Tentative Program

 

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Organized Session
[o-1-1] Interorbital and Interplanetary Transportation with EP 1

Session Date June 6 (Tue) 9:20 – 10:40
Room Pearl Room B
Chairpersons
2017-o-1-01 ( 9:20 – 9:40 )
Nuclear Electric Propulsion to EUROPA and MARS
Frank Jansen1, Frédéric MASSON2, Jean-Claude WORMS3, Emmanouil DETSIS3, Francois LASSOUDIERE4, Richard GRANJON5, Maria Cristina TOSI6, Simona FERRARIS6, Anatoly S. KOROTEEV7, Alexander V. SEMENKIN7, Alexander SOLODUKHIN7, Tim TINSLEY8, Zara HODGSON8, Lamartine Nogueira Frutuoso GUIMARÃES9, Tim Brandt 1, James Ap. Findlay8, Stephane Oriol 2
1Institute of Space Systems Bremen, DLR, Germany , Germany, 2CNES, Paris, France, 3European Science Foundation, Strasbourg, France , 4Airbus Safran Launchers, Vernon, France , 5Sagem Défense Sécurité, Valence, France , 6Thales Alenia Space, Torino, Italy, 7Keldych Research Centre, Moscow, Russia, 8National Nuclear Laboratory, Sellafield, United Kingdom, 9Instituto de Estudos Avançados, São José dos Campos; Brazil
2017-o-1-02 ( 9:40 – 10:00 )
Return Trajectory of Martian Moons eXplorer by way of Chemical-Electric Hybrid Propulsion
Makoto Horikawa1, Kazutoshi Takemura2, Takanao Saiki3, Yasuhiro Kawakatsu3, Hiroaki Yoshimura2
1Department of Applied Mechanics, Waseda University, Japan, 2Department of Applied Mechanics and Aerospace Engineering, Waseda University, 3Japan Aerospace Exploration Agency
2017-o-1-04 ( 10:00 – 10:20 )
Highlights of Electric Sail Propulsion Efforts at NASA’s Marshall Space Flight Center
Bruce M Wiegmann1, Andy Heaton1, Michal Bangham3, Robert Hoyt2
1Marshall Space Flight Center, NASA, USA, 2Tethers Unlimited, Inc., 3Bangham Engineering, Inc.
2017-o-1-05 ( 10:20 – 10:40 )
Dynamics of Single Charged Wire for Solar Wind Electric Sail
Fei Liu, Quan Hu, Jingrui Zhang, Keying Yang, Yanyan Li
School of Aerospace Engineering, Beijing Institute of Technology, China
[o-1-2] Interorbital and Interplanetary Transportation with EP 2

Session Date June 6 (Tue) 11:00 – 12:00
Room Pearl Room B
Chairpersons
2017-o-1-06 ( 11:00 – 11:20 )
Investigation of scaling laws for electrical thrusters by use of Particle-in-Cell simulations
Tim Brandt
Systems Enabling Technolgies, German Aerospace Center (DLR), Germany
2017-o-1-07 ( 11:20 – 11:40 )
Development of a Numerical Tool for Hall Thruster Plume and Spacecraft Interaction Analysis
Takanobu Muranaka1, Yasutaka Inanaga2
1Department of Electrical and Electronic Engineering, School of Engineering, Chukyo University, Japan, 2Advanced Technology R&D Center, Mitsubishi Electric
2017-o-1-08 ( 11:40 – 12:00 )
Two-Head Operations of Hall Thruster
Tomohiro Kita1, Takeshi Miyasaka2, Masahiro Sakoda1, Yoshimi Miyake1, Kazuya Oishi1, Ryo Kawamura1, Yuki Mamiya2, Kohei Kurita1, Hiroki Kanie2, Makoto Asahara2
1Department of Human and Information Systems, Gifu University, Japan, 2Department of Mechanical Engineering, Gifu University
[o-2-1] Launch Vehicle for Small Spacecrafts (1)

Session Date June 6 (Tue) 9:00 – 10:20
Room Meeting Room 7
Chairpersons
2017-o-2-01 ( 9:00 – 9:20 )
Compact and High Performance Rocket Design of Epsilon and Future Prospect of Solid Propellant Launch Vehicles
Yasuhiro Morita
Dept. of Space Flight Systems, ISAS/JAXA, Japan
2017-o-2-02 ( 9:20 – 9:40 )
Epsilon Launch Vehicle – Second Flight and its Evolutions –
Tatsuya Kanechika1, Kazuhiro Yagi1, Takayuki Imoto2
1Rocket Systems Department, IHI Aerospace Co., Ltd., Japan, 2JAXA
2017-o-2-03 ( 9:40 – 10:00 )
Development and Flight Results of Solid Propulsion System for Enhanced Epsilon Launch Vehicle
Koki Kitagawa1, Shinichiro Tokudome1, Keiichi Hori1, Haruhito Tanno2, Nobuyuki Nakano2
1Department of space flight systems, Institute of Space and Astronautical Science, JAXA, Japan, 2Solid Propulsion Office, Rocket Systems Dept., IHI Aerospace
2017-o-2-04 ( 10:00 – 10:20 )
Development and Flight Results of Structure Subsystem for Enhanced Epsilon Launch Vehicle
Hiroshi Ikaida, Kyoichi Ui, Toru Kamita, Ken Goto, Kenji Minesugi
Japan Aerospace Exploration Agency, Japan
[o-2-2] Launch Vehicle for Small Spacecrafts (2)

Session Date June 6 (Tue) 11:00 – 12:00
Room Meeting Room 7
Chairpersons
2017-o-2-05 ( 11:00 – 11:20 )
Conceptual Study of Japan’s Future Solid Rocket System
Shinichiro Tokudome1, Yasuhiro Saitoh2, Takayuki Yamamoto3, Koji Nakaya4, Tetsuya Ono4, Toshiaki Hara4, Yoshitaka Mochihara4, Hiroshi Ikaida4, Ryoma Yamashiro4
1Department of Space Flight Systems, Institute of Space and Astronautical Science, JAXA, Japan, 2The 4th Research Unit, Research and Development Directorate, JAXA, 3The 1st Research Unit, Research and Development Directorate, JAXA, 4Epsilon Rocket Project Team, Space Technology Directorate I, JAXA
2017-o-2-06 ( 11:20 – 11:40 )
Initial guess generation strategies for spaceplane trajectory optimisation
Federico Toso, Christie Alisa Maddock
Department of Mechanical and Aerospace Engineering, University of Strathclyde, UK
2017-o-2-07 ( 11:40 – 12:00 )
The low cost rocket with Low Melting Temperature Thermoplastic Propellant
Hikaru Isochi1, Hikaru Otabe1, Tsutomu Uematsu1, Nobuji Kato2, Keiichi Hori3, Yasuhiro Morita3, Ryojiro Akiba4
1Uematsu Electric Co.,Ltd., Japan, 2Katazen, 3JAXA, 4HASTIC
[o-3-1] Future Space Transportation System (1)

Session Date June 6 (Tue) 14:00 – 15:40
Room Meeting Room 7
Chairpersons
2017-o-3-01 ( 14:00 – 14:20 )
Technical and Flight Demonstrations for Reusable Launch Vehicle
Satoshi Nonaka, Takashi Ito, Yoshifumi Inatani
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan
2017-o-3-02 ( 14:20 – 14:40 )
Trajectory Optimization for a Reusable Sounding Rocket
Shunsuke Sato1, Takayuki Yamamoto1, Takahiro Nakamura2, Satoshi Nonaka2
1Research Unit 1, Research and development Directorate, JAXA, Japan, 2Department of Space Flight Systems, Institute of Space and Astronautical Science (ISAS), JAXA
2017-o-3-03 ( 14:40 – 15:00 )
Numerical analysis on reusable rocket aerodynamics with reduced-yaw-force configurations
Ayano Inatomi1, Keiichi Kitamura1, Satoshi Nonaka2
1College of Engineering Science, Yokohama National University, Japan, 2The Institute of Space and Astronautical Science, JAXA
2017-o-3-04 ( 15:00 – 15:20 )
Computational Study on Finned Reusable Rocket at High-Angle-of-Attack
Takuya Aogaki1, Keiichi Kitamura1, Satoshi Nonaka2
1Graduate School of Engineering, Yokohama National University, Japan, 2The Institute of Space and Astronautical Science, JAXA
2017-o-3-05 ( 15:20 – 15:40 )
Anomaly Detection Configured as a Combination of State Observer and Mahalanobis-Taguchi Method for a Rocket Engine
Yusuke Maru1, Hatsuo Mori2, Takashi Ogai2, Noriyoshi Mizukoshi2, Shinsuke Takeuchi1, Takayuki Yamamoto1, Tsuyoshi Yagishita1, Satoshi Nonaka1
1Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan, 2IHI corporation
[o-3-2] Future Space Transportation System (2)

Session Date June 6 (Tue) 16:00 – 17:20
Room Meeting Room 7
Chairpersons
2017-o-3-06 ( 16:00 – 16:20 )
Low Cost Reusable 1st Stage Launch Services From International Spaceports
Charles John Lauer
Rocketplane Global LLC, USA
2017-o-3-07 ( 16:20 – 16:40 )
The ispace Commercial Lunar Transportation System
Chit Hong Yam, Takeshi Hakamada, Mohamed Ragab
ispace inc., Japan
2017-o-3-08 ( 16:40 – 17:00 )
Utilizing Near Earth Asteroid as a Cycler (UNEAC) Concept: A Subsequent Study of ‘Near Earth Asteroid as an Alternative Interplanetary Manned Spaceship’ Proposal
Huai-Chien Chang
Consortium of Spacce Settlements, Astronautical Society of Taiwan., Taiwan
2017-o-3-09 ( 17:00 – 17:20 )
Cable Dynamics and It’s Control at the Simultaneous Deployment of the Cables from GEO Station during Space Elevator Construction
Yoshiki Yamagiwa1, Koki Tao1, Kiyotoshi Otsuka2, Yoji Ishikawa2
1Faculty of Engineering, Shizuoka University, Japan, 2Obayashi Corporation
[o-3-3] Future Space Transportation System (3)

Session Date June 7 (Wed) 9:00 – 10:40
Room Meeting Room 7
Chairpersons
2017-o-3-10 ( 9:00 – 9:20 )
Conceptual Design Investigation and Aerodynamic Study for Hypersonic Vehicle Baseline Configuration
Shigeru ASO, Yasuhiro Tani, Takaaki Hirayama
Department of Aeronautics and Astronautics, Kyushu University, Japan
2017-o-3-11 ( 9:20 – 9:40 )
Multi-Objective Design Optimisation of RBCC-Based Orbital TSTO Space Transportation Systems for Multi-Asset Deployment
George Nicholas Coulloupas, Hideaki Ogawa
School of Engineering, RMIT University, Australia
2017-o-3-12 ( 9:40 – 10:00 )
Detailed Design Status of Experimental Winged Rocket WIRES#015 with Liquid Methane Engine
Eiji Kamemoto1, Koichi Yonemoto1, Takahiro Fujikawa1, Hiroshi Yamasaki1, Masatomo Ichige1, Yusuke Ura1, Guna Surendra Gossamsetti1, Takumi Ohki1, Yuki Kubono1, Kento Shirakata1, Hirotoshi Tsukamoto1, Hayato Tobiyama1, Yasuaki Matsuoka1, Takumi Yano1, Toshiki Morito2, Toshiki Kato2
1Mechanical and Control Engineering, Kyushu Institute of Technology, Japan, 2Japan Aerospace Exploration Agency
2017-o-3-13 ( 10:00 – 10:20 )
Development Status of Experimental Winged Rocket WIRES#014-3A
Hayato Tobiyama1, Koichi Yonemoto1, Takahiro Fujikawa1, Hiroshi Yamasaki1, Masatomo Ichige1, Yusuke Ura1, Guna Surendra Gossamsetti1, Takumi Ohki1, Yuki Kubono1, Kento Shirakata1, Hirotoshi Tsukamoto1, Yasuaki Matsuoka1, Takumi Yano1, Shinji Ishimoto2, Takashi Mugitani2
1Kyushu Institute of Technology, Japan, 2Japan Aerospace Exploration Agency (JAXA)
2017-o-3-14 ( 10:20 – 10:40 )
Conceptual Design Optimization of Several Types of Fully Reusable Winged Launch Vehicles
Takahiro Fujikawa, Koichi Yonemoto
Department of Mechanical and Control Engineering, Kyushu Institute of Technology, Japan
[o-4-1] Oxygen/Methane Rocket Combustion and Heat Transfer (1)

Session Date June 6 (Tue) 9:00 – 10:20
Room Meeting Room 8
Chairpersons
2017-o-4-01 ( 9:00 – 9:20 )
Experimental and Numerical Investigation of Flow and Combustion in a Single Element Rocket Combustor using GH2/GOX and GCH4/GOX as Propellants
Christof Martin Roth, Simona Silvestri, Maria Palma Celano, Oskar Haidn
Institute of Turbomachinery and Flight Propulsion, Technical University of Munich, Germany
2017-o-4-02 ( 9:20 – 9:40 )
Heat Flux Estimation on a Chamber Wall of GH2/GOX and GCH4/GOX Single Element Rocket Combustor
YU DAIMON1, Hideyo Negishi1, Roman Keller2, Peter M. Gerlinger2
1Research and Development Directorate, Japan Aeropace Exploration Agency, Japan, 2IVLR, University of Stuttgart
2017-o-4-03 ( 9:40 – 10:00 )
Numerical investigation of single injector methane model rocket combustors with round and squared cross-section
Roman Keller1, Peter Gerlinger1, Yu Daimon2, Christof Roth3, Oskar J. Haidn3
1Institute of Combustion Technology for Aerospace Engineering, University of Stuttgart, Germany, 2Japan Aerospace Exploration Agency, 305-8505 Tsukuba, Ibaraki, Japan, 3Technische Universitat Munchen, 80333 Munich, Germany
2017-o-4-04 ( 10:00 – 10:20 )
Numerical Investigation of Eigenmode Damping Rates in a Single Element Rocket Combustion Chamber
Alexander Chemnitz, Nancy Kings, Moritz Schulze, Thomas Sattelmayer
Institute for Thermodynamics, Technische Universitaet Muenchen, Germany
[o-4-2] Oxygen/Methane Rocket Combustion and Heat Transfer (2)

