ray Imaging Spectrometer M. Mimura, M. Mimura, N. Hasebe, T. Hosojima (Waseda Univ.) et.al., Japan

10:00-10:20 2006-k-04 Improvement of the Lunar Gravity Field Map using Three Orbiter of SELENE T. Iwata (JAXA), N. Namiki (Kyushu Univ.), H. Noda, H. Hanada (National Astronomical Observa- tory) et.al., Japan

10:20-10:40 2006-k-05 Same-Beam Differential VLBI Using Two Satel- lites of SELENE Q. Liu, Q. Liu, F. Kikuchi, K. Matsumoto (National Astronomical Observatory of Japan) et.al., Japan June/8th (Thu) AM(2) Session d-10 at Room B Session b-10 at Room C Session a-10 at Room D Magneto Plasma Sails and Deep Space Navigation Electrodynamic Tethers Air Breathing Engine II(Scramjet) Chairperson :L.A. Changahuala (NASA/JPL) Chairperson :K. Toki (Tokyo Univ. of Chairperson :C. Bruno (Univ. of Rome) M. Horii (JAXA/OSFO) Agriculture and Tech.) T. Sato (JAXA) M. Okada (National Inst. of 10:50-11:10 2006-d-49 Polar Research) 10:30-10:50 2006-a-46 A Global Approach to Delta Differential One- Transition of Combustion Modes in a Scramjet way Range 11:30-11:50 2006-b-46 Engine J. S Border (JPL), USA Innovative Interplanetary Transportation Sys- T. Kouchi, T. Mitani, S. Tomioka, S. Ueda (JAXA), tem Using Electrodynamic Tether and Mag- Japan 11:10-11:30 2006-d-50 netic Coil (Mag-Tether) Use of Very Long Baseline Array Interferomet- Y. Yamagiwa, S. Watanabe, K. Katanagi, H. Otsu 10:50-11:10 2006-a-47 ric Data for Spacecraft Navigation (Shizuoka Univ.), Japan Scramjet Characteristics at Hypervelocity Con- T. J Martin-mur, P. Antreasian, J. Border (JPL, Cal- dition over Mach 10 Flight - Application of a ifornia Institute of Technology), J. Benson (National 11:50-12:10 2006-b-47 Diverging Combustor Radio Astronomy Observatory) et.al., USA MHD Analysis of Magnetosphere around Mag- M. Takahashi, T. Komuro, K. Sato, M. Kodera (JAXA neto Plasma Sail Kakuda Space Center) et.al., Japan 11:30-11:50 2006-d-51 H. Nishida (Tokyo Univ.), H. Ogawa, I. Funaki, Y. Nonlinear Consider Covariance Techniques for Inatani (ISAS/JAXA), Japan 11:10-11:30 2006-a-48 Interplanetary Aeromaneuver Navigation, Us- Performance Comparison of Combined Fuel ing a Sigma-point Filter Formulation 12:10-12:30 2006-b-48 Injection Methods in a Staged-Combustion M. E Lisano (JPL, California Institute of Technology), Numerical Simulation of Magneto Plasma Sail Scramjet Engine USA by Using Three-Dimensional Hybrid Code S. Ueda, S. Tomioka, T. Kouchi, K. Kobayashi (JAXA) Y. Kajimura, Y. Kajimura, D. Shinohara, K. Noda et.al., Japan 11:50-12:10 2006-d-52 (Kyushu Univ.) et.al., Japan Rosetta navigation at its first Earth swing-by 11:30-11:50 2006-a-49 T. A Morley, F. Budnik (ESA/ESOC), Germany 12:30-12:50 2006-b-49 Numerical Simulation of Scramjet Engine at Simulation of Magnetic Field Inflation by In- Hypervelocity Conditions 12:10-12:30 2006-d-53 jected Plasma in Magneto Plasma Sail by Using M. Kodera, M. Takahashi, K. Itoh (JAXA), Japan Stardust and Genesis: Interplanetary Sample Three-Dimensional Hybrid Code Return Missions and Flight Experience K. Noda, Y. Kajimura, D. Shinohara, H. Nakashima K. Williams, G. Carlisle (JPL/Caltech), USA (Kyushu Univ.), Japan June/8th (Thu) AM(2) Session c-6 at Room E Session f-2 at Room F Session k-2 at Room H Composites Small Satellite (2) Lunar & Martian Exploration (2)

Chairperson :L. Scatteia (CIRA) Chairperson :H. Sato (JAXA) Chairperson :T. Iwata (JAXA) Y. Okabe (Tokyo Univ.) T. Mizuno (JAXA) R.K. Fisackerty (ESA)

10:30-10:50 2006-c-24 10:50-11:10 2006-f-06 10:50-11:10 2006-k-06 Application of Composite Sandwich Structure Micro-platform of spacecraft-GC Design and Test of Altitude Measurement for to Payload Fairing G. Xiao-chun Gong, X. Guo-dong Xu, W. Feng Wang, Planetary Landing Radar C. Kong, J. Lee, Y. Jang, Y. Yi (Korea Aerospace W. Guo-qiang Wu (Harbin Institute of Technology), T. Sakai, S. Fukuda (JAXA), T. Sato (Tokyo Univ. of Research Institute) et.al., Republic of Korea China Science), H. Tomita (HIM Technology) et.al., Japan

10:50-11:10 2006-c-25 11:10-11:30 2006-f-07 11:10-11:30 2006-k-07 Boss Design of Aluminum Liner for Filament- Technology Demonstration Results on Univer- Present status of the development of the Wound Composite Pressure Vessel Considering sity of Tokyo’s Pico-Satellite LUNAR-A penetrator Weight Reduction R. Funase, Y. Nakamura, M. Nagai, N. Sako (Tokyo S. Tanaka, H. Shiraishi, A. Fujimura, K. Uesugi J. Hoon Yoon, J. Sung Park, Y. Soon Jang, Y. Moo Yi Univ.) et.al., Japan (ISAS/JAXA), Japan (KARI), Republic of Korea 11:30-11:50 2006-f-08 11:30-11:50 2006-k-08 11:10-11:30 2006-c-26 Development and Flight Report of Pico- Characteristics of the seismometer onboard Characterization of Mechanical Properties of Satellite Cute-1.7 + APD LUNAR-A penetrator Polymer Films for Cryogenic Composite Tank N. Miyashita, N. Miyashita, K. Konoue, K. Omagari R. Yamada (ISAS/JAXA), I. Yamada (Nagoya Univ.), Application (Tokyo Institute of Technology) et.al., Japan H. Shiraishi, S. Tanaka (ISAS/JAXA) et.al., Japan T. Yokozeki (IAT/JAXA), T. Yamagata (Aoyama Gakuin Univ.), T. Ogasawara (Institute of Aerospace 11:50-12:10 2006-f-09 11:50-12:10 2006-k-09 Technology, JAXA), Japan About Nano-satellite for Infrared Astrometry Terramechanics-Based Analysis on Slope (Nano-JASMINE) Project Traversability for a Planetary Exploration 11:30-11:50 2006-c-27 N. Sako, Y. Hatsutori, T. Tanaka, S. Nakasuka (Tokyo Rover Numerical Simulations of Delamination Propa- Univ.), Japan G. Ishigami, A. Miwa, K. Nagatani, K. Yoshida (To- gation in CFRP Structures hoku Univ.), Japan N. Hu, Y. Zemba, H. Fukunaga (Tohoku Univ.), Japan 12:10-12:30 2006-f-10 Inteligent Thermal Control and Design of 12:10-12:30 2006-k-10 Nano-Satellites Design and Mobility Evaluation of a Lunar Ve- T. Tanaka (Tokyo Univ.), Japan hicle using Mesh Crawler S. Wakabayashi, K. Matsumoto (IAT/JAXA), Japan June/8th (Thu) PM(1) Session o-3-1 at Room A Session d-11 at Room B Session k-3 at Room C Small Satellite Applications to Lunar & Martian Exploration (3) Observation Satellite Orbit Determination Chairperson :H. Okubo (Osaka Pref. Univ.) Chairperson :J. Foliard (CNES) Chairperson :T. Iwata (JAXA) F. Terui (JAXA/IAT) M. Horii (JAXA/OSFO) H. Akiyama (Akita Univ.)