Session Date June 6 (Tue) 11:00 – 12:20
Room Meeting Room 8
Chairpersons
2017-o-4-05 ( 11:00 – 11:20 )
Gaseous Film Cooling Investigation in a Multi-element Subscale GCH4-GOX Combustion Chamber
Maria Palma Celano, Simona Silvestri, Oskar J. Haidn
Lehrstuhl fuer Turbomaschinen und Flugantriebe, Germany
2017-o-4-06 ( 11:20 – 11:40 )
Subscale Firing Test for Regenerative Cooling LOX/Methane Rocket Engine
Toshiki Kato1, Daiki Terakado1, Hideaki Nanri1, Toshiki Morito1, Ideo Masuda1, Hiroya Asakawa2, Hiroyuki Sakaguchi2, Yasuhiro Ishikawa2, Takuma Inoue3, Shinji Ishihara3, Masahiro Sasaki3
1Research and Development Directorate, Japan Aerospace Exploration Agency, Japan, 2Aero-Engine & Space Operation Space Development Department, IHI Corporation, 3Space System Department, IHI Aerospace
2017-o-4-07 ( 11:40 – 12:00 )
Laser ignition of a multi-injector LOx/methane combustor
Michael Boerner1, Chiara Manfletti2, Justin Hardi1, Dmitry Suslov1, Gerhard Kroupa3, Michael Oschwald1
1Institute of Space Propulsion, German Aerospace Center (DLR), Germany, 2European Space Agency (ESA), 3CTR Carinthian Tech Research AG
2017-o-4-08 ( 12:00 – 12:20 )
Feasibility Study on Additive Manufacturing of Liquid Rocket Combustion Chamber
Shinichi Moriya1, Takuma Inoue2, Masahiro Sasaki2, Takayuki Nakamoto3, Takahiro Kimura3, Naoyuki Nomura4, Akira Kawasaki4, Toshiki Kato1, Ideo Masuda1
1JAXA, Japan, 2IHI Aerospace Co., Ltd., 3Technology Research Institute of Osaka Prefecture, 4Tohoku University
[o-4-3] Oxygen/Methane Rocket Combustion and Heat Transfer (3)

Session Date June 6 (Tue) 14:00 – 15:00
Room Meeting Room 8
Chairpersons
2017-o-4-09 ( 14:00 – 14:20 )
Experimental and Numerical Investigation of a Multi-Injector GOX-GCH4 Combustion Chamber
Simona Silvestri1, Maria Palma Celano1, Gregor Schlieben1, Christoph Kirchberger2, Oskar Haidn1
1Department of Mechanical Engineering, Chair of Turbomachinery and Flight Propulsion, Technical University of Munich, Germany, 2German Aerospace Center
2017-o-4-10 ( 14:20 – 14:40 )
Numerical Investigation of Injector Configurations in GOX/GCH4 Rocket Combustion Chambers
Christian Bauer, Simona Silvestri, Maria Palma Celano, Oskar Haidn
Institute for Turbomachinery and Flight Proplusion, Technische Universitaet Muenchen, Germany
2017-o-4-11 ( 14:40 – 15:00 )
Numerical Investigation for Recess Variation of a Shear Coax Injector in a GOX-GCH4 Combustion Chamber
YU DAIMON1, HIROUMI TANI1, HIROSHI TERASHIMA2
1Research and Development Directorate, Japan Aerospace Exploration Agency, Japan, 2Faculty of Engineering, Hokkaido University
[o-5-1] Hybrid Rocket for Space Transportation

Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 6
Chairpersons
2017-o-5-01 ( 9:00 – 9:30 )
Essentially Non-explosive Propulsion Paving a Way for Fail-Safe Space Transportation
Akiyo Takahashi, Toru Shimada
Institute of Space and Astronautical Science, JAXA, Japan
2017-o-5-02 ( 9:30 – 10:00 )
A Short Discussion on Performance, Safety and Environmental Aspects of Gel and Hybrid Rocket Propulsion Systems
Helmut K. Ciezki1, Karl-Wieland Naumann2, Mario Kobald1
1DLR – German Aerospace Center, Institute of Space Propulsion, Propellants Department, Germany, 2Bayern-Chemie GmbH, Business Development & Strategy, 84544 Aschau am Inn, Germany
2017-o-5-03 ( 10:00 – 10:20 )
Combined Trajectory Simulation and Optimization for Hybrid Rockets using ASTOS and ESPSS
Christian Schmierer1, Mario Kobald1, Johan Steelant2, Stefan Schlechtriem1
1Institute for Space Propulsion, German Aerospace Center, Germany, 2ESTEC, European Space Agency
2017-o-5-04 ( 10:20 – 10:40 )
Error Analysis for CAMUI type hybrid rocket regression simulationror Analysis for CAMUI type hybrid rocket regression simulation
Tor Viscor, Harunori Nagata
Mechanical and Space Engineering, University Hokkaido, Japan
[o-5-2] Development and Testing of Hybrid Rocket

Session Date June 6 (Tue) 11:00 – 12:40
Room Meeting Room 6
Chairpersons
2017-o-5-05 ( 11:00 – 11:30 )
Development of an Air-breathing Hybrid Rocket Booster
Yen-Sen Chen
Rocket Propulsion, TiSPACE Incorporated, Taiwan
2017-o-5-06 ( 11:30 – 12:00 )
A Record Flight of the Hybrid Sounding Rocket HEROS 3
Mario Kobald1, Christian Schmierer2, Ulrich Fischer1, Konstantin Tomilin1
1Institute of Space Propulsion, DLR, Germany, 2Stuttgart University
2017-o-5-07 ( 12:00 – 12:20 )
Engine Performance of a Swirling-Injection End-Burning Hybrid Rocket Engine using LOX/Paraffin-based Fuel
Kazuyuki Saito, Yuya Oishige, Daiki Hayashi, Takashi Sakurai
Department of aerospace engineering, Tokyo metropolitan university, Japan
2017-o-5-08 ( 12:20 – 12:40 )
Flow visualization in combustion chamber of Altering-intensity Swirling-Oxidizer-Flow-Type hybrid rocket engine
Kei Obata1, Toru Shimada2
1Aeronautics and Astronautics, University of Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA
[o-5-3] Internal Flow Dynamics of Hybrid Rocket

Session Date June 6 (Tue) 14:00 – 15:40
Room Meeting Room 6
Chairpersons
2017-o-5-09 ( 14:00 – 14:30 )
Internal Flow Dynamics and Stability in Hybrid Rocket Combustor with Swirl
Changjin Lee, Jungeun Kim, Sulha Lee
Department of Aerospace Engineering, Konkuk University, Korea
2017-o-5-10 ( 14:30 – 15:00 )
A Study on Module-Type Hybrid Rocket Engine with Multi-Section Swirl Injection Method for Optimum Combustion and Thrust Control
Shigeru ASO, Yasuhiro Tani, Masato Yamashita, Kazuya Komori, Tomohiro Yamasaki, Toru Shimada
Department of Aeronautics and Astronautics, Kyushu University, Japan
2017-o-5-11 ( 15:00 – 15:20 )
Delayed Detached Eddy Simulation of Combustive Flows in a Swirling-Oxidizer-Flow-Type Hybrid Rocket
Mikiro Motoe
Research and Development Directorate, Research Unit III, Japan Aerospace Exploration Agency, Japan
2017-o-5-12 ( 15:20 – 15:40 )
Preliminary Study on the Interaction Between Vortex Shedding and Acoustic Oscillations in Hybrid Rockets
Sungmin Lim1, Yohei Deguchi1, Yukihiro Kurosawa1, Takakazu Morita1, Jungpyo Lee2
1Tokai university, Department of aeronautics and astronautics, Japan, 2University of Brasilia
[o-5-4] Elemental Technologies for Hybrid Rocket

Session Date June 6 (Tue) 16:00 – 17:40
Room Meeting Room 6
Chairpersons
2017-o-5-13 ( 16:00 – 16:20 )
Numerical Optimization of the Torch Ignition System for the Hybrid Rocket Motor
Olexiy Shynkarenko, Domenico Simone, Artem Andrianov
Aerospace Engineering, University of Brasilia, Brazil
2017-o-5-14 ( 16:20 – 16:40 )
Flow in an oxidizer branch line of hybrid rockets
Daisuke Nakata1, Kazuki Yasuda1, Kugo Okada1, Kazuyuki Higashino1, Rikio Watanabe2
1Muroran Institute of Technology, Japan, 2Tokyo City University
2017-o-5-15 ( 16:40 – 17:00 )
Thermo-fluid Analysis of Hybrid Rocket with LOX Regenerative Cooling System
Tomoki Matsuno1, Toru Shimada2
1Department of Aeronautics and Astronautics, University of Tokyo, Japan, 2Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
2017-o-5-16 ( 17:00 – 17:20 )
Design and Experiment of a LOX Vaporization Nozzle for an A-SOFT Hybrid Rocket Engine
Tomokazu Mizukoshi, Tatsuya Takei, Takashi Sakurai
Department of Aerospace Engineering, Tokyo Metropolitan University, Japan
2017-o-5-17 ( 17:20 – 17:40 )
Investigation of Throttling Characteristics of End-Burning Hybrid Rockets
Yuji Saito1, Toshiki Yokoi1, Masaya Kimino1, Ayumu Tsuji1, Kazunobu Omura1, Hiroyuki Yasukochi2, Kentaro Soeda2, Tsuyoshi Totani1, Masashi Wakita1, Harunori Nagata1
1Department of Mechanical and Space Engineering, Hokkaido Univerisity, Japan, 2Institute for Photon Science and Technology, The University of Tokyo
[o-5-5] Fuels for Hybrid Rocket

Session Date June 7 (Wed) 9:00 – 10:40
Room Meeting Room 6
Chairpersons
2017-o-5-18 ( 9:00 – 9:20 )
A Measurement of Melting Fuel Behavior in Boundary Layer Combustion Type Hybrid Rockets
Ayana Banno1, Yo Kawabata1, Yutaka Wada1, Nobuji Kato2, Keiichi Hori3
1Department of Mechanical Science and Engineering, Chiba Institute of Technology, Japan, 2Katazen Corporation, 3ISAS/JAXA
2017-o-5-19 ( 9:20 – 9:40 )
Thermal behavior of aluminized wax-based solid fuel
Yui Murakami1, Yuki Matsumoto1, Reo Tanaka1, Kenichi Takahashi1, Ikkei Tanabe2, Mieko Kumasaki3
1College of Science and Technology, Nihon University, Japan, 2School of Engineering Science, Yokohama National University, 3Graduate school, Yokohama National University
2017-o-5-20 ( 9:40 – 10:00 )
Improvement of the regression rate of the hybrid rocket fuel by addition of the magnesium powder
Akira Takahashi, Raimu Kobayashi, Takamori Yamaguchi, Yuki Komori, Kenichi Takahashi
College of Science and Technology, Nihon University, Japan
2017-o-5-21 ( 10:00 – 10:20 )
Study on Wax Fuel for Hybrid Rockets
Taira Ishigaki1, Ichiro Nakagawa2
1Department of Mechanical Engineering, Tokai University, Japan, 2Department of Aeronautics and Engineering, Tokai University
2017-o-5-22 ( 10:20 – 10:40 )
Experimental investigation of fuel regression rate in low melting temperature thermoplastic fuels hybrid rocket using the altering intensity swirling oxidizer flow
Yo Kawabata1, Ayana Banno1, Kohei Ozawa2, Yutaka Wada1, Toru Shimada2, Nobuji Kato3, Keiichi Hori2, Ryo Nagase1
1Chiba Institute of Technology, Japan, 2Institute of Space and Astronautical Science / Japan Aerospace Exploration Agency, 3Katazen corporation
Technical Session Oral
[a-1] Liquid Propellant 1

Session Date June 7 (Wed) 11:00 – 12:00
Room Meeting Room 6
Chairpersons
2017-a-01 ( 11:00 – 11:20 )
Recent Research Activity on Rocket Engines in JAXA
Takeo Tomita, Masaharu Uchiumi, Satoshi Takada, Sadatake Tomioka, Koichi Okita
Research and Development Directorate, Japan Aerospace Exploration Agency, Japan
2017-a-03 ( 11:20 – 11:40 )
Research and Development Result of Cryogenic Propellant Valve for Small Thrust LOX/methane Rocket Engine
Hiroya Asakawa1, Hiroyuki Sakaguchi1, Hatsuo Mori1, Toshiki Kato2, Hideaki Nanri2, Toshiki Morito2, Ideo Masuda2
1Space Development Department, IHI Corporation, Japan, 2Research and Development Directorate, Japan Aerospace Exploration Agency
2017-a-04 ( 11:40 – 12:00 )
Experiment Result of Turbopump for Small Thrust LOX/methane Rocket Engine
Taiichi Motomura1, Hroyuki Sakaguchi1, Tooru Tsukano1, Toshiki Kato2, Hdeaki Nanri2, Toshiki Morito2, Ideo Masuda2
1Space Development Department, IHI Corporation, Japan, 2JAXA
[a-2] Liquid Propellant 2

Session Date June 7 (Wed) 16:00 – 17:00
Room Meeting Room 6
Chairpersons
2017-a-05 ( 16:00 – 16:20 )
Combustion chamber of BOREAS Demonstrator Design to tests
vincent leudiere1, julien herpe1, marie theron1, ariane deneuve2, louise lesaunier2, erwan humber2
1Launcher Directorate Department of Futur Innovation Launchers, CNES, France, 2Airbus Safran Launchers
2017-a-06 ( 16:20 – 16:40 )
Uncertainty Analysis as Applicable to a Miniature Cryogenic Test Stand for Rocket Research
Brunno B. Vasques, Qiaoqiao Xu Lu, Oskar J. Haidn
Institute of Space Propulsion, Munich Technical University, Germany
2017-a-07 ( 16:40 – 17:00 )
Comparative Study of Ethanol and Kerosene Propellant for Gas-Generator Fed Upper Stage Application, Using EcoSimPro
Robson Henrique dos Santos Hahn, Jan Deeken, Stefan Schlechtriem
Rocket Propulsion, DLR, Germany
[a-3] Flow Dynamics

Session Date June 8 (Thu) 9:00 – 10:40
Room Meeting Room 6
Chairpersons
2017-a-10 ( 9:00 – 9:20 )
Experimental Analysis of Priming in Evacuated Spacecraft Feedlines
Cristiano Bombardieri, Tobias Traudt, Michael Oschwald
Institute of Space Propulsion, German Space Center -DLR, Germany
2017-a-11 ( 9:20 – 9:40 )
Validation of a Lattice Boltzmann Modell for transient cryogenic two phase flow
Tobias Traudt, Max Wittal
Department of rocket propulsion, DLR, Germany
2017-a-12 ( 9:40 – 10:00 )
Effect of Axial Oscillation Amplitude on Unsteady Fluid Forces Acting on an Open Impeller
Naohito Suwa1, Toshiya Kimura1, Satoshi Kawasaki1, Kosei Goto2, Masaharu Uchiumi1
1Research and Development Directorate, Japan Aerospace Exploration Agency, Japan, 2East Japan Star Works co.,ltd
2017-a-13 ( 10:00 – 10:20 )
Study of Temperature Drift on a Capacitance Void Fraction Sensor for Cryogenic Two-Phase Flow
Shohei Tane1, Yuki Sakamoto1, Kota Uragaki1, Kazuma Minote1, Yo Nakajima1, Atsuhiro Furuichi1, Tetsuya Sato1, Hiroaki Kobayashi2
1Department of Applied Mechanics, Waseda University, Japan, 2JAXA
2017-a-14 ( 10:20 – 10:40 )
Equivalent Tubular Regression Rate in Hybrid Rockets with Complex Grain Geometries
Landon Thomas Kamps
Department of Mechanical and Space Engineering, Hokkaido University, Japan
[a-4] Combustion Instability

Session Date June 8 (Thu) 11:00 – 12:40
Room Meeting Room 6
Chairpersons
2017-a-15 ( 11:00 – 11:20 )
Interpretation of the response of cryogenic rocket flames to forced acoustics using large eddy simulation
Justin Steven Hardi1, Scott Kenneth Beinke1, Youhi Morii2, Taro Shimizu2, Hideto Kawashima3, Michael Oschwald1
1Rocket Propulsion Department, Institute of Space Propulsion, German Aerospace Center, Germany, 2JAXA’s Engineering Digital Innovation Center, Japan Aerospace Exploration Agency, 3Space Technology Directorate I, Japan Aerospace Exploration Agency
2017-a-16 ( 11:20 – 11:40 )
Dynamic Characteristics of Gas-Gas Coaxial Swirl-Jet Injector with Acoustic Excitation
Jinhyun Bae, Youngbin Yoon
Department of mechanical and aerospace engineering, Seould National University, Korea
2017-a-17 ( 11:40 – 12:00 )
Combustion Oscillation Behaviors of a Pintle Injector for an Ethanol/LOX Rocket Engine Combustor
Kazuki Sakaki1, Tomokazu Funahashi1, Shinji Nakaya1, Mitsuhiro Tsue1, Ryuichiro Kanai2, Kyohei Suzuki2, Takahiro Inagawa2, Tetsuo Hiraiwa3
1Department of Aeronautics and Astronautics, University of Tokyo, Japan, 2Interstellar Technologies Inc., 3Japan Aerospace Exploration Agency
2017-a-18 ( 12:00 – 12:20 )
Flame Visualization within a Rocket Combustion Chamber without Film Cooling
Shougo OZAKI1, Youhei KINO2, Yoshio NUNOME1, Sadatake TOMIOKA1, Takeo TOMITA1
1Japan Aerospace Exploration Agency, Japan, 2Department of Aerospace Engineering, Tohoku University
2017-a-19 ( 12:20 – 12:40 )
Reduced Dimension Analysis on Combustion Oscillation in a Model Rocket Combustor using a Deep Neural Network
Mitsuaki Tanabe
Aerospace Engineering, College of Science and Technology, Nihon University, Japan
[a-5] Air-breathing Engine

Session Date June 8 (Thu) 14:00 – 15:40
Room Meeting Room 6
Chairpersons
2017-a-20 ( 14:00 – 14:20 )
Fluid Film Damper Improvement for Reducing Vibration in Air-breathing Engine Testing
Tsung-Han Lin1, Yu-Hung Liou1, Ming-Chung Lo2
1National Chung-Shan Institute of Science and Technology, Taiwan, 2National Defense University
2017-a-21 ( 14:20 – 14:40 )
Research on Fuel Mixing in the Non-combustion Situation which Simulated in the Dual-Mode Combustor
Takuya Arakawa1, Sadatake Tomioka2
1Department of Aerospace Engineering, University of Tohoku, Japan, 2Japan Aerospace Exploration Agency,Kakuda Space Center
2017-a-22 ( 14:40 – 15:00 )
On Rocket-Airbreather Combination of Propulsion System for a TSTO Launch Vehicle
Sadatake Tomioka1, Tatsushi Isono2, Kan Kobayashi1, Masatoshi Kodera1, Kouichiro Tani1
1Research and Development Division, Japan Aerospace Exploration Agency, Japan, 2Department of Aerospace Engineering, Tohoku University
2017-a-23 ( 15:00 – 15:20 )
Breakdown of Counter-Rotating Supersonic Streamwise Vortices Generated by Swept Ramp Injector
Takakage Arai, Shingo Shichiri, Yamato Tsukazaki, Kazuma Hashimoto, Shoji Sakaue
Department of Aerospace Engineering, Osaka Prefecture University, Japan
2017-a-24 ( 15:20 – 15:40 )
Experimental Study of Ramjet Engine for High-Mach Integrated Control Experiment (HIMICO)
Akira Sato1, Sho Wakabayashi1, Yo Iwasaki1, Hidekazu Yoshida1, Tetsuya Sato1, Hideyuki Taguchi2, Takayuki Kojima2, Yuto Masuda3, Mitsuhiro Tsue3, Shinji Nakaya3
1Department of Applied Mechanics, Waseda University, Japan, 2JAXA, 3The University of Tokyo
[a-6] Solid Propellant

Session Date June 8 (Thu) 16:00 – 17:40
Room Meeting Room 6
Chairpersons
2017-a-25 ( 16:00 – 16:20 )
High Density Composite Propellants for the upper stage rocket motor
Kotaro Matsumoto1, Akihiro Iwasaki2, Hiroto Habu1
1Japan Aerospace Exploration Agency, Japan, 2SOKENDAI (The Graduate University for Advanced Studies)
2017-a-26 ( 16:20 – 16:40 )
Continuous Kneading of AP Composite Propellant Slurry by an Peristaltic Artificial Muscle Mixer
Akihiro Iwasaki1, Shun Yoshihama2, Kyota Ashigaki3, Kotaro Matsumoto4, Yasuyuki Yamada3, Kengo Tagami5, Taro Nakamura3, Hiroto Habu4
1School of Physical Sceiences, The Graduate University for Advanced Studies, Japan, 2Graduate School of Science and Engineering, Chuo University, 3Faculty of Science and Engineering, Chuo University, 4Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 5Progress Technologies
2017-a-27 ( 16:40 – 17:00 )
Study of an Automatic Material Input Method for the Continuous Production of Solid Propellant by a Peristaltic Mixer
Kyota Ashigaki1, Shun Yoshihama2, Akihiro Iwasaki3, Kengo Tagami4, Yasuyuki Yamada1, Hiroto Habu5, Taro Nakamura1
1Faculty of Science and Engineering, Chuo University, Japan, 2Graduate School of Science and Engineering, Chuo University, 3The Graduate University for Advanced Studies, 4PROGRESS TECHNOLOGIES Inc, 5Japan Aerospace eXploration Agency
2017-a-28 ( 17:00 – 17:20 )
Active Interruption of Motor Combustion for Ammonium-Perchlorate Composite Propellant
Yosuke Meichin, Masafumi Tanaka
Graduate School of Science and Engineering, National Defense Academy, Japan
2017-a-29 ( 17:20 – 17:40 )
Analyzing dispersion of particles and voids in AP/HTPB composite propellants by X-ray CT
Naomasa Hosomi1, Kana Otakae1, Natsuyo Uegaki2, Akihiro Iwasaki3, Kotaro Matsumoto4, Hirofumi Yamamoto5, Masaki Yamagata5, Hiroto Habu4, Soichiro Yamaguchi2
1Graduate School of Science and Engineering, Kansai University, Japan, 2Faculty of Engineering Science, Kansai University, 3School of Physical Sciences, The Graduate University for Advanced Studies, 4Division for Space Flight Systems, Institute of Space and Astronautical Science, 5Faculty of Chemistry, Materials and Bioengineering, Kansai University
[a-7] ADN

Session Date June 9 (Fri) 9:00 – 10:40
Room Meeting Room 6
Chairpersons
2017-a-30 ( 9:00 – 9:20 )
The Experimental Investigations and Validations of an ADN-based Liquid Thruster Family
Zhaopu Yao, Wei Zhang, Meng Wang, Jun Chen, Yan Shen
Beijing Institute of Control Engineering, China
2017-a-31 ( 9:20 – 9:40 )
Preparation and thermal decomposition behaviour of high energetic ionic liquids based on ammonium dinitramide and amine nitrates
Hiroki Matsunaga1, Katsumi Katoh1, Hiroto Habu2, Masaru Noda1, Atsumi Miyake3
1Department of Chemical Engineering, Fukuoka University, Japan, 2Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 3Institute of Advanced Sciences, Yokohama National University
2017-a-32 ( 9:40 – 10:00 )
Thermal properties of ADN based ionic liquid gel propellants
KENTO SHIOTA1, Yu-ichiro Izato2, Hiroki Matsunaga3, Hiroto Habu4, Atsumi Miyake5
1Graduate School of Environment and Information Sciences , Yokohama National University and Japan Society for the Promotion of Science, Japan, 2Graduate School of Environment and Information Sciences , Yokohama National University, 3Department of Chemical Engineering, Fukuoka University, 4Division for Space Flight Systems, Institute of Space and Astronautical Science , 5Institute of Advanced Sciences, Yokohama National University
2017-a-33 ( 10:00 – 10:20 )
Laser ignition and thermal property of ammonium dinitramide based energetic ionic liquid propellants by including chemical dyes
Mamoru Hayata
Graduated school of environment and information sciences, Yokohama National University, Japan
2017-a-34 ( 10:20 – 10:40 )
Investigation for Ignition of ADN-based Ionic Liquid with Visible Pulse Laser
Noboru Itouyama1, Hiroto Habu2
1Department of Chemical System Engineering, The University of Tokyo, Japan, 2Japan Aerospace eXploration Agency, JAXA
[a-8] Low Toxicity

Session Date June 9 (Fri) 11:00 – 12:40
Room Meeting Room 6
Chairpersons
2017-a-35 ( 11:00 – 11:20 )
Investigation into Prototype of a Hydroxyalmmonium Nitrate (HAN)-based Micropropulsion System
jitkai Chin 1, Wai Siong Chai 1, Kean How Cheah2, Kai Seng Koh 3
1deppartment of Chemical and environmental engineering , University of nottingham malaysia campus, Malaysia, 2Taylors University, 3heriot-watt university Malaysia
2017-a-36 ( 11:20 – 11:40 )
A kinetic model for combustion of Hydroxylammonium nitrate (HAN)-based propellants
Yu-ichiro Izato1, Mitsuo Koshi1, Atsumi Miyake2
1Graduate school of environmental and information sciences, Yokohama National University, Japan, 2Institute of advanced sciences, Yokohama National University
2017-a-37 ( 11:40 – 12:00 )
Influence of injector for performance of N2O/DME bipropellant thruster
Takamasa Asakura1, Shouta Hayasi1, Yano Yasuyuki2, Akira Kakami1
1Department of Mechanical Design Systems Engineering, University of Miyazaki, Japan, 2Technical Center, University of Miyazaki
2017-a-38 ( 12:00 – 12:20 )
Performance Characteristics of Low-Power DC Arcjet Thrusters with Low-Toxicity Propellants
Takefumi Mimura1, Yuki Fukutome1, Suguru Shiraki1, Katsuya Shimogaito1, Kazuyoshi Okuda1, Hirokazu Tahara1, Kyoko Takada1, Ai Momozawa2, Yuichiro Nogawa3, Daisuke Nakata4
1Department of Mechanical Engineering, Osaka Institute of Technology, Japan, 2Tokyo City University, 3Splije, 4Muroran Institute of Technology
2017-a-39 ( 12:20 – 12:40 )
Evaluation of laser ignition for HAN-based monopropellant of RCS thruster
Masaya Furusawa
Department of mechanical engineering, Nagaoka University of Technology, Japan
[a-9] Space Plane, Hybrid Propellant, Detonation Engine