13:30-14:00 2006-o-3-01v 13:30-13:50 2006-d-54 13:30-13:50 2006-k-11 VHF Broadband Digital Interferometer on a Precise Orbit Determination for ADEOS-II Investigations of ILOM Project - In situ Lunar Small Satellite S. Nakamura, N. Kudo (JAXA), Y. Yamamoto (Fujitsu Orientation Measurement by PZT telescope on Z. Kawasaki, T. Morimoto, T. Ushio (Osaka Univ.), Ltd), O. Montenbruck (DLR, GSOC), Japan the Moon Japan H. Araki, H. Hanada, H. Noda, K. Matumoto (NAO) 13:50-14:10 2006-d-55 et.al., Japan 14:00-14:30 2006-o-3-02v Precise Orbit Determination for GRACE-B A small satellite for global imaging observation N. Kudo, S. Nakamura (JAXA), S. Katagiri (Fujitsu 13:50-14:10 2006-k-12 of the ionosphere-thermosphere-mesosphere- Limited), Japan Energy for the moon explorations plasmasphere M. Oda (IAT/JAXA), Japan A. Saito (Kyoto Univ.), M. Working group (MTI satel- 14:10-14:30 2006-d-56 lite working group), Japan Evaluating Interferometric Baseline Perfor- 14:10-14:30 2006-k-13 mances in a Close Formation Flight by Using Extensions of NASAs Exploration Architec- 14:30-15:00 2006-o-3-03v Relative GRACE GPS Navigation Solutions ture: Performance Capabilities and Market Monitoring Earth’s environments with GPS re- A. O Kohlhase (DLR), R. Kroes (TU Delft), S. Damico Economics of a Lunar Propellant Production ceiving system and micro accelerometer on low (DLR), Germany Facility Earth orbiting satellites A. Charania (SEI), H. Kanamori (Shimizu Corpora- T. Tsuda, Y. Fukuda (Kyoto Univ.), A. Araya (Univ. 14:30-14:50 2006-d-57 tion), USA Tokyo), A. Saito (Kyoto Univ.) et.al., Japan Precise Maneuver Calibration for Remote Sens- ing Satellites 14:30-14:50 2006-k-14 15:00-15:30 2006-o-3-04v Y. T Yoon, O. Montenbruck, M. Kirschner Research Issues on Mars Exploring Micro Plane Advanced Remote Sensing Concept by Small (DLR/GSOC), Germany Using Energy Transmisson Satellites Constellation K. Yonemoto (Kyushu Institute of Technology), Japan N. Miyamura (Tokyo Univ.), Japan 14:50-15:10 2006-d-58 Precise Orbit Determination for the TerraSAR- 14:50-15:10 2006-k-15 X Mission The Mars Water Experiment O. Montenbruck, Y. Yoon, E. Gill, M. Garcia- A. Toigo (Kobe Univ.), M. Richardson, I. Mcewan fernandez (DLR/GSOC), Germany (California Institute of Technology), D. Banﬁeld (Cor- nell Univ.), Japan 15:10-15:30 2006-d-59 Overview of Orbit Determination Experiments using Satellite-to-Satellite Tracking Data via the DRTS M. Ogawa, S. Taniguchi, M. Saitoh (JAXA), S. Kawa- zoe (FUJITSU Ltd) et.al., Japan June/8th (Thu) PM(1) Session a-11 at Room D Session c-7 at Room E Session f-3 at Room F Combined Cycle Engine High Temperature Materials Spacecraft and Space Station (1)

Chairperson :H. Nagata (Hokkaido Univ.) Chairperson :M. Tagawa (Kobe Univ.) Chairperson :M. Lauer (ESA/ESOC/OPS/-GFI) T. Arai (Osaka Pref. Univ.) S. Sugimoto (JAXA) K. Kimura (NICT)

13:30-13:50 2006-a-50 13:30-13:50 2006-c-28 13:30-13:50 2006-f-11 Numerical Investigation of Flow Structures in Current Status of The Development of Hot Engineering Research for New Tethered Solar Constant Area Mixers for Ejector-jets Structures Based on Ultra High Temperature Power Satellite E. Kitamura, G. Masuya (Tohoku Univ.), Japan Ceramic Materials Within The PRORA-USV S. Sasaki, K. Tanaka, K. Higuchi, N. Okuizumi SHS Project (JAXA) et.al., Japan 13:50-14:10 2006-a-51 L. Scatteia, A. Del vecchio, G. Marino (CIRA - Italian Aerodynamic Performance of the Combined- Aerospace Research Centre), R. Savino (Department 13:50-14:10 2006-f-12 Cycle Engine Inlet in a Supersonic Region of Space Science and Engineering (DISIS) Univ. of Ground Control of Remote Synchronization K. Tani, T. Kanda, K. Kato, N. Sakuranaka (JAXA) Naples ”Federico II”, ITALY), Italy System for Onboard Crystal Oscillators of et.al., Japan Quasi-Zenith Satellites 13:50-14:10 2006-c-29 T. Iwata (AIST), N. Takasaki (Tokyo Univ.), M. Imae 14:10-14:30 2006-a-52 Eﬀects of Microstructural Characteristics on (AIST), A. Iwasaki (Tokyo Univ.) et.al., Japan Computational Analysis of the Ejector-jet- Tensile Properties of Unidirectional SiC/SiC Mode of RBCC Engine Composites 14:10-14:30 2006-f-13 S. Hasegawa, K. Tani (JAXA), Japan M. Kotani, T. Ogasawara, T. Ishikawa, H. Hatta Quasi-real-time Signal Delay Estimation of (JAXA), Japan Remote Synchronization System for Onboard 14:30-14:50 2006-a-53 Crystal Oscillators Preliminary Tests of Downstream Combustion 14:10-14:30 2006-c-30 N. Takasaki, A. Iwasaki (Tokyo Univ.), T. Iwata, M. Ramjet-mode in a Combined Cycle Engine Gas Leakage Properties of Two Dimen- Imae (AIST) et.al., Japan Combustor sional Carbon/Carbon Composites Processed K. Kato, T. Kanda, K. Kobayashi, K. Kudo (JAXA) by Leakage Suppression Treatment 14:30-14:50 2006-f-14 et.al., Japan F. Ono, S. Ueda, M. Takegoshi (JAXA), Japan Development of Inter-Satellite Communication System for Formation Flight SCOPE Mission 14:50-15:10 2006-a-54 14:30-14:50 2006-c-31 T. Toda, Y. Saito, Y. Tsuda, I. Shinohara Progress of Scramjet and Combined-Cycle En- Processing and properties of high temperature (ISAS/JAXA) et.al., Japan gine Research at JAXA composites using superior polyimide ”Tri-A PI” T. Kanda (JAXA), Japan T. Ogasawara, Y. Ishida, R. Yokota (JAXA), T. 14:50-15:10 2006-f-15 Watanabe (Kawasaki Heavy Industries) et.al., Japan The worst case is studied for the projective advanced 14:50-15:10 2006-c-32 M. Yukizane, H. Fujii, H. Takikawa, T. Watanabe On the challenges in the analysis of structures (Tokyo Metoropolitan Univ.), Japan of functionally graded materials for space applications R. P. Shimpi (I.I.T. Bombay, India), India June/8th (Thu) PM(1) Session r-1-1 at Room G Session h-6 at Room H Solar Power System Combustion and Synthesis

Chairperson :F. Little (Texas A&M) Chairperson :M. Tsue (Tokyo Univ.) H. Brandhorst (Arburn Univ.) H. Nomura (Nihon Univ.)

13:30-13:50 2006-r-1-01 13:30-13:50 2006-h-23 The Concept of Solar Power Satellites: Past, Microgravity Experiments of Flame Spread Be- Present and Future havior Along a Fuel Droplet Array in Fuel J. C Mankins (Artemis Innovation Management Solu- Vapor-Air Mixture tions LLC), USA Y. Suganuma, H. Nomura, Y. Ujiie (Nihon Univ.), M. Mikami (Yamaguchi Univ.), Japan 13:50-14:10 2006-r-1-02 European steps towards solar power satellites 13:50-14:10 2006-h-24 L. Summerer, T. Reunes (ESA), Netherlands A Study on Flame Spread in Two-dimensional Droplet Clouds considering Local Flame-spread 14:10-14:30 2006-r-1-03 Limit Summary of Studies on Space Solar Power H. Shigeno, H. Shigeno, H. Oyagi, M. Mikami (Yam- Systems of Japan Aerospace Exploration aguchi Univ.) et.al., Japan Agency(JAXA) M. Masahiro, F. Tatsuhito, S. Yuka (JAXA), Japan 14:10-14:30 2006-h-25 Ignition of Solid Fuels at Low Pressure 14:30-14:50 2006-r-1-04 Y. Nakamura, A. Aoki (Hokkaido Univ.), Japan Roadmap for SSPS Technology R&D H. Nagayama (Mitsubishi Research Institute, Inc.), T. 14:30-14:50 2006-h-26 Fujita, Y. Saito, M. Mori (JAXA), Japan Eﬀects of DC Electric Fields on Combustion Be- havior of Droplet Pairs under Microgravity 14:50-15:10 2006-r-1-05 K. Yamashita, O. Imamura, I. Kume, J. Osaka (Tokyo International Rocket Experiment on the Univ.) et.al., Japan Retrodirective Antenna for Microwave Power Transmission with Furoshiki Deployment 14:50-15:10 2006-h-12 N. Kaya, N. Kaya, M. Iwashita (Kobe Univ.), S. Naka- Study on characteristics of thermo-acoustic suka (Tokyo Univ.) et.al., Japan streaming by microgravity experiment and numerical simulation 15:10-15:30 2006-r-1-06 Y. Yamauchi, T. Kuwahara, M. Tanabe (Nihon Univ. High-Voltage High-Energy Stretched Lens Ar- ), Japan ray Square-Rigger (SLASR) for Direct-Drive Solar Electric Propulsion J. Howell (NASA), M. J. O’neill (ENTECH, Inc.), J. C. Mankins (Artemis Innovation Management Solutions, LLC), USA June/8th (Thu) PM(2) Session o-3-2 at Room A Session d-12 at Room B Session k-4 at Room C Small Satellite Uses and Evolution Attitude Dynamics and Control Atomospheric & Plasma Exploration

Chairperson :T. Tsuda (Kyoto Univ.) Chairperson :F. Terui (JAXA/IAT) Chairperson :M. Hirahara (Rikkyo Univ.) S Nishida (JAXA/IAT) J. Fertig (ESA/ESOC) Y. Takahashi (Tohoku Univ.)