Session Date June 9 (Fri) 14:00 – 15:40
Room Meeting Room 6
Chairpersons
2017-a-40 ( 14:00 – 14:20 )
Preliminary Numerical Simulation of Flow around Spaceplane for Airframe Engine Integration
Susumu Hasegawa1, Takeshi Kanda2
1Research Unit IV, JAXA, Japan, 2Chubu University
2017-a-41 ( 14:20 – 14:40 )
Coupled Aerodynamic Characteristics of Airframe and Engine of Space Plane
Kanenori Kato1, Kohichi Takasaki1, Kouichiro Tani1, Susumu Hasegawa1, Kazuhide Mizobata2, Takeshi Kanda3
1Japan Aerospace Exploration Agency, Japan, 2Muroran Institute of Technology, 3Chubu University
2017-a-42 ( 14:40 – 15:00 )
An Experimental Study on Stability of Rotating Detonation Waves
Daisuke Ikema, Atsushi Yokota, Wataru Kurata, Kazuhiro Ishii
Department of Mechanical Engineering, Yokohama National University, Japan
2017-a-43 ( 15:00 – 15:20 )
Effect of carbon black diameter on performance for a throttleable solid propellant microthruster using laser heating
Daichi Haraguchi1, Shota Isakari2, Yasuyuki Yano3, Akira Kakami1
1Department of Mechanical Design Systems Engineering, University of Miyazaki, Japan, 2Department of Mechanical Systems Engineering, University of Miyazaki, 3Technical Center, University of Miyazaki
2017-a-44 ( 15:20 – 15:40 )
Design and performance of 0.4 N class hybrid microthruster using powder fuel
Takuya Watanabe1, Yoshikazu Iwao2, Yasuyuki Yano3, Akira Kakami1
1Department of Mechanical Design Systems Engineering, University of Miyazaki, Japan, 2Department of Mechanical Systems Engineering, University of Miyazaki, 3Technical Center, University of Miyazaki
[b-1] EP Activities & Missions

Session Date June 6 (Tue) 14:00 – 15:20
Room Pearl Room B
Chairpersons
2017-b-01 ( 14:00 – 14:20 )
Current Electric Propulsion Research and Development Activities at IRS
Georg Herdrich, Tilman Binder, Adam Boxberger, Ashley Chadwick, Yung-An Chan, Michael Dropmann, Manfred Ehresmann, Roland Gabrielli, Nicholas Harmansa, Quang-Hoa Le, Christoph Montag, Francesco Romano, Stefanos Fasoulas
Institute of Space Systems (IRS), University of Stuttgart, Germany
2017-b-02 ( 14:20 – 14:40 )
Field Emission Cathodes for an Electrodynamic Tether Experiment on the H-II Transfer Vehicle
Yasushi Ohkawa, Teppei Okumura, Yuuta Horikawa, Yoshiyuki Miura, Satomi Kawamoto, Koichi Inoue
Research and Development Directorate, JAXA, Japan
2017-b-03 ( 14:40 – 15:00 )
Research and Development of High Power and High Specific-Impulse Hall Thrusters for In-Space Propulsion
Kyohei Fujiwara1, Tensei Kawakami1, Yuya Takahata1, Tetsuo Kakuma1, Yusuke Furukubo1, Mitsuyoshi Kobayashi1, Hirokazu Tahara1, Kyoko Takada1, Tomoyuki Ikeda2
1Department of Mechanical Engineering, Osaka Institute of Technology, Japan, 2Tokai University
2017-b-04 ( 15:00 – 15:20 )
Development of Coaxial Pulsed Plasma Thruster systems for Powered Flight onboard the Osaka Institute of Technology 2nd PROITERES Nano-Satellite
Kosuke Enomoto1, Ryota Fujita1, Koki Ryuho1, Kohei Ono1, Naoki Morikawa1, Hirokazu Tahara1, Kyoko Takada1, Takashi Wakizono2
1Department of Mechanical Engineering, Osaka Institute of Technology, Japan, 2High Serve Inc.
[b-2] Cathode

Session Date June 6 (Tue) 16:00 – 17:40
Room Pearl Room B
Chairpersons
2017-b-05 ( 16:00 – 16:20 )
A New External Loop for Cathode Independent Life Test to Simulate effect of Discharge Current Oscillation between Cathode and Thruster
Liqiu Wei, Wenbo Li, Yongjie Ding, Daren Yu
Institute for Advanced Power, Harbin Institute of Technology, China
2017-b-06 ( 16:20 – 16:40 )
Numerical Simulation of High Current Hollow Cathode
Kohei Kojima1, Shigeru Yokota2, Akira Osada3, Junko Yamasaki3, Moyuru Yonaha3, Tatsuya Kimura4, Yoshihiro Kawamata5, Masaaki Yasui6
1Space Vehicle & Engine Testing Section,Space Vehicle & Equipment Engineering Department, Mitsubishi Heavy Industries, Ltd, Japan, 2Division of Engineering Mechanics and Energy, University of Tsukuba, 3Department of Engineering Mechanics and Energy, University of Tsukuba, 4Propulsion & Mechanical Systems Design Section, Space Systems Engineering Department, Mitsubishi Heavy Industries, Ltd, 5Satellite Propulsion Equipment Design Section,Space Vehicle & Equipment Engineering Department, Mitsubishi Heavy Industries, Ltd, 6Space Vehicle & Equipment Engineering Department, Mitsubishi Heavy Industries, Ltd
2017-b-07 ( 16:40 – 17:00 )
Plasma Diagnosis by Langmuir Probing on High Current Hollow Cathode
Kohei Kojima1, Shigeru Yokota2, Junko Yamasaki3, Moyuru Yonaha3, Tatsuya Kimura4, Yoshihiro Kawamata5, Masaaki Yasui6
1Space Vehicle & Engine Testing Section,Space Vehicle & Equipment Engineering Department, Mitsubishi Heavy Industries, Ltd, Japan, 2Division of Engineering Mechanics and Energy, University of Tsukuba, 3Department of Engineering Mechanics and Energy, University of Tsukuba, 4Propulsion & Mechanical Systems Design Section, Space Systems Engineering Department, Mitsubishi Heavy Industries, Ltd, 5Satellite Propulsion Equipment Design Section,Space Vehicle & Equipment Engineering Department, Mitsubishi Heavy Industries, Ltd, 6Space Vehicle & Equipment Engineering Department, Mitsubishi Heavy Industries, Ltd
2017-b-08 ( 17:00 – 17:20 )
Hybrid-PIC Simulation on Thermal Characteristics of Hollow Cathode
Kenichi Kubota1, Yuya Oshio2, Hiroki Watanabe3, Shinatora Cho1, Yasushi Ohkawa4, Ikkoh Funaki5
1Aeronautical Technology Directorate, Japan Aerospace Exploration Agency, Japan, 2Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology, 3Faculty of System Design, Tokyo Metropolitan University, 4Research and Development Directorate, Japan Aerospace Exploration Agency, 5Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
2017-b-09 ( 17:20 – 17:40 )
Experimental Investigation of LaB6 Hollow Cathode with Radiative Heater
Yuya Oshio1, Kenichi Kubota2, Hiroki Watanabe3, Shinatora Cho2, Yasushi Ohkawa2, Ikkoh Funaki2
1Tokyo University of Agriculture and Technology, Japan, 2JAXA, 3Tokyo Metropolitan University
[b-3] Hall Thruster 1

Session Date June 7 (Wed) 9:00 – 10:20
Room Pearl Room B
Chairpersons
2017-b-10 ( 9:00 – 9:20 )
Experimental study on low-frequency oscillation of the plume divergence angle of hall thrusters
Liqiu Wei, Yongjie Ding, Wenbo Li, Xinyong Yang, Daren Yu
Institute for Advanced Power, Harbin Institute of Technology, China
2017-b-11 ( 9:20 – 9:40 )
Study on Suppression Method and Reliability of Pulse Current of Hall Thruster Ignition Process
Liqiu Wei, Wenbo Li, Daren Yu
Institute for Advanced Power, Harbin Institute of Technology, China
2017-b-12 ( 9:40 – 10:00 )
Performance Improvement of a 2 kW-Class Magnetically Shielded Anode-Layer Thruster
Yushi Hamada1, Rei Kawashima2, Kimiya Komurasaki2, Hiroyuki Koizumi1
1Department of Advanced Energy, The University of Tokyo , Japan, 2Department of Aeronautics and Astronautics, The University of Tokyo
2017-b-13 ( 10:00 – 10:20 )
Operating Characteristics of Anode-layer-type Hall Thruster Using Alternative Propellant
Junko Yamasaki, Shigeru Yokota, Kohei Shimamura
Department of Engineering, University of Tsukuba, Japan
[b-4] Hall Thruster 2

Session Date June 7 (Wed) 11:00 – 12:40
Room Pearl Room B
Chairpersons
2017-b-14 ( 11:00 – 11:20 )
Effect of an Indent Channel on the Discharge Characteristics of a No-Wall-Loss Hall Thruster
Liqiu Wei, Yongjie Ding, Wuji Peng, Hezhi Sun, Yu Xu, Ming Zeng, Fufeng Wang, Daren Yu
Institute for Advanced Power, Harbin Institute of Technology, China
2017-b-15 ( 11:20 – 11:40 )
Effects of the Magnetic Field Gradient on the Wall Power Deposition of Hall Thrusters
Liqiu Wei, Yongjie Ding, Peng Li, Xu Zhang, Hezhi Sun, Wuji Peng, Daren Yu
Institute for Advanced Power, Harbin Institute of Technology, China
2017-b-16 ( 11:40 – 12:00 )
Magnetic-field-tailored Hall Thruster with High Propellant Efficiency
Holak Kim1, Seunghun Lee2, Keuntae Doh1, Youbong Lim1, Wonho Choe1
1Korea Advanced Institute of Science and Technology (KAIST), Korea, 2Korea Institute of Science and Technology (KIMS)
2017-b-17 ( 12:00 – 12:20 )
A Horizontal pendulum-type Thrust Stand for evaluating higher frequency variation by applying acceleration measurement to null-balance method
Yusuke Yamauchi1, Yasuyuki Yano2, Akira Kakami1
1Department of Mechanical Design Systems Engineering, University of Miyazaki, Japan, 2Technical Center, University of Miyazaki
2017-b-18 ( 12:20 – 12:40 )
Propellant Flow Analysis within Electric Propulsion Test Facility
Yoshinori Nakayama
Department of Aerospace Engineering, National Defense Academy, Japan
[b-5] Ion Thruster

Session Date June 7 (Wed) 16:00 – 17:20
Room Pearl Room B
Chairpersons
2017-b-19 ( 16:00 – 16:20 )
Experiment and analysis on the neutralization of the electron cyclotron resonance ion thruster
Juan Yang, Yizhou Jin, Yizhi Huang, Haibo Meng, Wenbin Huang
College of Astronautics, Northwestern Polytechnical University, China
2017-b-20 ( 16:20 – 16:40 )
Transient Behaviour of Ion Extraction and Acceleration of Variable Thrust Ion Thruster
Masakatsu Nakano1, Naoji Yamamoto2, Yasushi Ohkawa3, Ikkoh Funaki3
1Tokyo Metropolitan College of Industrial Technology, Japan, 2Kyushu University, 3JAXA
2017-b-21 ( 16:40 – 17:00 )
Development of Thrust Variable System by Controlling Duty Ratio of Ion Beam Extraction in Ion Thrusters
Ippei Takesue1, Kensuke Iijima1, Yutaro Kawahara1, Koichi Ushio1, Taichi Morita1, Naoji Ymamoto1, Masakatsu Nakano2, Yasushi Ohkawa3, Ikkoh Funaki3
1Department of Advanced Energy Engineering Science, Kyushu University, Japan, 2Tokyo Metropolitan College of Industrial Technology, Tokyo Metropolitan University, 3Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
2017-b-23 ( 17:00 – 17:20 )
Numerical Analysis of a Miniature Microwave Discharge Ion Thruster Using Water as Propellant
Kengo Nakamura
Mechanical Engineering and Materials Science, Yokohama National, Japan
[b-6] MPD Thruster

Session Date June 8 (Thu) 9:00 – 10:20
Room Pearl Room B
Chairpersons
2017-b-24 ( 9:00 – 9:20 )
Performance of 100 kW Steady State Applied-Field MPD Thruster
Adam Boxberger, Roland Antonius Gabrielli, Georg Herdrich
Space Transportation Technologies, University of Stuttgart, Institute for Space Systems, Germany
2017-b-25 ( 9:20 – 9:40 )
Performance Characteristics of High-Power Steady-State MPD Thrusters with Cusp Field Using Permanent Magnets for Manned Mars Exploration
Syota Saito, Kengo Chino, Yoshikazu Sugiyama, Hirokazu Tahara, Kyoko Takada
Department of Mechanical Engineering, Osaka Institute of Technology, Japan
2017-b-26 ( 9:40 – 10:00 )
The Effect of Anode Configuration on Hydrogen MPD Thruster Performance: A Numerical Study
Shitan Tauchi
Department of Space and Astronautical Science, SOKENDAI (The Graduate University for Advanced Studies), Japan
2017-b-27 ( 10:00 – 10:20 )
Operation Characteristic of Applied-Field Magnetoplasmadynamics Thruster Using Hollow Cathode
Hayato Kasuga
Department of Aerospace Engineering, University of Nagoya, Japan
[b-7] Simulation & Modeling