15:40-16:10 2006-o-3-05v 15:40-16:00 2006-d-60 15:40-16:00 2006-k-17 Possibility of small satellite in on-orbit servicing On Attitude Dynamics of Spin-stabilized satel- Orbital Characteristics of Venues Exploring Mis- and demonstration experiments on SmartSat-1 lite sion, PLANET-C S. Kimura, S. Kimura, Y. Nagai, H. Yamamoto (NICT) Y. V Kim (CSA), Canada N. Ishii, H. Yamakawa (JAXA), M. Kimura (NEC Toshiba et.al., Japan Space Systems, Ltd), M. Nakamura (JAXA) et.al., Japan 16:00-16:20 2006-d-61 16:10-16:40 2006-o-3-06v Nonlinear Adaptive Control for Stabilizing 16:00-16:20 2006-k-18 Activities of Small Spacecraft Systems Research Spacecraft System at Capturing Phase Space telescope in Earth orbit for planetary sci- Center and on-going Projects T. Kida, A. Ito, Y. Ikeda, T. Nagashio (Univ. of ence: TOPS mission H. Okubo, H. Azuma (Osaka Prefecture Univ.), Japan Electro-Comunications), Japan Y. Takahashi, Y. Takahashi, T. Sakanoi, A. Yamazaki (To- hoku Univ.) et.al., Japan 16:40-17:10 2006-o-3-07v 16:20-16:40 2006-d-62 A Small Satellite Platform for Technology Robust Gain-Scheduling Attitude Control of 16:20-16:40 2006-k-19 Demonstration Time Varying Flexible Spacecraft - A Case SCOPE : FUTURE FORMATION-FLYING M. Kato, M. Kato, S. Okada, H. Imamura (JAXA) Study of ETS-VIII MAGNETOSPHERIC SATELLITE MISSION et.al., Japan T. Ohtani, Y. Hamada (JAXA), T. Nagashio, T. Kida Y. Saito, T. Takashima, K. Maezawa (ISAS/JAXA), M. (Univ. of Electro-Communications), Japan Fujimoto (Tokyo Institute of Technology) et.al., Japan 17:10-17:40 2006-o-3-08v Space Debris Removal by A Small Satellite 16:40-17:00 2006-d-63 16:40-17:00 2006-k-20 S. Nishida, S. Kawamoto, Y. Ohkawa, F. Terui (JAXA) Optimization for Reaction-Wheel Conﬁgura- BepiColombo Mission and Mercury Magneto- et.al., Japan tion spheric Orbiter T. Nishiyama, S. Yoshikawa (Mitsubishi Electric Cor- H. Hayakawa, H. Yamakawa, H. Ogawa, Y. Sone (JAXA) poration), K. Yamada (Nagoya Univ.), Japan et.al., Japan

17:00-17:20 2006-d-64 17:00-17:20 2006-k-21 Spacecraft Attitude Control Using a Double BepiColombo Project to Mercury: Its Payload and Gimbal Control Moment Gyro Technologies K. Yamada (Nagoya Univ.), T. Shima (Mitsubishi Y. Kasaba, T. Takashima, H. Hayakawa, T. Mukai Electric Corporation), Japan (ISAS/JAXA) et.al., Japan

17:20-17:40 2006-d-65 17:20-17:40 2006-k-22 Routine and Contingency Attitude Manoeuvre Wide range temperature characteristics of Flux- Planning for the PLANCK Mission gate Magnetometer Sensor for Bepi-Colombo A. J c Mcdonald (LogicaCMG), G. Gienger (ESA), MMO Germany Y. Nishio, U. Mizuo, M. Tanaka, F. Tohyama (Tokai Univ.) et.al., Japan June/8th (Thu) PM(2) Session e-1 at Room D Session c-8 at Room E Session f-4 at Room F Jets and Shock Waves Health Monitoring & NDE Spacecraft and Space Station (2)

Chairperson :K. Suzuki (Tokyo Univ.) Chairperson :S. Ueda (JAXA) Chairperson :S. Fukuda (JAXA) T. H. Moulden C-W. Kong (KARI) K. Tanaka (JAXA) (Univ. of Tennessee Space Inst.) 15:20-15:40 2006-c-33 15:20-15:40 2006-f-16 15:20-15:40 2006-e-01 Smart Honeycomb Sandwich Panels with Dam- The ATV JULES VERNE mission overview Numerical Simulation of Shock-Induced Mo- age Detection and Shape Recovery Functions L. Francillout, T. Martin, D. Carbonne, P. Labour- tion of Solid Bodies using a Cartesian Cut Cell Y. Okabe (Tokyo Univ.), S. Minakuchi, N. Shiraishi, N. dette (CNES) et.al., France Method Takeda (Graduate School of Frontier Sciences, Tokyo Y. Sakamura, Y. Umebayashi, K. Nakayama, T. Suzuki Univ.), Japan 15:40-16:00 2006-f-17 (Toyama Pref. Univ.), Japan THE ATV opportunities and CAM demo com- 15:40-16:00 2006-c-34 putation 15:40-16:00 2006-e-02 Monitoring of Crack Progress in Composite Ad- S. Kerambrun (AtosOrigin), T. Martin, L. Francillout Performance of straight and slanted entry noz- hesive Joints using FBG Sensors (CNES), E. De pasquale (ESA) et.al., France zles S. Takeda, T. Yokozeki, T. Ogasawara (JAXA), Japan R. Ethirajan (IIT Kanpur), S.C. Kumar, S. Elangovan, 16:00-16:20 2006-f-18 A.J. Stanley (MIT Chennai) et.al., India 16:00-16:20 2006-c-35 Omnidirectional Vision System for Spacecraft Development of Air-Coupled Ultrasonic Scan- On-Orbit Monitoring 16:00-16:20 2006-e-04 ner for Nozzle and Tank Shape Composites A. Takeya, K. Yamada, S. Matsuoka (Mitsubishi Elec- Utilization of swirling effect to improve the per- S. Sugimoto, T. Ishikawa (JAXA), Y. Shinagawa, T. tric Corporation), K. Ijichi (Institute for Unmanned formance of supersonic nozzle for micro-particle Ogiwara (Gnes Corporation), Japan Space Experiment Free Flyer) et.al., Japan delivery Y. Liu, G. Costigan (Univ. of Oxford), UK 16:20-16:40 2006-c-36 16:20-16:40 2006-f-19 Development of Spherical Ti-6Al-4V Tank by Contact Dynamics Analysis of a Spacecraft in Superplastic Blow Forming and Diffusion Bond- Micro Gravity with an Air-floating Test Bed ing H. Nakanishi, D. Tanaka, K. Yoshida (Tohoku Univ.), Y. Yi, J. Yoon, H. Lee (KARI), Republic of Korea Japan

16:40-17:00 2006-c-37 16:40-17:00 2006-f-20 Experimental Impact Force Identiﬁcation of Vibration Propagation Suppression of Space- CFRP Structures Using Strain Sensors craft using Piezoelectric Sensors and Actuators H. Fukunaga, H. Miyazawa, N. Hu (Tohoku Univ.), Y. Il Yun, S. Nakasuka (Tokyo Univ.), Japan Japan 17:00-17:20 2006-f-21 Hierarchical Self-Assembly Planning of Modu- lar Structure Systems K. Ukegawa, M. Natori (ISAS/JAXA), Japan June/8th (Thu) PM(2) Session r-1-2 at Room G Session h-7 at Room H ISS and Space Exploration Materials Processing and Crystal Growth

Chairperson :L. Summerer (ESTEC) Chairperson :G. Sazaki (Tohoku Univ.) J. Howell (NASA) Y. Jianding (JAXA)

16:00-16:20 2006-r-1-24 15:40-16:00 2006-h-29 A Wireless Power Based Space Transportation System Fabrication of Ferroelectric Oxide Glass using Containerless F. E Little ( Texas A&M Univ.), USA J. Yu, Y. Arai, S. Yoda (JAXA), Japan 16:00-16:20 2006-h-30 16:20-16:40 2006-r-1-08 Growth of Ferroelectric Oxide Crystal using Containerless Observation of High Energy Electrons and Gamma- Processing rays with CALET at the JEM/ISS H. Masukuni, T. Motegi (Chiba Institute of Technology), J. Yu, Y. T. Tamura (Kanagawa Univ.), S. Torii (Waseda Univ.), J. Arai (JAXA) et.al., Japan Nishimura, T. Yamagami (ISAS/JAXA) et.al., Japan 16:20-16:40 2006-h-31 16:40-17:00 2006-r-1-09 Utilization of chemical fixation and fluorescence labeling tech- ORGANIZATION AND FUNCTION OF INTERNA- niques on protein crystal growth studies TIONAL SPACE STATION (ISS) MULTILATERAL I. Yoshizaki (JAXA), Y. Iimura, S. Fukuyama (Advanced Engineering MEDICAL OPERATIONS Services Co., Ltd.), L. Rong (JAXA) et.al., Japan J. Michael Duncan (NASA Lyndon B. Johnson Space Center), A. E. Sargsyan (Wyle Laboratories, Life Sciences Group), T. 16:40-17:00 2006-h-32 A. Taddeo (NASA Lyndon B. Johnson Space Center), P. Ver- Molecular level in situ observations of the impurity effects on non Mcdonald (Wyle Laboratories, Life Sciences Group) et.al., the growth of protein crystals by advanced optical microscopy USA G. Sazaki (Institute for Materials Research, Tohoku Univ.), A. Van driessche (Laboratorio de Estudios Cristalograficos, Instituto Andaluz 17:00-17:20 2006-r-1-10 de Ciencias de la Tierra), G. Dai (National Microgravity Laboratory, Polar Region Exploration for International Lunar Base Chinese Academy of Sciences), I. Yoshizaki (ISS science project office, K. Matsumoto, M. Oda, S. Wakabayashi, S. Kawamoto JAXA) et.al., Japan (IAT/JAXA) et.al., Japan 17:00-17:20 2006-h-33 JAXA-GCF Project — High-quality Protein Crystals Grown 17:20-17:40 2006-r-1-11 under Microgravity Environment for Better Understanding Planetary Defense Using Extensions of NASAs Explo- of Protein Structure ration Architecture M. Motohara, M. Sato (JAXA), H. Tanaka (Japan Space Forum), K. A. Charania, J. Wallace (SpaceWorks Engineering, Inc. Inaka (Maruwa Food Industries, Inc) et.al., Japan (SEI)), USA 17:20-17:40 2006-h-34 17:40-18:00 2006-r-1-23 PLATE-SHAPED In0.3Ga0.7As CRYSTALS GROWN BY Update for the Stretched Lens Array SquareRigger THE TRAVELING LIQUIDUS ZONE METHOD WITH (SLASR) for Space REDUCED CONVECTION IN A MELT H. W. Brandhorst (Auburn Univ.), M. J. O’neill (ENTECH, K. Kinoshita, Y. Ogata (JAXA ISS Science Project Office), S. Adachi Inc.), USA (Advanced Engineering Services Co. Ltd.), S. Yoda (JAXA ISS Sci- ence Project Office) et.al., Japan June/9th (Fri) AM(1) Session d-13 at Room B Session k-5 at Room C Session e-2 at Room D Minor Bodies & Deep Space Trajectory Design around Lagrange Low Speed Aerodynamics and Turbulence Point Exploration (1) Chairperson :J. Kawaguchi (JAXA/ISAS) Chairperson :O. Mori (JAXA) Chairperson :Y. Sakamura (Toyama Pref. Univ.) L.A. Canguhuala (NASA/JPL) D. Izzo (ESA/ESTEC) H. Kihara (Kyushu Univ.)

09:00-9:20 2006-d-66 09:00-9:20 2006-k-23 09:00-9:20 2006-e-05 Optimization of Trajectories from Earth to L2 Scientific Results on Asteroid 25143Itokawa Aerodynamic Characteristics of Nonslender Fexi- S. Aida (Tokyo Univ.), Y. Kawakatsu, J. Kawaguchi Observed by Hayabusa Spacecraft ble Delta Wing in Pitching Motion (JAXA), Japan A. Fujiwara, J. Kawaguchi (JAXA), D. K. Yeomans S. Kato, H. Kawazoe, M. Okano (Tottori Univ.), Japan (JPL/NASA), M. Abe (JAXA) et.al., Japan 09:20-9:40 2006-d-67 09:20-9:40 2006-e-06 Fuel optimal transfer to small amplitude Lis- 09:20-9:40 2006-k-24 CFD Design Study of Subsonic Landing Phase sajous orbits around the L2 Libration point LIDAR for Asteroid Explore HAYABUSA - De- Aerodynamics for The Lifting Body Re-Entry J. Schoenmaekers (ESA/ESOC), M. Lorenzo-barreiro velopment and On Orbit Evaluation - Y. Yamamoto (JAXA), Japan (SSL), J. Pulido-cobo (GMV), Germany T. Mizuno (ISAS/JAXA), K. Tsuno, E. Oku- mura (NEC Toshiba Space Systems), M. Nakayama 09:40-10:00 2006-e-07 09:40-10:00 2006-d-68 (Toshiba), Japan Steady-state evaluation of two dimensional RANS Preliminary Analysis of Low Energy Interplan- equations in turbulence flow for NACA 4412 in etary Transfer with Multi-impulse Escape 09:40-10:00 2006-k-25 ground effect with fixed and moving ground condi- M. Nakamiya (Sokendai Univ.), H. Yamakawa The Minor Body Sample Return Mission in the tions (JAXA), Japan Post-Hayabusa Era A. Firooz (Internet), M. A Gadami (Internet), Iran M. Abe, H. Yano, T. Iwata, Y. Kawakatsu 10:00-10:20 2006-d-69 (ISAS/JAXA) et.al., Japan 10:00-10:20 2006-e-08 On the Interplanetary Flight from the Sun- Structure of the k-e Turbulence Model Earth L2 Point 10:00-10:20 2006-k-26 T. H Moulden (UTSI), USA M. Matsumoto (Tokyo Univ.), J. Kawaguchi ESAs Don Quijote NEO mission: An opportu- (ISAS/JAXA), Japan nity for the investigation of an artificial impact crater on an asteroid 10:20-10:40 2006-d-70 A. Galvez (ESA), France Stable Periodic Orbits with Low Thrust Accel- eration in the Restricted Three Body Problem 10:20-10:40 2006-k-27 M. Morimoto (National Astronomical Observatory), H. Surface Science Package on rovers for micro- Yamakawa, K. Uesugi (JAXA), Japan gravity target H. Demura (Univ. of Aizu), H. Naraoka (Okayama Univ.), H. Yano, T. Yoshimitsu (ISAS/JAXA) et.al., Japan June/9th (Fri) AM(1) Session g-1 at Room E Session r-1-3 at Room F Session f-5 at Room G Mission and Design Hokkaido Satellite Project Ground Support System

Chairperson :D.A. Smith (Boeing co.) Chairperson :N. Kamimori (JAXA) Chairperson :T. Kato (JAXA) K. Mizobata (Muroran Inst. of R. Suzuki (NICT) N. Nishigori (Fujitsu) Tech.) 09:00-9:20 2006-r-1-12 09:00-9:20 2006-f-22 09:00-9:20 2006-g-01 Hokkaido satellite project: Business Model Interoperability reduces cost and risk at Sval- A HYBRID LAUNCH SYSTEM FOR MI- S. Satori (Hokkaido Institute of Technology), K. Ishimura, T. bard Satellite Station CROSATELLITE PAYLOADS USING CA- Totani (Hokkaido Univ.), S. Era (ATF Corporation) et.al., A. Jose Jensen (Kongsberg Satellite Services), R. Skat- MUI HYBRID UPPERSTAGES WITH THE Japan teboe, B. Pedersen (Kongsberg Satellite Services), Nor- ROCKETPLANE XP way C. J. Lauer (Rocketplane Ltd.), H. Nagata (Hokkaido 09:20-9:40 2006-r-1-13 Univ.), T. Uematsu (HASTIC), Japan Hokkaido Satellite Project : System Design of a Engi- 09:20-9:40 2006-f-23 neering Test CubeSat ON-GROUND SUPPORT TO THE MARS 09:20-9:40 2006-g-02 K. Ishimura, T. Totani (Hokkaido Univ.), S. Era (ATF), A. EXPRESS AND ROSETTA AOCS DURING MANEUVER COMPUTATION AT ATV-CC Nakamura (AIDMA) et.al., Japan SPECIAL OPERATIONS J. Goester, J. Goester, J. Berges, D. Carbonne (CNES) M. Lauer (ESA/ESOC/OPS-GFI), Germany et.al., France 09:40-10:00 2006-r-1-14 Hokkaido Satellite Project: Structural and Thermal 09:40-10:00 2006-f-24 09:40-10:00 2006-g-03 Design of Engineering Test CubeSat Cortex - Experience With The Tracking Data Study of Space Transportation for Space Solar T. Totani, T. Sakakibara (Hokkaido Univ.), T. Yasunaka (Ue- System At ESOC/ESA Power Systems matsu Electric Co., Ltd.), K. Ishimura (Hokkaido Univ.) et.al., G. Ziegler (EDS at ESOC/ESA), I. Munoz (GMV at S. Kitamura, Y. Ohkawa, H. Aoki (JAXA), Japan Japan ESOC/ESA), Germany