Session Date June 8 (Thu) 11:00 – 12:20
Room Pearl Room B
Chairpersons
2017-b-28 ( 11:00 – 11:20 )
Numerical Simulation of Helicon Plasma Thruster Discharge by Fluid Model
Guangqing XIA, Qiuyun WU
School of Aeronautics and Astronautics, Dalian University of Technology, China
2017-b-29 ( 11:20 – 11:40 )
Numerical Modelling of a Reed Valve System for the Estimation of Air Refreshing Performance in a Pulse Detonation Beamed Microwave Rocket
Florian Nguyen1, Alseny Diallo2, Yuki Harada1, Keita Nishii1, Kimiya Komurasaki1, Hiroyuki Koizumi1
1Department of Aeronautics and Astronautics, University of Tokyo, Japan, 2ESI Group, Japan
2017-b-30 ( 11:40 – 12:00 )
Numerical simulation of laser-ablation plasma in a Magnetic Thrust Chamber for demonstration of a Laser Fusion Rocket
Tomihiko Kojima1, Masafumi Edamoto1, Naoya Saito1, Satoshi Miura1, Yutaro Itadani1, Taichi Morita1, Naoji Yamamoto1, Hideki Nakashima1, Hideo Nagatomo2, Shinsuke Fujioka2, Akifumi Yogo2, Hiroaki Nishimura2, Atsushi Sunahara3, Yoshitaka Mori4, Tomoyuki Johzaki5
1Department of Advanced Energy Engineering Science, Kyushu University, Japan , Japan, 2Institute of Laser Engineering, Osaka University, Japan, 3Institute of Laser Technology, Japan, 4The Graduate School for the Creation of New Photonics Industries, Japan, 5Faculty of Engineering, Hiroshima University, Japan
2017-b-31 ( 12:00 – 12:20 )
A 1-D Numerical Analysis of a Laser Supported Detonation with Multiple Thermal Non-equilibrium and Precursor Radiation Heating
Hiroshi Katsurayama, Kenta Mishima, Yasuo Katoh
Graduate School of Sciences and Technology for Innovation, Yamaguchi University, Japan
[b-8] Advanced Thruster 1

Session Date June 8 (Thu) 14:00 – 15:40
Room Pearl Room B
Chairpersons
2017-b-32 ( 14:00 – 14:20 )
Further Investigations; Multi-Objective Design Optimisation of a Small Scale HEMP-T
Angus Muffatti, Hideaki Ogawa
RMIT, Australia
2017-b-33 ( 14:20 – 14:40 )
Experimental Study for Effects of Plasma Density on the Performance in an Electrodeless Inductive Plasma Accelerator
Kazuya Yaginuma1, Shintarou Komatsu1, Hiroyasu Kurashige2, Hiroyuki Koizumi1, Kimiya Komurasaki1
1Department of Aeronautics and Astronautics, The University of Tokyo, Japan, 2Graduate School of Frontier Sciences, The University of Tokyo
2017-b-34 ( 14:40 – 15:00 )
Effect of improvement in neutral depletion on propulsion performance in electrodeless thruster
Kazuki Takase1, Kazunori Takahashi2, Yoshinori Takao3
1Department of Systems Integration, Yokohama National University, Japan, 2Department of Electrical Engineering, Tohoku University, 3Faculty of Engineering, Division of Systems Research, Yokohama National University
2017-b-35 ( 15:00 – 15:20 )
Study of electric propulsion using sheet plasma in TPD-Sheet IV
Miku Nishimura1, Toshikio Takimoto1, Akira Tonegawa1, Hideyuki Horisawa1, Kohnosuke Sato2, Kazutaka Kawamura1
1Department of physics, University of Tokai, Japan, 2Chubu Electric Power Co. Inc.
2017-b-36 ( 15:20 – 15:40 )
Effect of cathode electrode shape on performance of Vacuum Arc Thruster
Yayoi Murakami, Kazuhiro Toyoda, Kateryna Aheieva, Mengu Cho
Kyushu Institute of Technology, Japan
[b-9] Advanced Thruster 2

Session Date June 8 (Thu) 16:00 – 17:40
Room Pearl Room B
Chairpersons
2017-b-37 ( 16:00 – 16:20 )
New Test-Setup for IPG6-S, de Laval Nozzle design and first Tests
Francesco Romano1, Georg Herdrich1, Tony Schönherr2, Stefanos Fasoulas1
1Institute of Space Systems (IRS), University of Stuttgart, Germany, 2ESA/ESTEC, Noordwijk, The Netherlands
2017-b-38 ( 16:20 – 16:40 )
Effects of Positional Relationship between Magnetic Cusp and RF Antenna on Thrust Performance in RF Plasma Thruster
Tomohiro Shimada, Yuya Oshio, Hiroyuki Nishida
Department of engineering, University of Tokyo University of Agriculture and Technology, Japan
2017-b-39 ( 16:40 – 17:00 )
Multi-Coil Magnetic Sail Experiment in Laboratory.
Kazuma Ueno1, Yuma Ohio2, Ikkoh Funaki3, Hiroshi Yamakawa4
1School of Engineering, Chukyo University, Japan, 2Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology, 3Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 4Research Institute for Sustainable Humanosphere, Kyoto University
2017-b-40 ( 17:00 – 17:20 )
Experimental and Numerical Investigation of Thrust Generation and Vector Control with a Magnetic Thrust Chamber
Taichi Morita1, Satoshi Miura2, Masafumi Edamoto2, Hideo Nagatomo3, Atsushi Sunahara4, Tomihiko Kojima2, Naoya Saito2, Yutaro Itadani2, Yoshitaka Mori5, Tomoyuki Johzaki6, Akifumi Yogo3, Hiroaki Nishimura3, Shinsuke Fujioka3, Naoji Yamamoto1, Hideki Nakashima1
1Faculty of Engineering Sciences, Kyushu University, Japan, 2Interdisciplinary Graduate School of Engineering Sciences, Kyushu University, 3Institute of Laser Engineering, Osaka University, 4Institute for Laser Technology, 5The Graduate School for the Creation of New Photonics Industries, 6Graduate School of Engineering, Hiroshima University
2017-o-1-09 ( 17:20 – 17:40 )
Thrust measurement of a Plasma Sail with a Magnetic Nozzle injecting a thermal plasma generated by LaB6 Cathode
Yoshihiro Kajimura3, Tatsumasa Hagiwara1, Yuya Oshio2, Ikkoh Funaki3
1Department of Electrical and Computer Engineering, National Institute of Technology,Akashi College,Japan, 2Tokyo University of Agriculture and Technology, 3Japan Aerospace Exploration Agency, Japan
[b-10] Electrothermal Thruster

Session Date June 9 (Fri) 9:00 – 10:20
Room Pearl Room B
Chairpersons
2017-b-41 ( 9:00 – 9:20 )
DIRECT WATER PROPELLANT DC ARCJET THRUSTER AND BEYOND
Yuichiro Nogawa
President, CEO, Splije LLC, Japan
2017-b-42 ( 9:20 – 9:40 )
Performance Characteristics of Low-Power Water-Cooled and Anode-Radiation-Cooled DC Arcjet Thrusters Using Water and HAN Propellants
Kazuyoshi Okuda1, Yuki Fukutome1, Suguru Shiraki1, Katsuya Shimogaito1, Takefumi Mimura1, Hirokazu Tahara1, Kyoko Takada1, Ai Momozawa2, Yuichiro Nogawa3, Daisuke Nakata4
1Department of Mechanical Engineering, Osaka Institute of Technology, Japan, 2Tokyo City University, 3Splije, 4Muroran Institute of Technology
2017-b-43 ( 9:40 – 10:00 )
400-V Bus-Direct Driven High-Power Arcjet Thruster Using Dimethyl ether as Additive for Extending Lifetime
Toshihisa Kishida1, Hiroaki Murata2, Yasuyuki Yano3, Akira Kakami1
1Department of Mechanical Design Systems Engineering, University of Miyazaki, Japan, 2Department of Mechanical Systems Engineering, University of Miyazaki, 3Technical Center, University of Miyazaki
2017-b-44 ( 10:00 – 10:20 )
Development of Chemically Augmented Electrothermal Thrusters
Shoko Shibagaki1, Kai Wada1, Souto Komine2, Miya Isoda2, Mitsutoshi Tsuchiya2, Yuka Arai2, Tomoyuki Ikeda3, Hideyuki Horisawa4
1Department of Mechanical Engineering, Tokai University, Japan, 2Department of aeronautics and astronautics, Tokai University, 3Associate professor, Department of aeronautics and astronautics, Tokai University, 4Professor, Department of aeronautics and astronautics, Tokai University
[b-11] Pulsed Plasma Thruster

Session Date June 9 (Fri) 11:00 – 12:20
Room Pearl Room B
Chairpersons
2017-b-45 ( 11:00 – 11:20 )
Optimization and Experimental Analysis of the coaxial PPT PETRUS
Christoph Montag1, Georg Herdrich1, Tony Schönherr2
1University of Stuttgart, Institute of Space Systems (IRS), Germany, 2ESA, ESTEC
2017-b-46 ( 11:20 – 11:40 )
Plasma Characteristics in the Discharge Channel of an Ablative Pulsed Plasma Thruster
Lei Yang, Yuping Huang, Zaiping Zheng, Zhenxiang Xu, Liyuan Yan
Beijing Research Institute of Precise Mechatronics and Controls, China
2017-b-47 ( 11:40 – 12:00 )
Plasma Characterization of a Short-pulse Laser-assisted Pulsed Plasma Thruster
Kentaro Kato1, Haruhito Kato1, Toshiki Oi2, Hideyuki Horisawa2
1Department of mechanical engineering , Tokai University, Japan, 2Department of aerospace engineering, Tokai University
2017-b-48 ( 12:00 – 12:20 )
One-Dimensional Flowfield Calculation of Coaxial Pulsed Plasma Thrusters
Ryota Fujita1, Tobias Haase2, Keita Kanaoka1, Kohei Ono1, Naoki Morikawa1, Koki Ryuho1, Kosuke Enomoto1, Hirokazu Tahara1, Kyoko Takada1, Takashi Wakizono3
1Department of Mechanical Engineering, Osaka Institute of Technology, Japan, 2University UniBw Munchen, 3High-Serve Inc.
[b-12] Low Power Thruster 1

Session Date June 9 (Fri) 14:00 – 15:40
Room Pearl Room B
Chairpersons
2017-b-49 ( 14:00 – 14:20 )
Numerical study on the micro-cathode arc thruster
Jinyue Geng1, Zichang Xiong2, Hai-Xing Wang2
1Beijing Insititute of Control Engineering, China, 2Beijing University of Aeronautics and Astronautics
2017-b-50 ( 14:20 – 14:40 )
Effect of Anode Magnetic Shield on Performance and Life in Low Power Cylindrical Hall Thruster
Liqiu Wei, Yongjie Ding , Yu Xu, Wuji Peng
Institute for Advanced Power, Harbin Institute of Technology, China
2017-b-51 ( 14:40 – 15:00 )
10 W Level Micro Thruster with Anode Layer
Seunghun Lee1, Holak Kim2, Keuntae Doh2, Youbong Lim2, Wonho Choe2
1Plasma Processing Laboratory, Korea Institute of Materials Science, Korea, 2Dept. of Physics, Korea Advanced Institue of Science and Technology
2017-b-52 ( 15:00 – 15:20 )
Research and Development of Low-Power Cylindrical Hall Thrusters and Magnetic-Field-Expansion Cathode s for the Osaka Institute of Technology Moon-Exploration 3rd PROITERES Nano-Satellite
Tensei Kawakami1, Kyohei Fujiwara1, Mitsuyoshi Kobayashi1, Yusuke Furukubo1, Tetsuo Kakuma1, Yuya Takahata1, Hirokazu Tahara1, Kyoko Takada1, Tomoyuki Ikeda2
1Department of Mechanical Engineering, Osaka Institute of Technology, Japan, 2Tokai University
2017-b-53 ( 15:20 – 15:40 )
Characterization of a Laser-diode-coupled Fiber-tip Heat Source for Micropropulsion Applications
Kai Wada1, Shoko Shibagaki1, Souto Komine2, Miya Isoda2, Yuka Arai2, Mitsutoshi Tsuchiya2, Tomoyuki Ikeda2, Hideyuki Horisawa2
1Department of mechanical engineering, Tokai University, Japan, 2Department of aeronautics and astronautics, Tokai University
[b-13] Laser & Microwave Thruster

Session Date June 9 (Fri) 14:00 – 15:40
Room Meeting Room 5
Chairpersons
2017-b-54 ( 14:00 – 14:20 )
Effect of Bremsstrahlung emission from laser-induced plasma on the propagation of ionization wave and shock wave
Ippei Yokota1, Kohei Shimamura2, Naoto Ozaki1, Inoru Kiyono1, Kohei Matsui3, Shigeru Yokota2, Kimiya Komurasaki3
1Department of Engineering System, University of Tsukuba, Japan, 2Department of systems and information engineering, University of Tsukuba, 3Department of Aeronautics & Astronautics, University of Tokyo
2017-b-55 ( 14:20 – 14:40 )
Acceleration of Laser-Ablation Plasma by Alternating Electric Fields
Haruhito Kato, Yuki Nakamura, Kaede Yano, Hideyuki Horisawa
Tokai University, Japan
2017-b-56 ( 14:40 – 15:00 )
The effect of ambient gas species on propagation velocity of laser-induced discharge in laser propulsion
Kohei Matsui1, Toru Shimano2, Jeseph Ampadu Ofosu2, Kimiya Komurasaki1, Hiroyuki Koizumi2
1Department of Aeronautics and Astronautics, The University of Tokyo, Japan, 2Department of Advanced Energy, The University of Tokyo
2017-b-57 ( 15:00 – 15:20 )
Pulsed-laser ablation plasma diagnostics
Kaede Yano, Haruhito Kato, Yuki Nakamura, Akihiro Osamura, Ryo Edamura, Hideyuki Horisawa
Department of Aeronautics and Astronautics, Tokai University, Japan
2017-b-58 ( 15:20 – 15:40 )
Feasibility of Laser Ablation Propulsion using Magnetic Fluid as a Propellant
Takuyuki Sakai
Department of Engineering, University of Tsukuba , Japan
[b-14] Low Power Thruster 2