10:00-10:20 2006-g-04 10:00-10:20 2006-r-1-15 10:00-10:20 2006-f-25 Robust Optimal Design Method for Future Hokkaido Satellite Project:Development of Magnetic Automatic Monitoring and Diagnostic System Space Transportation Vehicle Torquer for Engineering Test CubeSat for Infrared Imaging Surveyor ASTRO-F S. Imamura, T. Tsuchiya (Tokyo Univ.), Japan Y. Aoyanagi, T. Iwamoto (Hokkaido Institute of Technology), R. Takaki, M. Hashimoto, H. Honda, A. Choki (JAXA) K. Ishimura, T. Totani (Hokkaido Univ.) et.al., Japan et.al., Japan 10:20-10:40 2006-g-05 Use of a Modular Multi-Disciplinary Optimiza- 10:20-10:40 2006-r-1-16 10:20-10:40 2006-f-26 tion Tool to Design Space Exploration Vehicles Hokkaido Satellite Project: Communication System Engineering Database for ISAS Spacecraft Op- S. Geoﬀrey Moon (UTIAS), Canada T. Sato, R. Mitsuhashi, S. Satori (Hokkaido Institute Of Tech- eration Needs (EDISON) for Low Earth Orbit nology), K. Ishimura (Hokkaido Univ) et.al., Japan Satellites 10:40-11:00 2006-g-06 H. Honda, R. Takaki, M. Hashimoto, A. Choki Multidisciplinary Design Optimization for Hy- 10:40-11:00 2006-r-1-17 (ISAS/JAXA) et.al., Japan personic Experimental Vehicle Hokkaido Satellite Project: Development of Hyper- T. Tsuchiya, Y. Takenaka (Tokyo Univ.), H. Taguchi spectral Camera (JAXA), Japan S. Ueno, S. Satori, R. Mitsuhashi, R. Miura (Hokkaido Insti- tute of Technology) et.al., Japan June/9th (Fri) AM(1) Session j-1 at Room H Non-GEO Satellote (1)

Chairperson :T. Ikegami (Meiji Univ.) R. Suzuki (NICT)

09:00-9:20 2006-j-01 ELEMENTAL TECHNOLOGIES FOR REAL- IZATION OF PANEL EXTENSION SATEL- LITE (PETSAT) Y. Sugawara, S. Nakasuka, T. Eishima, H. Sahara (Tokyo Univ.) et.al., Japan

09:20-9:40 2006-j-02 THERMAL CONTROL OF PANEL EXTEN- SION SATELLITE (PETSAT) K. Higashi (DaVinci Co.Ltd), S. Nakasuka, Y. Sug- awara, H. Sahara (Tokyo Univ.) et.al., Japan

09:40-10:00 2006-j-03 Optimization Study of Constellation Parame- ters for LEO Satellite Communication System R. Suzuki (NICT), Y. Yasuda (Waseda Univ.), Japan

10:00-10:20 2006-j-05 Research of Volatile Code Rate Inter-satellite Communication System for Micro-satellite Formation-ﬂying Constellation G. Wu (Harbin Institute Technology Research Cen- ter of Satellite Technology), Z. Sun, D. Zhao, Z. Liu (Harbin Institute Technology Research Center of Satel- lite Technology), China June/9th (Fri) AM(2) Session d-14 at Room B Session k-6 at Room C Session e-3 at Room D Minor Bodies & Deep Space High Speed and High Enthalpy Wind Orbit Transfer Exploration (2) Tunnel Testing Chairperson :N.M. Ivanov (RMCC) Chairperson :O. Mori (JAXA) Chairperson :K. Komurasaki (Tokyo Univ.) Y. Kawakatsu (JAXA/ISAS) D. Izzo (ESA/ESTEC) T. Yamada (JAXA/ISAS)

10:50-11:10 2006-d-71 10:50-11:10 2006-k-28 10:30-10:50 2006-e-09 An Approach for Computing Fixed-Time, Very Development of the Sampling Device for Un- Force/Heat Flux Measurements in the JAXA Low-Thrust Orbit Transfers in Presence of J2 differentiated Asteroid Surface and Sub-Surface 1.27 m Hypersonic Wind-Tunnel for HB-2 Type and Shadow Effects Materials Ballistic Model: A Summary Y. Gao, X. Li (Academy of Opto-Electronics, Chinese H. Yano (ISAS/JAXA), T. Noguchi (Ibaraki Univ.), S. S. Kuchi-ishi, S. Watanabe, S. Nagai, T. Koyama Academy of Sciences), China Matsunaga (Tokyo Institute of Technology), O. Mori (JAXA) et.al., Japan (ISAS/JAXA) et.al., Japan 11:10-11:30 2006-d-72 10:50-11:10 2006-e-10 Hybrid optimization algorithm for multi- 11:10-11:30 2006-k-29 Numerical and experimental investigations of revolution low-thrust transfers Concept and System Consideration of Tethered the HSFD 2 transonic aerodynamics J. Gil, M. Molina, L. Tarabini, M. Graziano (GMV Sampling for Minorbody Exploration in Deep M. D Leplat, P. Champigny, P. Thorigny (ONERA), SA), Spain Space J. Oswald (CNES) et.al., France S. Matunaga (Tokyo Institute of Technology), O. Mori, 11:30-11:50 2006-d-73 K. Nakaya (ISAS/JAXA), S. Masumoto (Tokyo Insti- 11:10-11:30 2006-e-11 Optimal Low Thrust Rendezvous Trajectories tute of Technology) et.al., Japan Laser absorption spectroscopy of oxygen Between Halo Orbits molecule in free piston shock tunnel M. J Volle (a.i. solutions, Inc.), USA 11:30-11:50 2006-k-30 H. Tanno, T. Komuro, K. Sato, K. Itoh (JAXA- Study of sampling method by the use of a rigid KSPC), Japan 11:50-12:10 2006-d-74 sampler connected by tether Considerations on Orbital Control of a Rigid H. Takikawa, H. A Fujii, M. Yukizane, T. Watanabe 11:30-11:50 2006-e-12 Satellite System under Nonholonomic Con- (Tokyo Metropolitan Univ.), Japan Numerical Studies on Non-Uniformity in straint Freestream of Shock Tunnel with Conical Noz- K. Fujita, S. Hokamoto (Kyushu Univ.), Japan zle T. Yamada (Tokyo Univ.), K. Suzuki (Graduate School 12:10-12:30 2006-d-75 of Frontier Sciences, Tokyo Univ.), Japan Preliminary Trajectory Design of Laser- Propelled Space Vehicles H. Yamakawa, I. Funaki (JAXA), Japan June/9th (Fri) AM(2) Session g-2 at Room E Session r-1-4 at Room F Session m-1 at Room G Concept International Collaboration in Space Geophysics Communications Chairperson :H. Nagata (Hokkaido Univ.) Chairperson :U. Sastrokusumo (Inst. Tech. Chairperson :Y. Takahashi (Tohoku Univ.) T. Tsuchiya (Tokyo Univ.) Bandung) Y. Saito (JAXA/ISAS) K. Kondo (National Institute of 11:10-11:30 2006-g-07 Multimedia Education) 10:50-11:10 2006-m-01 The study of feasibility and characteristic of Observation of Auroral Phenomena by For- Space Elevator 11:10-11:30 2006-r-1-18 mation Flight of Polar Patrol Balloons - M. Ohta, H. A. Fujii, T. Watanabe (Tokyo Metropoli- INTERNATIONAL COOPERATION USING Instrumentation and Observational Results tan Univ.), T. Ogasawara (Tokyo Metropolitan Insti- COMMUNICATIONS SATELLITE IN THE from Circum-Antarctica Balloon Experiment in tute of Technology), Japan AFTERMATH OF DISASTERS 2002/2003- K. Nagami, I. Nakajima, H. Juzoji (Tokai Univ. school H. Yamagishi, A. Kadokura, Y. Ebihara (National 11:30-11:50 2006-g-08 of Medicine), K. Igarashi (NICT) et.al., Japan Institute of Polar Research), T. Yamagami (JAXA) Color Design Considerations for Commercial et.al., Japan Space Tourism Vehicles 11:30-11:50 2006-r-1-19 M. Onuki, M. Onuki (Space Frontier Foundation), C. TELEMEDICINE PACKAGE FOR DISAS- 11:10-11:30 2006-m-02 John Lauer (Rocketplane Ltd.), P. Smith (Astronauti- TERS Sounding rocket observations of neutral tem- cal Designer, Artist) et.al., USA K. Nagami, I. Nakajima, H. Juzoji (Tokai Univ. School perature and density in the polar lower ther- of Medicine), K. Igarashi (NICT) et.al., Japan mosphere during the DELTA campaign 11:50-12:10 2006-g-09 J. Kurihara, T. Abe, K. Oyama (ISAS/JAXA), N. Open Architecture Approaches to Enhance Hu- 11:50-12:10 2006-r-1-20 Iwagami (Tokyo Univ.) et.al., Japan man Exploration Sustainability International Satellite Collaboration Experi- D. A. Smith (Boeing), USA ments in NIME 11:30-11:50 2006-m-03 K. Kondo, K. Kondo, K. Asai, N. Osawa (National Development of a Measurement Technique for Institute of Multimedia Education), Japan Medium-Energy Electrons: Observation of En- ergetic Electrons During the DELTA Campaign 12:10-12:30 2006-r-1-21 K. Ogasawara, K. Asamura, T. Takashima, T. Mukai Contribution for Post-Tsunami Syndrome: (JAXA) et.al., Japan Multimedia Application in Medical Teleeduca- tion and Telemedicine using New Post Partners 11:50-12:10 2006-m-04 Network Electron density measurement under the effects U. Sastrokusumo, A. Bayu Suksmono, M. Ridwan Ef- of electron beam injection during the DELTA fendi, A. Adesena (ITB) et.al., Indonesia campaign M. Wakabayashi, T. Ono (Tohoku Univ.), M. Ya- 12:30-12:50 2006-r-1-22 mamoto (Kochi Univ. of Technology), Japan Secure Satellite TCP/IP Connection and Se- cure Satellite Client Authentication: Experi- ments in the New Post-Partner Project K. Umeno (NICT), H. Terai (ChaosWare, Inc.), Japan June/9th (Fri) AM(2) Session j-2 at Room H Non-GEO Satellote (2)

Chairperson :R. Suzuki (NICT) N. Fuke (KDDI)

10:50-11:10 2006-j-06 Launch of Kirari(OICETS) from Baikonur T. Yamawaki, N. Takahashi, K. Arai (JAXA), I. Mase (NTspace) et.al., Japan

11:10-11:30 2006-j-07 Functional demonstrations of the Laser Utiliz- ing Communication Equipment on OICETS T. Jono, Y. Takayama, N. Kura, K. Ohinata (JAXA) et.al., Japan

11:30-11:50 2006-j-08 The way how 920 ﬁre departments expect a reliable circuit to support telemedicine en rout ¡ An investigation on a nationwide satellite broadband communication system via HEO¿ S. Inoguchi, H. Juzoji, K. Nagami, I. Nakajima (Tokai Univ.) et.al., Japan

11:50-12:10 2006-j-09 Strict Temporal Synchronization of Distribute Satellite System G. Xiao-chun Gong, X. Gong-dong Xu, W. Guo-qiang Wu, W. Bao-lin Wu (Harbin Institute of Technology), China June/9th (Fri) PM(1) Session o-4-1 at Room A Session d-15 at Room B Session k-7 at Room C Minor Bodies & Deep Space Disaster Monitoring Orbit Control Exploration (3) Chairperson :H. Une (Geographical Survey Inst.) Chairperson :O. Montenbruck (DLR) Chairperson :H. Yano (JAXA) M. Hara (VTI Research Inst.) S. Nakasuka (Tokyo Univ.) A. Galvez (ESA)

14:30-15:00 2006-o-4-01v 14:50-15:10 2006-d-76 14:40-15:00 2006-k-31 Earthquake Damage Detection by Satellite CALIPSO INSERTION AND MAINTE- Integrated Guidance and Navigation Strategy SAR Intensity Imagery NANCE IN THE AQUA TRAIN FORMA- for Flyby and Gas-Liquid Equilibrium Thruster M. Matsuoka, K. Horie (Earthquake Disaster Mitiga- TION for Small Satellite tion Research Center, NIED), H. Ohkura (National Re- C. Salcedo (CNES), France O. Mori (JAXA), K. Tarao (Tokyo Univ.), T. Ya- search Institute for Earth Science and Disaster Preven- mamoto, J. Kawaguchi (JAXA), Japan tion (NIED)), F. Yamazaki (Chiba Univ.), Japan 15:10-15:30 2006-d-77 EXPERIMENT OF AUTONOMOUS ORBIT 15:00-15:20 2006-k-32 15:00-15:30 2006-o-4-02v CONTROL ON DEMETER : IN-FLIGHT RE- Development of gas-liquid equilibrium thruster Monitoring Active Volcano with ASTER SULTS for the small satellite M. Urai (Geological Survey of Japan, AIST), Japan A. Lamy, M. Charmeau, R. Bertrand, D. Laurichesse T. Yamamoto, O. Mori, M. Shida (JAXA/ISAS), (CNES), France Japan 15:30-16:00 2006-o-4-03v ALOS follow-on type satellites program con- 15:30-15:50 2006-d-78 15:20-15:40 2006-k-33 cept for JAXA Disaster/Crisis management Coupled Inclination and Eccentricity Control Periodic Orbits in Binary Asteroids Systems program for MetOp Utilizing Low Thrust Propulsion M. Kojima, Y. Osawa, M. Shimada, Y. Iida (Oﬃce of O. Luengo (EUMETSAT (under GMV consultancy)), M. Morimoto (National Astronomical Observatory), H. Space Application, JAXA) et.al., Japan P. Righetti (EUMETSAT), Spain Yamakawa (JAXA), Japan

15:50-16:10 2006-d-79 15:40-16:00 2006-k-34 The orbit control of Integral using momentum Search the Optimal Launch Opportunities for dumping manoeuvres aiming for an optimal Interplanetary Mulitple Encounter Mission Us- ground station coverage ing the Genetic Algorithm M. Rosengren (European Space Operation Centre), D. Qiao, P. Cui, H. Cui (Deep Space Exploration Re- Germany search Center, Harbin Institute of Technology), China

16:10-16:30 2006-d-80 16:00-16:20 2006-k-35 Autonomous Regulation of Spacecraft Motion MISSIONS TO THE EDGE OF THE SO- About Unstable Periodic Orbits Using Impul- LAR SYSTEM USING A NEW ADVANCED sive maneuvers DUAL-STAGE GRIDDED ION THRUSTER H. Fukuzawa (ESTECH CORP.), Japan WITH VERY HIGH SPECIFIC IMPULSE R. Walker, D. Izzo (ESA/ESTEC), D. Fearn (EP So- lutions), R. Walker (ESA/ESTEC), Netherlands June/9th (Fri) PM(1) Session e-4 at Room D Session g-3 at Room E Session t-1 at Room F System Engineering and Information Entry Plasma Flow Diagnostics Technology (1) Chairperson :H. Kawazoe (Tottori Univ.) Chairperson :M. Yoshida (JAXA) Chairperson :K. Tachi (JAXA) H. Ogawa (JAXA/ISAS) S.Ishimoto (JAXA) O.L de Weck (MIT)

14:30-14:50 2006-e-13 14:30-14:50 2006-g-11 14:40-15:00 2006-t-01 Spectroscopic temperature measurements in Conceptual Study of Hybrid Re-Entry Vehicle Knowledge Management by using IT in JAXA the plenum region of a Huels type arc heated for Future Manned Space Flight S. Sobue, T. Sano, Y. Tanaka (JAXA), Japan wind tunnel Y. Yamamoto (JAXA), Japan K. Kitagawa, Y. Miyagawa, K. Inaba (Aichi Institute 15:00-15:20 2006-t-02 of Technology), N. Yoshikawa (Nagoya Univ.) et.al., 14:50-15:10 2006-g-12 Using Space Engineering Evaluation from Im- Japan Drop Test for Recovery System with a Mem- agery Technologies (USEEIT) to Support Ex- brane Aeroshell Using a Large Scientiﬁc Bal- ploration and Discovery 14:50-15:10 2006-e-14 loon J. C Casas (NASA), R. Merrell (Medical Informat- Diagnostics of Arc-heater Plumes by Cavity En- T. Hirotani, K. Yamada (JAXA), A. Sakurai (Kyushu ics and Technology Applications Consortium,Virginia hanced Absorption spectroscopy Univ.), K. Suzuki (Tokyo Univ.) et.al., Japan Commonwealth Univ.), D. Boyle (SpaceCraft Technol- H. Takayanagi, M. Matsui, K. Komurasaki, Y. ogy Center, Texas A&M Univ.), G. May (ProVision Arakawa (Tokyo Univ.), Japan 15:10-15:30 2006-g-13 Technologies) et.al., USA The automatic-ﬂight experiment of small-size 15:10-15:30 2006-e-15 Parafoil from a balloon 15:20-15:40 2006-t-11 Radiative Characteristics of Arc-discharged K. Hiraki, Y. Saito, Y. Mizuta, M. Inoue (Kyusyu In- Detecting Failure of Spacecraft Using Separated Micro-air Plasma-jets at Low Pressures stitute of Technology), Japan States in Particle Filters K. Kubota, M. Funatsu, H. Shirai, F. Takakusagi T. Murakami (Tokyo Institute of Technology), Y. (Gunma Univ.), Japan 15:30-15:50 2006-g-14 Kawahara (Tokyo Univ.), K. Takadama (Tokyo Insti- JAXA/CNES/ONERA Cooperation on the Re- tute of Technology), Japan 15:30-15:50 2006-e-16 search for HSFD2 Guidance and Control Radiative Characteristics of N2 Second Positive T. Tsukamoto, H. Suzuki, T. Ninomiya (JAXA), F. 15:40-16:00 2006-t-04 Bands of Microwave-discharged Plasmas Jouhaud (ONERA) et.al., Japan INFORMATION ARCHITECTURE TECH- K. Shibusawa, K. Shibusawa, M. Funatsu, H. Shirai NOLOGIES OF PANEL EXTENSION SATEL- (Gunma Univ.) et.al., Japan LITE T. Okada (SOHLA), S. Nakasuka, Y. Nakamura, Y. Sugawara (Tokyo Univ.) et.al., Japan