Session Date June 9 (Fri) 16:00 – 17:40
Room Pearl Room B
Chairpersons
2017-b-59 ( 16:00 – 16:20 )
Numerical Simulation of the Internal Plasma in a Miniature Microwave Discharge Thruster
Koichi Ushio, Tomoki Koyama, Bunsuke Ueno, Takuya Matsuo, Masashi Kusuda, Yu Okuda, Taichi Morita, Naoji Yamamoto, Hideki Nakashima
Department of Advanced Energy Engineering Science, Kyushu University, Japan
2017-b-62 ( 16:20 – 16:40 )
Numerical Investigation of Steady and Transient Ion Beam Extraction Mechanisms for Electrospray Thrusters
Kazuma Emoto
Graduate School of Engineering, Yokohama National University, Japan
2017-b-63 ( 16:40 – 17:00 )
Evaluation of Ion Beam Characteristics for Ionic Liquid Electrospray Thrusters
Naoki Inoue
Department of Mechanical Engineering and Materials Science, Yokohama National University, Japan
2017-b-60 ( 17:00 – 17:20 )
Proposal of Unified Micro-Propulsion System using Water Propellant for CubeSats
Hiroyuki Koizumi1, Yoshinori Takao2, Masakatsu Nakano3, Ryu Funase1, Yuichi Nakagawa1, Daiki Tomita1, Kimiya Komurasaki1
1The University of Tokyo, Japan, 2Yokohama National University, 3Tokyo Metropolitan College of Industrial Technology
2017-b-61 ( 17:20 – 17:40 )
Design and Test of a 100 µN-class Thrust Stand for a Miniature Ion Thruster with CubeSat
Yuichi Nakagawa
Department of Aeronautics and Astronautics, University of Tokyo, Japan
[c-1] Reentry TPS 1

Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 5
Chairpersons
2017-c-01 ( 9:00 – 9:20 )
Experimental Investigation of Material Demisability in Uncontrolled Earth Re-entries
Adam S. Pagan1, Bartomeu Massuti-Ballester1, Georg Herdrich1, James A. Merrifield2, James C. Beck3, Volker Liedtke4, Benoit Bonvoisin5
1Institute of Space Systems, University of Stuttgart, Germany, 2Fluid Gravity Engineering Ltd., 3Belstead Research Ltd., 4Aerospace and Advanced Composites GmbH, 5ESA-ESTEC
2017-c-02 ( 9:20 – 9:40 )
In-Situ Measurement of Thermal Deformation of CFRP Ablator at Arc-Heated Wind Tunnel Test Using Digital Image Correlation
Kan Sawai1, Yasuhiro Fukuda2, Jun Koyanagi2, Yuelin Zhang1, Satoru Yoneyama1, Kenichi Hirai3
1Department of Mechanical Engineering, Aoyama Gakuin University, Japan, 2Department of Materials Science and Technology, Tokyo University of Science, 3IHI AEROSPACE Co.,Ltd.
2017-c-03 ( 9:40 – 10:00 )
Delamination of CFRP Ablator under Rapid Heating
Jun Koyanagi1, Yasuhiro Fukuda1, Takuya Aoki2, Akinori Yoshimura2, Saori Nagi3, Ken-ichi Hirai3
1Department of Materials Science and Technology, Tokyo University of Science, Japan, 2Japan Aerospace Exploration Agency, 3IHI Aerospace
2017-c-04 ( 10:00 – 10:20 )
Spall fracture mechanisms and strength evaluation of CFRP against high-speed impact
Daisuke Yoshimizu
Department of Aerospace Engineering, University of Nagoya, Japan
2017-c-05 ( 10:20 – 10:40 )
Dust Erosion of the Thermal Protection System for Martian Atmospheric Entry
Takahiro Yamanaka, Jun Koyanagi
Department of Material Science and Technology, Tokyo University of science, Japan
[c-2] Reentry TPS 2

Session Date June 6 (Tue) 11:00 – 12:00
Room Meeting Room 5
Chairpersons
2017-c-06 ( 11:00 – 11:20 )
The Ablation Performance and Dynamics of the Heat Shield Material ZURAM
Adam S. Pagan1, Christian Zuber2, Bartomeu Massuti-Ballester1, Georg Herdrich1, Hermann Hald2, Stefanos Fasoulas1
1Institute of Space Systems, University of Stuttgart, Germany, 2Institute of Structures and Design, German Aerospace Centre (DLR) Stuttgart
2017-c-07 ( 11:20 – 11:40 )
Development of Mid Density Carbon Phenolic Ablators for Future Re-entry Capsules
Saori Nagi1, Kenichi Hirai1, Jun Koyanagi2, Kazuhiko Yamada3
1Technologies Development Department, IHI Aerospace Co., Ltd., Japan, 2Tokyo University of Science, 3Japan Aerospace Exploration Agency
2017-c-09 ( 11:40 – 12:00 )
Ablative Performance of High Density Carbon Phenolic after Cold Soak Exposure
Hayato Yano, Kenichi Hirai
IHI AEROSPACE Co., Ltd., Japan
[c-3] Measurement and Simulation

Session Date June 6 (Tue) 14:00 – 15:40
Room Meeting Room 5
Chairpersons
2017-c-10 ( 14:00 – 14:20 )
Strain and temperature measurement of CFRP laminate using TFBG sensor
Naoto Nakamura1, Shin-ichi TAKEDA2
1Tokyo University of Agriculture and Technology, Japan, 2JAXA
2017-c-11 ( 14:20 – 14:40 )
Evaluation of long-term thermal stabilities of polyimide resin TriA-X based composites using FBG sensors
Shin-ichi Takeda1, Yuki Kubota1, Takuya Aoki1, Yuichi Ishida1, Toshio Ogasawara2
1Aeronautical Technology Directorate, JAXA, Japan, 2Tokyo University of Agriculture and Technology
2017-c-12 ( 14:40 – 15:00 )
Effect of absorbed water on total electron emission yield
Shunsuke Inoue, Kazuhiro Toyoda
Kyushu Institute of Technology, Japan
2017-c-13 ( 15:00 – 15:20 )
Generation and evaluation of polymer monolith bicontinuous structure by self consistent field simulation
Mayuko Takahashi
Department of Mechanical Engineering, Tokyo University of Science, Japan
2017-c-14 ( 15:20 – 15:40 )
Dispersion simulation of multifunctional PANI/carbon nanomaterials
Michihiro Yamamoto1, Jun Koyanagi1, Xiuyan Cheng2, Tomohiro Yokozeki2
1Department of Materials Science and Technology, Tokyo University of Science, Japan, 2Department of Aeronautics and Astronautics, Graduate School of Engineering The University of Tokyo
[c-4] Material Characterizations

Session Date June 6 (Tue) 16:00 – 17:20
Room Meeting Room 5
Chairpersons
2017-c-15 ( 16:00 – 16:20 )
Structural study of extremely supersaturated KDP and ADP solution droplets using electrostatic levitation
Yong Chan Cho, Wonhyuk Jo, Sooheyong Lee, Geun Woo Lee
Frontier in Extreme Physics, Korea Research Institute of Standards and Science, Korea
2017-c-16 ( 16:20 – 16:40 )
Analysis of material characteristics of magnetic elastomer for fluid force control
Ryohei Aoki
University of TOYO, Japan
2017-c-17 ( 16:40 – 17:00 )
Parameter Identification of a Copper-Base Alloy Using Digital Image Correlation and Application to a Liquid Rocket Engine Combustion Chamber Wall
Ray Gordan Thiede1, Joerg Richard Riccius1, Stefanie Reese2
1Institute of Space Propulsion, Department of Rocket Propulsion, DLR, Lampoldshausen, Germany, 2Institute of Applied Mechanics, RWTH Aachen University, Aachen
2017-c-18 ( 17:00 – 17:20 )
Charging Characteristics of Spacecraft Dielectric Material at Cryogenic Temperature
Yuki Shibuya, Rikio Watanabe, Akihiro Miyasaka
The Tokyo City University, Japan
[c-5] Structure Concept, Design and Experiment

Session Date June 7 (Wed) 9:00 – 10:40
Room Meeting Room 5
Chairpersons
2017-c-19 ( 9:00 – 9:20 )
An Electromagnetically Actuated, Self-Reconfigurable Space Structure
Martin Eric William Nisser, Andreas Borggraefe, Dario Izzo
Advanced Concepts Team, European Space Agency, Netherlands
2017-c-20 ( 9:20 – 9:40 )
Weightless Condtruction of a High Tower to the Stratosphere
Ryojiro Akiba1, Ken Higuchi2, Ryuichi Mitsuhashi3, Riho Hiramoto3, Junya sasaki1
1HQ, Hokkaido Aerospace Science and Technology Incubation Center (HASTIC), Japan, 2Muroran Institute of Technoogy, 3Hokkaido University of Science
2017-c-21 ( 9:40 – 10:00 )
Concept of Large Space Structure Using Three-Dimensional Self-Deployable Truss
Daishi Kawarabayashi, Yasuyuki Miyazaki
Department of Aerospace Engineering, Nihon University, Japan
2017-c-22 ( 10:00 – 10:20 )
Preliminary study of deployable structures assembled with scissors members applied for parabolic reflectors
Kohtaroh Yamaguchi1, Rikio Watanabe1, Akihiro Miyasaka1, Ken’ichi Kawaguchi2
1Tokyo City University, Japan, 2The University of Tokyo
2017-c-23 ( 10:20 – 10:40 )
Structural Characteristics of BCON Truss
Momoko Fukunaga, Yasuyuki Miyazaki
Department of Aerospace Engineering , Nihon University, Japan
[c-6] Satellite Structures and Subsystems

Session Date June 7 (Wed) 11:00 – 12:40
Room Meeting Room 5
Chairpersons
2017-c-24 ( 11:00 – 11:20 )
Studies of on-orbit calibration of Gyro sensor in Nano-satellite “SPROUT”
Kai Yoshihara, Masahiko Yamazaki, Yasuyuki Miyazaki
Science and technology, Nihon University, Japan
2017-c-25 ( 11:20 – 11:40 )
Structure design, analysis and vibration test of Structure Thermal Model of Vietnam’s MicroDragon Satellite
Duong Cong Tran
Department of Applied Science for Integrated System Engineering, Kyushu Institute of Technology, Japan
2017-c-26 ( 11:40 – 12:00 )
Study on Competitive Structure Design of Nano Satellite
Manh Duc Nguyen
Graduate School of System Design and Management, Keio University, Japan
2017-c-27 ( 12:00 – 12:20 )
Development of CALET CALorimeter/Sensor structure
Osamu Maeda1, Takahito Amanuma1, Daisuke Nakayama1, Akira Kito1, Yukihiro Ueda2, Kazuhiro Fujimoto2, Koki Oikawa3, Tetsuya Honda3, Norio Sugi3, Shoji Torii4, Shunsuke Ozawa4, Tadahisa Tamura5, Yuki Shimizu5
1Nippi Corporation, Japan, 2IHI AeroSpace, 3JAXA, 4Waseda University, 5Kanagawa University
2017-c-28 ( 12:20 – 12:40 )
Actuator Development Projects in the Space Exploration Innovation Hub Center
Tomoaki Yano, Masatsugu Ohtsuki
Space Exploration Hub Center, JAXA, Japan
[c-7] High Precise Deployable Space Structures

Session Date June 7 (Wed) 16:00 – 17:40
Room Meeting Room 5
Chairpersons
2017-c-29 ( 16:00 – 16:20 )
An imporovement of NIPPI HIMAT
Osamu Maeda, Manato Makita, Takahiro Yumoto, Kazuhiro Abe
NIPPI Corporation, Japan
2017-c-30 ( 16:20 – 16:40 )
Induced Vibration of High-Precision Extensible Optical Bench during Extension on Orbit
Kosei Ishimura1, Manabu Ishida1, Taro Kawano1, Kenji Minesugi1, Kazuhisa Abe2, Takashi Sasaki2, Ryo Iizuka1, Nobutaka Bando1
1Japan Aerospace Exploration Agency, Japan, 2NIPPI
2017-c-31 ( 16:40 – 17:00 )
Numerical Study on Hysteresis Properties for Local Non-linearity of Extensible Truss Structures
Gaishun Iku, Atsuhiko Senba
Department of Vehicle and Mechanical Engineering, Meijo University, Japan
2017-c-32 ( 17:00 – 17:20 )
Validation of on-orbit thermal deformation and finite element model prediction in X-ray astronomical satellite HITOMI
Taro Kawano1, Kosei Ishimura1, Ryo Iizuka1, Kuniyuki Omagari2, Akira Kito3
1Japan Aerospace Exploration Agency, Japan, 2NEC Corporation, 3NIPPI Corporation
2017-c-33 ( 17:20 – 17:40 )
A Numerical Study on Shape Repeatability of Pin Jointed Beam with Frictional Contact Conditions
Takeshi AKITA1, Keisuke Nakajima2, Hiroaki Tanaka3
1Department of Innovative Mechanical and Electronic Engineering, Chiba Institute of Technology, Japan, 2Department of Mechanical Science and Engineering, Chiba Institute of Technology, 3Department of Aerospace Engineering, National Defense Academy
[c-8] High Precise Space Antenna and Subsystems