16:00-16:20 2006-t-05 Safety design of Centrifuge Rotor for excessive rotor motion T. Takegai (NEC TOSHIBA Space Systems, Ltd.), N. Sato, T. Nakano (JAXA), R. Okamura (NEC TOSHIBA Space Systems, Ltd.) et.al., Japan June/9th (Fri) PM(1) Session m-2 at Room G Session j-3 at Room H Astrophysics GEO Satellite Communication and Broadcasting

Chairperson :S. Torii (Waseda Univ.) Chairperson :T. Ikegami (Meiji Univ.) K. Yoshimura (High Energy R. Suzuki (NICT) Accelerator Research Organization) 14:30-14:50 2006-j-10 14:30-14:50 2006-m-05 Study of Integrating Ku-band Satellite Network with Ter- The Observation Results of High Energy Cosmic restrial GSM Cellular Network for Implementing the En- Rays Obtained by the RUNJOB Long-duration hanced Location-Based Services Balloons J. Suryana, S. Hartono (STEI ITB), S. Hassan (USM Malaysia), M. Hareyama (Waseda Univ.), Japan K. Igarashi (NiCT Japan) et.al., Indonesia

14:50-15:10 2006-m-06 14:50-15:10 2006-j-11 The first BESS-Polar flight over Antarctica Characteristics of Satellite System with Wideband K. Yoshimura, A. Yamamoto, S. Haino, M. Hasegawa Spreading Signals overlaid on FDMA Signals within the (High Energy Accelerator Research Organization (KEK)) Same FSS Network et.al., Japan N. Fuke, K. Sugiyama (KDDI R&D Laboratories), N. Kawai (KDDI), Japan 15:10-15:30 2006-m-07 Cosmic-Ray Electron Energy Spectrum above 100 15:10-15:30 2006-j-12 GeV by Polar Patrol Balloon in Antarctica S-Band Digital Multimedia Satellite Boadcasting Services K. Yoshida (Shibaura Institute of Technology), S. Torii (Moba-HO!) for Personal & Mobile Users in Japan (Waseda Univ.), T. Yamagami (JAXA), T. Tamura (Kana- Y. Yamaguchi (MBCO), Japan gawa Univ.) et.al., Japan 15:30-15:50 2006-j-13 15:30-15:50 2006-m-08 Improvement in Power Efficiency of Miniature TWT for An overview and initial results of the X-ray As- 21-GHz-band Onboard Phased Array Antenna tronomy Satellite K. Yamagata, K. Yamagata, S. Tanaka, K. Imai (Japan Broad- T. Dotani (JAXA), Japan casting Corporation), Japan

15:50-16:10 2006-m-09 15:50-16:10 2006-j-14 Development Status of Monitor of All-sky X-ray A proposed method for applying a Ku-band device to the Image (MAXI) on ”KIBO” S-band ¡Aiming to track ETS-VIII satellite to transmit K. Kawasaki, M. Matsuoka, S. Ueno, H. Tomida (JAXA) vital data from life vest on sea surface ¿ et.al., Japan I. Nakajima, H. Juzoji, K. Nagami (Tokai Univ. School of Medicine), N. Hamamoto (NICT) et.al., Japan 16:10-16:30 2006-m-10 Infrared Astronomical Satellite: ASTRO-F 16:10-16:30 2006-j-15 H. Shibai (Nagoya Univ.), Japan Automatic Satellite Tracking Dish Antenna System for Broadband IP based Ambulance Telemedicine J. Suryana, S. Hartono (Institut Teknologi Bandung), S. Has- san (USM Malaysia), K. Tanaka (NICT) et.al., Indonesia June/9th (Fri) PM(2) Session o-4-2 at Room A Session d-16 at Room B Session k-8 at Room C Minor Bodies & Deep Space Disaster Information Attitude and Orbit Control System Exploration (4) Chairperson :M. Kawamura (Toyohashi Univ. Chairperson :J. O’Donnell (NASA/GSFC) Chairperson :H. Yano (JAXA) of Tech.) T. Iwata (JAXA/IAT) A. Galvez (ESA) A. Takeda (Tohoku Bunka Gakuen) 16:40-17:00 2006-d-81 16:30-16:50 2006-k-36 Development and 3D Motion Experiments of Small A Solar Power Sail Mission for A Jovian Orbiter 16:10-16:40 2006-o-4-04v Spin Axis Controller and Trojan Asteroid Flybys Detection of Crustal Deformation of the North- T. Saiki, Y. Tsuda (ISAS/JAXA), M. Matsumoto, K. J. Kawaguchi (JAXA), Japan ern Pakistan Earthquake by Satellite Data Tarao (Tokyo Univ.) et.al., Japan U. Hiroshi, S. Fujiwara, M. Tobita, S. Ozawa (Geo- 16:50-17:10 2006-k-39 graphical Survey Institute) et.al., Japan 17:00-17:20 2006-d-82 SMALL JOVIAN ORBITER FOR MAGNE- GNC for an automatic ISS survey vehicle (ASVIS) TOSPHERIC AND AURORAL STUDIES 16:40-17:10 2006-o-4-05v L. Strippoli, D. Modrego, P. Colmenarejo (GMV), J. Y. Kasaba, T. Takashima (ISAS/JAXA), H. Misawa Development of Centralized Multimedia Infor- Manuel Del cura (SENER) et.al., Spain (Planetary Plasma and Atmospheric Research Cen- mation and Data Sharing System for Mid- ter, Tohoku Univ.), J. Kawaguchi (ISAS/JAXA) et.al., disaster Evacuation Process 17:20-17:40 2006-d-83 Japan M. Hara, H. Yagi, K. Lwin (VTI), Japan The Space Technology-7 Disturbance Reduction System Precision Control Flight Validation Exper- 17:10-17:30 2006-k-44 iment Control System Design Solar sail-based interplanetary communication J. R O’donnell, O. C Hsu, P. G Maghami, F. Landis network Markley (NASA Goddard Space Flight Center), USA L. Hartman (Canadian Space Agency), Canada