Session Date June 8 (Thu) 9:00 – 10:40
Room Meeting Room 5
Chairpersons
2017-c-34 ( 9:00 – 9:20 )
Study on Anisotropic Characteristics of a CFRP Deformable Reflector System
Hiroaki Tanaka
Department of aerospace engineering, National defense academy of japan, Japan
2017-c-35 ( 9:20 – 9:40 )
Evaluation of Thermal Characteristics of Thermal Expansion Actuator in A Vacuum
Takeshi Shimada1, Kosei Ishimura2, Hiroyuki Ogawa3, Shun Okazaki3
1Department of Aeronautics and Astronautics, School of Engineering, The University of Tokyo, Japan, 2Institute of Space and Astronautical Science/ The Japan Space Exploration Agency (JAXA), 3The Japan Space Exploration Agency (JAXA)
2017-c-36 ( 9:40 – 10:00 )
Suppression of Out-of-plane Thermal Deformation of CFRP Reflectors by Linear Actuators
Shun Tanaka, Tadashige Ikeda
Department of Aerospace Engineering, Nagoya University , Japan
2017-c-37 ( 10:00 – 10:20 )
Preliminary design study on tension truss antenna surface for shape stability
Noriyasu Yasui, Rikio Watanabe, Akihiro Miyasaka
Tokyo City University, Japan
2017-c-38 ( 10:20 – 10:40 )
Fundamental Design method of Antenna surface including compression members
Yuichirou Takano, Rikio Watanabe, Akihiro Miyasaka
Department of Mechanical Systems Engineering,Faculty of Engineering, University of Tokyo City, Japan
[c-9] Membrane Structures I

Session Date June 8 (Thu) 11:00 – 12:20
Room Meeting Room 5
Chairpersons
2017-c-40 ( 11:00 – 11:20 )
Wrinkling of a Membrane with a Curved Small Thin Film
Masanori Matsushita1, Osamu Mori2, Nobukatsu Okuizumi2, Yasutaka Satou3, Takashi Iwasa4, Saburo Matunaga5
1Department of Mechanical and Aerospace Engineering, Tokyo Institute of Technology, Japan, 2Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 3Mitsubishi Electric Corporation, 4Department of Mechanical and Aerospace Engineering, Tottori University, 5Department of Mechanical Engineering, Tokyo Institute of Technology
2017-c-41 ( 11:20 – 11:40 )
Valuation Film Shape of Multi-layer Structure with Boom
Takuma Nakamura1, Osamu Mori2, Hiraku Sakamoto3, Nobukatsu Okuizumi2
1Department of mechanical engineering, University of Aoyamagakuin, Japan, 2Japan Aerospace Exploration Agency, 3Department of Science and Engineering, Tokyo Institute of Technology
2017-c-42 ( 11:40 – 12:00 )
Data Driven Model Reduction for Spin-type Membrane Space Structure
Masahiko Yamazaki
Aerospace Engineering, Nihon University, Japan
2017-c-43 ( 12:00 – 12:20 )
Estimation Method of Missing Components for Spin Deployable Membrane Dynamics
Shoji Kawazoe
Department of Aerospace Engineering, University of Nihon, Japan
[c-10] Membrane Structures II

Session Date June 8 (Thu) 14:00 – 15:00
Room Meeting Room 5
Chairpersons
2017-c-44 ( 14:00 – 14:20 )
Effect of Creases on the Stiffness of Spinning Circular Membrane
Nobukatsu Okuizumi
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan
2017-c-46 ( 14:20 – 14:40 )
Deployment Properties of Boom-Membrane Integrated Space Structures
Hiroshi Furuya1, Hiraku Sakamoto1, Hiraku Watanabe2
1Department of Mechanical Engineering, Tokyo Institute of Technology, Japan, 2Sakase Adtech Co. Ltd.
2017-c-47 ( 14:40 – 15:00 )
Similarity Rules for Spin Deployment Membrane
Tomohiro Suzuki, Yuki Tatematsu, Yasuyuki Miyazaki, Masahiko Yamazaki
Department of aerospace engnering, Nihon university, Japan
[c-11] Vibration and Control

Session Date June 8 (Thu) 16:00 – 17:40
Room Meeting Room 5
Chairpersons
2017-c-48 ( 16:00 – 16:20 )
Non-linear System Identification of Extensible Truss Structures Using Hilbert Transform
Masashi Hayashi, Atsuhiko Senba, Toshio Matsumoto
Department of Vehicle and Mechanical Engineering, Meijo University, Japan
2017-c-49 ( 16:20 – 16:40 )
Performance Evaluation of Predictive Vibration Suppression using Piezoelectric Transducer
Kei Asahina, Masumi Ueno, Kanjuro Makihara
Department of Aerospace Engineering, Tohoku University, Japan
2017-c-50 ( 16:40 – 17:00 )
Basic Characteristics Evaluation of the Spaceborne Cooler Launch and On-orbit Vibration Isolation System using Pseudoelastic Shape Memory Alloy
Seong-Cheol Kwon, Young-Hyeon Jeon, Hyun-Ung Oh
Department of Aerospace Engineering, University of Chosun, Korea
2017-c-51 ( 17:00 – 17:20 )
Fundamental Study on Vibration Characteristics of Space Solar Power Systems
Kengo Noguchi, Rikio Watanabe, Akihiro Miyasaka
Tokyo City University , Japan
2017-c-52 ( 17:20 – 17:40 )
Numerical Analysis on Passive Shape Control for Two-dimensional Truss Structures Using Additional Masses
Takato Watanabe, Atsuhiko Senba
Department of Vehicle and Engineering, Meijo University, Japan
[c-12] Shock

Session Date June 9 (Fri) 9:00 – 10:20
Room Meeting Room 5
Chairpersons
2017-c-53 ( 9:00 – 9:20 )
A study of Reusable Landing Shock Absorber System for Exploration on Planet
Shota Iwabuchi, Kenji Minesugi
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan
2017-c-55 ( 9:20 – 9:40 )
Analytical Study of Landing Shock Absorber in the Simulated High-Speed Impact Test
Keisuke Nakamura
Department of Applied Mechanics, Waseda University, Japan
2017-c-56 ( 9:40 – 10:00 )
Shock Resistance of Piezoelectric Stack Actuators
Tadashige Ikeda1, Hiroaki Tanaka2, Hidehiro Hata3, Nozomu Kogiso4, Kosei Ishimura5, Takashi Iwasa6
1Nagoya University, Japan, 2National Defense Academy of Japan, 3Kumamoto University, 4Osaka Prefecture University, 5JAXA, 6Tottori University
2017-c-57 ( 10:00 – 10:20 )
Shock Response Spectrum Analysis of Pyroshock Experiment and Finite Element Simulation
Yu-Liang Chen1, Chin-Yu Huang2, Jiu-Zhang Lu1, Meng-Chiau Wu1, Wen-Kuan Huang1, Chia-Wei Yeh1
1Department of Power Vehicle and Systems Engineering, Chung Cheng Institute of Technology, National Defense University, Taiwan, 2School of Defense Science, Chung Cheng Institute of Technology, National Defense University
[c-13] Design and Performance of Ground Test Facilities and Tools

Session Date June 9 (Fri) 11:00 – 12:40
Room Meeting Room 5
Chairpersons
2017-c-58 ( 11:00 – 11:20 )
High-Fidelity Validation of Vision-Based Sensors for Spacecraft Navigation
Connor Robert Beierle, Joshua Anthony Sullivan, Simone D’Amico
Stanford University, Department of Aeronautics & Astronautics, Space Rendezvous Laboratory, USA
2017-c-59 ( 11:20 – 11:40 )
Surface shape measuring method for space structures based on images in ultra-violet range
Naoko Kishimoto1, Takashi Iwasa2, Ken Higuchi3
1Department of Mechanical Engineering, Setsunan University, Japan, 2Department of Mechanical Engineering, Tottori University, 3Department of Aerospace Engineering, Muroran Institute of Technology
2017-c-60 ( 11:40 – 12:00 )
Preliminary Investigations of Pneumatic Gravity Compensation System for Deployable Space Structures
Masato Taki, Rikio Watanabe, Akihiro Miyasaka
Engineering, Tokyo City University, Japan
2017-c-61 ( 12:00 – 12:20 )
Verification of the Side-wall heating to Specimen Arc-heated
Takayuki Shimoda1, Keiichi Okuyama2
1Institute of Space and Aeronautical Sience , Japan Aerospace Exoploration Agency , Japan, 2Kyushu Institute of Technology
2017-c-62 ( 12:20 – 12:40 )
Three-dimensional Surface Shape Measurement of Parabola Antenna Model with 1.5m diameter using Granting Projection Method
Kento Ota1, Taku Harada2, Takashi Iwasa1
1Department of Mechanical and Aerospace Engineering, Tottori University, Japan, Japan, 2Master of Mechanical and Aerospace Engineering Tottori University, Jaqpan
[d-1] Flight Dynamics Operations 1

Session Date June 6 (Tue) 9:00 – 10:20
Room Meeting Room 1
Chairpersons
ISTS-2017-d-001/ISSFD-2017-001 ( 9:00 – 9:20 )
Feasibility of Metop-A Mission Extension on Drifting Local Time
Pierluigi Righetti, Richard Dyer
Operations, EUMETSAT, Germany
ISTS-2017-d-002/ISSFD-2017-002 ( 9:20 – 9:40 )
Metop long term free-dynamics attitude analysis, for improved re-entry prediction
Stefano Pessina1, Pierluigi Righetti1, João Branco2, Victor Moreno Villa3, Thomas Vincent Peters3
1EUMETSAT, Germany, 2GMV, Portugal, 3GMV, Spain
ISTS-2017-d-003/ISSFD-2017-003 ( 9:40 – 10:00 )
Flight Dynamics Support to extend Instruments useful Lifetime
Antimo DAMIANO1, Pier Luigi RIGHETTI2, Ruediger LANG2, Francisco SANCHO3
1RHEA Group at EUMETSAT, Belgium, 2EUMETSAT, 3Working Group Solutions (WGS) at EUMETSAT
ISTS-2017-d-004/ISSFD-2017-004 ( 10:00 – 10:20 )
Non-Nominal Attitude Manoeuvres during Metop-A Extended Lifetime
Francisco Sancho1, Jörg Fischer2, Stefania Tarquini3
1WGS Workgroup Solutions at EUMETSAT, Germany, Germany, 2Jade Aerospace at EUMETSAT, Germany, 3EUMETSAT, Germany
[d-2] Orbit Dynamics (Martian Moon)

Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 2
Chairpersons
ISTS-2017-d-005/ISSFD-2017-005 ( 9:00 – 9:20 )
Quasi-Satellite Orbits around Deimos and Phobos motivated by the DePhine Mission Proposal
Sofya Spiridonova1, Kai Wickhusen2, Ralph Kahle1, Jürgen Oberst2
1Spaceflight Technology Department, German Space Operations Center, DLR Oberpfaffenhofen, Germany, 2Planetary Geodesy Department, Institute of Planetary Research, DLR Berlin
ISTS-2017-d-006/ISSFD-2017-006 ( 9:20 – 9:40 )
Trajectory analysis for the Phobos proximity phase of the MMX mission
Elisabet Canalias1, Laurence Lorda1, Thierry Martin1, Jean Charles Marty2, Julien Laurent-Varin2, Yuya Mimasu3
1CNES, France, 2CNES-GRGS, 3JAXA-ISAS
ISTS-2017-d-007/ISSFD-2017-007 ( 9:40 – 10:00 )
THE DYNAMICAL ENVIRONMENT FOR THE EXPLORATION OF PHOBOS
Daniel Jay Scheeres, Stefaan Van wal, Zubin Olikara
Aerospace Engineering Sciences, University of Colorado, USA
ISTS-2017-d-008/ISSFD-2017-008 ( 10:00 – 10:20 )
Orbital Operations Strategy in the Vicinity of Phobos
Hitoshi Ikeda, Shinji Mitani, Yuya Mimasu, Go Ono, Kenichiro Nigo, Yasuhiro Kawakatsu
Japan Aerospace Exploration Agency, Japan
ISTS-2017-d-009/ISSFD-2017-009 ( 10:20 – 10:40 )
Quasi-Satellite Orbits around Phobos for the Sample Return Mission
Javier Martin Avila, Simone Centuori
Flight Systems – Mission Analysis & Navigation, DEIMOS Space, Spain
[d-3] Trajectory Design & Optimization 1

Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 3
Chairpersons
ISTS-2017-d-010/ISSFD-2017-010 ( 9:00 – 9:20 )
A LINEAR ANALYSIS FOR THE FLIGHT PATH CONTROL OF THE CASSINI GRAND FINALE ORBITS
Mar Vaquero, Yungsun Hahn, Duane Roth, Mau Wong
Mission Design and Navigation, NASA Jet Propulsion Laboratory, USA
ISTS-2017-d-011/ISSFD-2017-011 ( 9:20 – 9:40 )
Uncertainty Analysis of Mars Entry Trajectories Using Stochastic Collocation
Yuechen Huang, Haiyang Li, Yazhong Luo
College of Aerospace Science and Engineering , National University of Defense Technology, China
ISTS-2017-d-012/ISSFD-2017-012 ( 9:40 – 10:00 )
Orbit Design for Martian Moons Explorer
Naoko Ogawa1, Yuichi Tsuda1, Yuto Takei1, Hiroka Inoue1, Shota Takahashi2, Yasuhiro Kawakatsu1
1Japan Aerospace Exploration Agency, Japan, 2Keio University
ISTS-2017-d-013/ISSFD-2017-013 ( 10:00 – 10:20 )
Descend isochrones in Martian atmosphere
Miljan Kolcic
Department of Astronomy, Faculty of Mathematics University of Belgrade, Serbia
ISTS-2017-d-014/ISSFD-2017-014 ( 10:20 – 10:40 )
Method of Robust Orbit Insertion and its Application to MMX Mission
Shota Takahashi
Department of Mechanical Engineering, Faculty of Science and Technology, Keio University, Japan
[d-4] Flight Dynamics Operations 2