17:40-18:00 2006-d-84 17:30-17:50 2006-k-37 Design and On-orbit Evaluation of Attitude Con- MICROSATELLITE-CLASS SOLARSAIL trol System for Small Scientific Satellite “REIMEI” DEMONSTRATOR —MISSION DESIGN S. Sakai, Y. Fukushima, H. Saito (JAXA), Japan AND DEVELOPMENT STATUS Y. Tsuda, K. Nakaya, T. Saiki, O. Mori (ISAS/JAXA) 18:00-18:20 2006-d-85 et.al., Japan Spacecraft Attitude and Body Rate Estimation with Star Sensors and Their On-Orbit Verification 17:50-18:10 2006-k-38 Results Spinning Solar Sail With Rotationally Skew S. Yoshikawa, H. Shimoji, K. Miyatake, H. Kawano (Mit- Fold Membrane For Solar System Exploration subishi Electric Corporation) et.al., Japan H. Furuya, Y. Inoue (Tokyo Institute of Technology), Japan 18:20-18:40 2006-d-86 Automated Transfer Vehicle (ATV) Flight Dynam- ics System M. Molina, J. Lozano, L. Alvarez (GMV SA), P. Des- mazeaux (CNES) et.al., Spain June/9th (Fri) PM(2) Session e-5 at Room D Session g-4 at Room E Session t-2 at Room F System Engineering and Information Plasma Flow Facilities Reusable Rocket Technology (2) Chairperson :K. Hiraki (Kyushu Inst. of Tech.) Chairperson :T. Mori (MHI) Chairperson :K. Takadama K. Suzuki (Tokyo Univ.) H. Ogawa (JAXA) (Univ. of Electro-Communications) G. Motet (National Inst. in 16:00-16:20 2006-e-17 16:00-16:20 2006-g-15 Applied Science) Performance of Zirconium Cathode Arc-heater Aerodynamic Studies on Vertical Landing of as Atomic Oxygen Generator Reusable Rocket Vehicle 16:30-16:50 2006-t-06 M. Matsui, T. Ikemoto, H. Takayanagi, K. Komurasaki S. Nonaka, T. Suzuki, K. Watanabe, H. Ogawa Independent Verification and Validation for (Tokyo Univ.) et.al., Japan (ISAS/JAXA) et.al., Japan space program Y. Miyamoto, Y. Miyamoto, M. Katahira (JAXA), H. 16:20-16:40 2006-e-18 16:20-16:40 2006-g-16 Nakao (JAMSS), Japan Spectroscopic study of a laser-sustained plasma Evaluation of Engine Cycles for Small Engineer- supersonic jet ing Test Rocket Engine 16:50-17:10 2006-t-07 T. Inoue, T. Hirasawa, Y. Arakawa, K. Komurasaki M. Sato, R. Nakatani, T. Kimura, T. Hashimoto IV&V activities for H-II Transfer Vehicle’s (Tokyo Univ.), Japan (JAXA) et.al., Japan Avionics Safety Design S. Shirasaka (Mitsubishi Electric Corporation), K. 16:40-17:00 2006-e-19 16:40-17:00 2006-g-17 Nakamura (JAXA), Japan Performance Characteristics of the Inductively- Current Status of Development of A Small En- Coupled High Enthalpy Flow Generator with gineering Test Rocket Engine 17:10-17:30 2006-t-08 CO2 Gas M. Yoshida, H. Aoki, H. Hukuzoe, Y. Naruo (JAXA) H-II Transfer Vehicle’s End-To-End Test Con- T. Yamada (ISAS/JAXA), K. Fujita (ISTA/JAXA), et.al., Japan cept S. Nonaka, N. Ishii (ISAS/JAXA), Japan K. Kiritani (JAXA), S. Shirasaka (Mitsubishi Electric 17:00-17:20 2006-g-18 Corporation), Japan 17:00-17:20 2006-e-20 Performance Evaluation Tests of Small Turbop- Heat-resistance Experiments of SiC-based Ce- ump 17:30-17:50 2006-t-09 ramics in High-temperature Air Plasma-jets S. Takada, M. Yoshida, M. Kikuchi, T. Sudo (JAXA) ESOC Flight Dynamics Precise Emulators for M. Funatsu, M. Funatsu, K. Ito, H. Shirai (Gunma et.al., Japan the Cryosat, Herschel and Planck Missions: De- Univ.) et.al., Japan velopment and Applications 17:20-17:40 2006-g-19 S. Matteo Pessina, L. Tucci (Terma GmbH Application of Highly Reliable Design Method- c/o ESA/ESOC, OPS GFT), S. Kasten-coors ology to Liquid Rocket Engine Conceptual De- (ESA/ESOC, OPS GFT), Germany sign N. Kuratani, H. Aoki, R. Nakatani (JAXA), Y. Kawa- 17:50-18:10 2006-t-10 mata (MHI) et.al., Japan Study of Integrated Verification Environment for Spacecraft Onboard Software System H. O. Ueda, S. Ikeda, T. Takahashi (JEDI Center, JAXA), T. Kobori (Mitsubishi Space Software Co., Ltd), Japan June/9th (Fri) PM(2) Session m-3 at Room G Session j-4 at Room H Space and Balloon Technology WINDS Satellite

Chairperson :S. Matsunaga (Tokyo Inst. of Tech.) Chairperson :S. Tanaka (NHK) M. Natori (JAXA/ISAS) T. Ikegami (Meiji Univ.)

16:40-17:00 2006-m-11 16:40-17:00 2006-j-16 Experimental Study on folding and deployment of Development of High-speed Network for WINDS tape tether for a Sounding Rocket Experiment Y. Hashimoto, T. Takahashi, N. Yoshimura, R. Suzuki S. Nakafushi, H. A Fujii, T. Watanabe, T. Kikuchi (Tokyo (NICT) et.al., Japan Metropolitan Univ.) et.al., Japan 17:00-17:20 2006-j-17 17:00-17:20 2006-m-12 Active Phased Array Antenna for WINDS Measurement of the Deployment Drag for Design- M. Yajima, T. Kuroda, T. Maeda, M. Shimada (JAXA) ing of the Foldaway Tape Tether Deployer et.al., Japan T. Watanabe, H. A Fujii, T. Kikuchi, S. Nakafushi (Tokyo Metropolitan Univ.) et.al., Japan 17:20-17:40 2006-j-18 Ka band High Power Multi-port Ampliﬁer (MPA) 17:20-17:40 2006-m-13 for WINDS Satellite Short to Long Duration Balloon Flights from ES- T. Kuroda, M. Yajima, M. Shimada (JAXA), M. Kitahara RANGE (C-TECH) et.al., Japan S. Kemi, O. Norberg (Swedish Space Corporation), Sweden 17:40-18:00 2006-j-19 Study of Secured and Reliable Wideband IP-based Videoconference over Ka-band WINDS Satellite Link between Bandung-Tokyo J. Suryana, S. Hartono (Institut Teknologi Bandung), K. Umeno, K. Igarashi (NICT) et.al., Indonesia

18:00-18:20 2006-j-20 Spatial Temporal Rainfall Model for Evaluating the Performance of Ka-band Satellite Links with Site Diversity J. Suryana, S. Hartono (Institut Teknologi Bandung), K. Tanaka, K. Igarashi (NICT) et.al., Indonesia

18:20-18:40 2006-j-21 Study of Ka-band Satellite Link Performance at High Intense Rain Cities in Indonesia using WINDS J. Suryana, S. Hartono (Institut Teknologi Bandung), K. Tanaka, K. Igarashi (NICT) et.al., Indonesia June/9th (Fri) PM(3) Session o-4-3 at Room A Session e-6 at Room D Session g-5 at Room E Data Arcive & Application Atomospheric Flight Vehicle Concepts Demo Flight

Chairperson :M. Arakida (Asian Disaster Chairperson :M. Funatsu (Gunma Univ.) Chairperson :Y. Yamamoto (JAXA) Reduction Center) H. Tanno (JAXA/ISAS) T. Tsukamoto (JAXA) M. Matsuoka (Earthquake Disaster Mitigation Research Center) 17:30-17:50 2006-e-21 17:50-18:10 2006-g-20 Experimental Study on Shock-Shock Interac- Development Plan of a Small-scale Supersonic 17:20-17:50 2006-o-4-06v tion Wave-rider Flight Experiment Vehicle in Cooperation be- Development of Sediment Disaster Mitigation GIS T. Kurokawa, H. Kawazoe (Tottori Univ.), . Fujii, T. tween Universities by Using High Resolution Satellite Imagery and Irikado (JAXA), Japan K. Mizobata, R. Minato, N. Tanatsugu, H. Kimura Forest Database (Muroran Institute of Technology) et.al., Japan M. Kawamura (Toyohashi Univ. of Technology), K. Tsu- 17:50-18:10 2006-e-22 jino (Fukui National Coleege of Technology), Y. Ohtsuji Experimental Investigation of the Interaction 18:10-18:30 2006-g-21 (Toyohashi Univ. of Technology), Japan between Applied Magnetic Field and Weakly Flight Trajectory Analysis of a Small-scale Su- Ionized Plasma personic Flight Experiment Vehicle 17:50-18:20 2006-o-4-07v M. Kawamura (Tokyo Univ.), K. Wakatsuki (Tokai H. Kimura, S. Hada, K. Mizobata, R. Minato (Muroran Applications of Long TermSatellite Data Archives Univ.), A. Matsuda (JAXA), Y. Takizawa (Tokyo Institute of Technology) et.al., Japan on Retrieval of the Time Serial Spatial Information Univ.) et.al., Japan such as Past Disaster Events 18:30-18:50 2006-g-22 T. Atsushi (Tohoku Bunka Gakuen Univ.), Japan 18:10-18:30 2006-e-23 Preliminary Design of a Small-scale Turbojet Aerothermodynamic Studies on Low-Ballistic- Engine for a Supersonic Flight Experiment Ve- Coeﬃcient Jovian Entry Probe with Membrane hicle Aeroshell R. Minato, I. Tokura, N. Tanatsugu (Muroran Institute K. Suzuki (Tokyo Univ.), Japan of Technology), T. Himeno (Univ. of Tokto) et.al., Japan 18:30-18:50 2006-e-24 A Study on Water-Impact Shock of Reentry 18:50-19:10 2006-g-23 Capsule Flight Demonstration of Subscale Precooled K. Hiraki, K. Ideno, E. Ide, M. Inoue (Kyushu Institute Turbojet Engine Onboard Balloon-based Oper- of Technology), Japan ation Vehicle K. Fujita (IAT/JAXA), S. Sawai (ISAS/JAXA), H. Kobayashi, H. Taguchi (IAT/JAXA) et.al., Japan