Session Date June 6 (Tue) 11:00 – 11:40
Room Meeting Room 1
Chairpersons
ISTS-2017-d-015/ISSFD-2017-015 ( 10:20 – 10:40 )
Rosetta Navigation during the End of Mission Phase
Pablo Munoz1, Vicente Companys2, Frank Budnik2, Bernard Godard3, Dario Pellegrinetti1, Gabriele Bellei4, Rainer Bauske5, Waldemar Martens2
1Flight Dynamics, GMV at ESA/ESOC, Germany, 2Flight Dynamics, ESA/ESOC, 3Flight Dynamics, Telespazio VEGA at ESA/ESOC, 4Flight Dynamics, Deimos Space at ESA/ESOC, 5Flight Dynamics, Terma at ESA/ESOC
ISTS-2017-d-016/ISSFD-2017-016 ( 10:40 – 11:00 )
Operational experience and assessment of the implementation of the maplet technique for Rosetta’s optical navigation
Klaas Vantournhout1, Ramon Pardo de Santayana2, Francesco Castellini3, Mathias Lauer4
1CGI Deutschland Ltd. & Co. KG, Germany, 2LSE Space, 3Telespazio-VEGA Deutschland, 4European Space Operations Centre, European Space Agency ESA
[d-5] Orbit Dynamics (Small Body) 1

Session Date June 6 (Tue) 11:00 – 12:40
Room Meeting Room 2
Chairpersons
ISTS-2017-d-017/ISSFD-2017-017 ( 11:00 – 11:20 )
Assessing the Hazard Posed by Ryugu Ejecta Dynamics on Haybusa2 spacecraft
Stefania Soldini, Yuichi Tsuda
Department of Space Flight Systems, Institute of Space and Astronautical Science/JAXA, Japan
ISTS-2017-d-018/ISSFD-2017-018 ( 11:20 – 11:40 )
Investigation of 1:1 resonance in a rotating 4 th degree and order gravitational field
Jinglang Feng1, Ron Noomen2, Xiyun Hou1, Pieter N.A.M. Visser2, Jianping Yuan3, Jingshi Tang1, Lin Liu1
1School of Astronomy and Space Science, Nanjing University, China, China, 2Faculty of Aerospace Engineering, Delft University of Techonolgy, the Netherlands, 3School of Astronautics, Northwestern Polytechnic University, China
ISTS-2017-d-019/ISSFD-2017-019 ( 11:40 – 12:00 )
Orbital Stability Regions for Hypothetical Natural Satellites
Samantha M Rieger2, Daniel Scheeres1, Brent Barbee2
1Aerospace Engineering Sciences, University of Colorado Boulder, USA, 2Goddard Space Flight Center, Greenbelt, MD, USA
ISTS-2017-d-020/ISSFD-2017-020 ( 12:00 – 12:20 )
stability analysis of orbital motions around uniformly rotating irregular asteroids
Xiyun Hou1, Daniel Jay Scheeres2, Xiaosheng Xin1, Jingshi Tang1, Lin Liu1
1School of Astronomy and Space Science, Nanjing University, China, China, 2Department of Aerospace Engineering Sciences, University of Colorado Boulder, USA
ISTS-2017-d-021/ISSFD-2017-021 ( 12:20 – 12:40 )
On the Equilibrium Points of Doubly Synchronous Binary Asteroid Systems
Xiaosheng Xin1, Xiyun Hou2, Lin Liu2, Guangliang Dong1
1Beijing Institute of Tracking and Telecommunications Technology, China, 2School of Astronomy and Space Science, Nanjing University
[d-6] Trajectory Design & Optimization 2

Session Date June 6 (Tue) 11:00 – 12:20
Room Meeting Room 3
Chairpersons
ISTS-2017-d-022/ISSFD-2017-022 ( 11:00 – 11:20 )
Systematic Search for Moon-to-Moon Transfers for the Design of Solar-Perturbed Multiple Lunar Flybys
Kenta Oshima1, Yasuhiro Kawakatsu2, Tomohiro Yanao1
1Waseda University, Japan, 2JAXA
ISTS-2017-d-023/ISSFD-2017-023 ( 11:20 – 11:40 )
Design of High-Energy Escape Trajectories with Lunar Gravity Assist
Lorenzo Casalino
Department of Mechanical and Aerospace Engineering, Politecnico di Torino, Italy
ISTS-2017-d-024/ISSFD-2017-024 ( 11:40 – 12:00 )
Matching of Patched-Hyperbolas for Lunar Gravity-Assist Trajectory Design
Yuki Kayama1, Chit Hong Yam2, Kenta Oshima3, Shuntaro Suda4, Yasuhiro Kawakatsu2
1Department of Advanced Energy, The University of Tokyo, Japan, 2Department of Space Flight Systems, JAXA, 3Department of Applied Mechanics, Waseda University, 4Division of Mechanical and Space Engineering, Hokkaido University
ISTS-2017-d-179/ISSFD-2017-179 ( 12:00 – 12:20 )
Patented Orbits Transfers and Manoeuvres Review
Christophe R Koppel
C.E.O., KopooS Consulting Ind., France
[d-7] Flight Dynamics Operations 3

Session Date June 6 (Tue) 14:00 – 15:20
Room Meeting Room 1
Chairpersons
ISTS-2017-d-026/ISSFD-2017-026 ( 14:00 – 14:20 )
Lessons learned from initial Sentinel-3A manoeuvres operations
Daniel Aguilar Taboada, Pier Luigi Righetti, Rami Houdroge
Operations, EUMETSAT, Germany
ISTS-2017-d-027/ISSFD-2017-027 ( 14:20 – 14:40 )
Sentinel-3A Flight Dynamics LEOP operational experience
Mikel Catania1, Claudia Dietze2, Jochen Klein3
1Flight Dynamics for CGI/LSE at ESOC, Germany, Germany, 2Flight Dynamics for CS at ESOC, Germany, 3Flight Dynamics for CGI at ESOC, Germany
ISTS-2017-d-028/ISSFD-2017-028 ( 14:40 – 15:00 )
Sentinel-1A: Flight Dynamics Analysis of the August 2016 Collision Event
Petr Kuchynka1, Miguel A. Martin Serrano2, Mikel Catania3, Xavier Marc4, Dirk Kuiper5, Vitali Braun6, Holger Krag4
1GMV/ESOC, Germany, 2SCISYS/ESOC, 3LSE/ESOC, 4ESA/ESOC, 5CGI/ESOC, 6IMS/ESOC
ISTS-2017-d-029/ISSFD-2017-029 ( 15:00 – 15:20 )
Sentinel-1B Flight Dynamics operations during LEOP and acquisition of its reference orbit: achieving the Sentinel-1 constellation
Miguel Angel Martin Serrano1, Javier Sanchez2, Andre Vasconcelos1, Xavier Marc3
1ESOC Flight Dynamics, SCISYS at ESOC/ESA, Germany, 2ESOC Flight Dynamics, GMV GmbH at ESOC/ESA, 3ESOC Flight Dynamics, ESA
[d-8] Orbit Dynamics (Small Body) 2

Session Date June 6 (Tue) 14:00 – 15:40
Room Meeting Room 2
Chairpersons
ISTS-2017-d-030/ISSFD-2017-030 ( 14:00 – 14:20 )
Orbit-Attitude Coupled Dynamics of Solar Sail Spacecraft around Small Bodies
Shota Kikuchi1, Yuichi Tsuda2, Jun’ichiro Kawaguchi2
1Department of Aeronautics and Astronautics, The University of Tokyo, Japan, 2Japan Aerospace Exploration Agency (JAXA)
ISTS-2017-d-031/ISSFD-2017-031 ( 14:20 – 14:40 )
Reliability Analysis of Ballistic Landing in Binary Asteroid 65803 (1996GT) Didymos under Uncertainty and GNC Error Considerations
Onur Celik1, Ozgur Karatekin2, Birgit Ritter2, Joan Pau Sanchez3
1Space and Astronautical Sciences, The Graduate University for Advanced Studies (SOKENDAI), Japan, 2Dynamics of the Solar System, Royal Observatory of Belgium, 3Space Research Group, Centre of Autonomous and Cyber-Physical Systems, Cranfield University
ISTS-2017-d-032/ISSFD-2017-032 ( 14:40 – 15:00 )
Mascot: Analyses of the Descent and Bouncing Trajectories to Support the Landing Site Selection
Laurence Lorda1, Elisabet Canalias1, Thierry Martin1, Jens Biele2
1CNES, France, 2DLR
ISTS-2017-d-033/ISSFD-2017-033 ( 15:00 – 15:20 )
Small-Body Lander/Hopper Simulations using the GPU
Stefaan Van wal1, Robert Reid2, Daniel Scheeres1
1Department of Aerospace Engineering Sciences, University of Colorado Boulder, USA, 2Jet Propulsion Laboratory, California Institute of Technology
ISTS-2017-d-034/ISSFD-2017-034 ( 15:20 – 15:40 )
Family of Quasi-Stable Orbit around Asteroids in Strongly Perturbed Environment
Yusuke Oki1, Yuichi Tsuda2
1Department of Aeronautics and Astronautics, The university of Tokyo, Japan, 2JAXA
[d-9] Flight Dynamics Operations 4

Session Date June 6 (Tue) 16:00 – 17:40
Room Meeting Room 1
Chairpersons
ISTS-2017-d-035/ISSFD-2017-035 ( 16:00 – 16:20 )
Recent Developments and Future Directions in CCSDS Flight Dynamics Standards
David Scott Berry
Mission Design & Navigation Section, California Institute of Technology, Jet Propulsion Laboratory, USA
ISTS-2017-d-036/ISSFD-2017-036 ( 16:20 – 16:40 )
In-flight Characterisation and Calibration of Galileo FOC Reaction Control System
Riccardo Di Corato1, Pere Ramos Bosch1, Xavier Pena2
1Flight Dynamics, ESOC, Germany, 2Flight Dynamics, CNES
ISTS-2017-d-037/ISSFD-2017-037 ( 16:40 – 17:00 )
Manoeuvre Optimization in the Galileo L7 Orbit Acquisition
Andre Vasconcelos1, Pere Ramos Bosch2, Dave Hocken1, Javier Sanchez3, Gerald Ziegler1
1Scisys GmbH at ESA/ESOC, Flight Dynamics Division, Earth Observation Section, Germany, 2ESA/ESOC, Flight Dynamics Division, Earth Observation Section, 3GMV at ESA/ESOC, Flight Dynamics Division, Earth Observation Section
ISTS-2017-d-038/ISSFD-2017-038 ( 17:00 – 17:20 )
Microscope mission: on-orbit assessment of the drag-free and attitude control system
Pascal PRIEUR1, Thomas LIENART1, Manuel RODRIGUES2, Troelz DENVER3, Pierre TOUBOUL2, Gilles METRIS4
1CNES, France, 2ONERA, 3Denmark Technical University, 4Université Côte d’Azur, OCA, CNRS, IRD, Geoazur
ISTS-2017-d-039/ISSFD-2017-039 ( 17:20 – 17:40 )
A Comparison of Fuel Gauging Methods Utilising the Experience of S/C De-orbiting Operations
Lutz Massonne
ESOC Flight Dynamics, Telespazio VEGA Deutschland GmbH, Germany
[d-10] Guidance, Navigation and Control (Small Body)

Session Date June 6 (Tue) 16:00 – 17:20
Room Meeting Room 2
Chairpersons
ISTS-2017-d-041/ISSFD-2017-041 ( 16:00 – 16:20 )
Autonomous Navigation of a Formation of Spacecraft in the Proximity of a Binary Asteroid
Massimiliano L Vasile, Francesco Torre
Mechanical & Aerospace Engineering, University of Strathclyde, Department of Mechanical & Aerospace Engineering, UK
ISTS-2017-d-042/ISSFD-2017-042 ( 16:20 – 16:40 )
Improved Shape Determination for Autonomous Navigation
Benjamin Bercovici, Ann Dietrich, Jay Warren McMahon
Aerospace Engineering Sciences, University of Colorado Boulder, USA
ISTS-2017-d-043/ISSFD-2017-043 ( 16:40 – 17:00 )
The High-fidelity Asteroid Deflection Evaluation Software (HADES): Assessing the Impact of Environmental and System Uncertainties on Autonomous Proximity Operations
Massimo Vetrisano, Juan Luis Cano, Simone Centuori
Flight System – Mission Analysis & Navigation , Deimos Space SLU, Spain
ISTS-2017-d-044/ISSFD-2017-044 ( 17:20 – 17:20 )
Range Measurement based Localization between Mothership and Lander Considering Asteroid Shape Using Particle Filter
Hirokazu Ishida
Department of Aeronautics and Astronautics, The University of Tokyo, Japan
[d-11] Attitude Dynamics

Session Date June 7 (Wed) 9:00 – 10:20
Room Meeting Room 1
Chairpersons
ISTS-2017-d-046/ISSFD-2017-046 ( 9:00 – 9:20 )
Dynamical Modelling for Flat-Spin Recovery Applications
Jozef C. van der Ha, Frank L. Janssens
Consultant, Mission Design & Operations, USA
ISTS-2017-d-047/ISSFD-2017-047 ( 9:20 – 9:40 )
Utilisation of the Dzhanibekov’s Effect for the Possible Future Space Missions
Pavel M. TRIVAILO1, Hirohisa Kojima2
1School of Engineering, RMIT University, Australia, Australia, 2Department of Aerospace Engineering, TMU University, Japan
ISTS-2017-d-048/ISSFD-2017-048 ( 9:40 – 10:00 )
Dynamics of a Space Multi-pointing Stewart System Using the New Form of Kane’s Method
Quan HU, Fei LIU, Yao ZHANG
School of Aerospace Engineering , Beijing Institute of Technology , China
ISTS-2017-d-049/ISSFD-2017-049 ( 10:00 – 10:20 )
Optimal Fault-Tolerant Configurations of Thrusters
Yasuhiro Yoshimura, Hirohisa Kojima
Aerospace Engineering, Tokyo Metropolitan University, Japan
[d-12] Guidance, Navigation and Control (Landing) 1

Session Date June 7 (Wed) 9:00 – 10:20
Room Meeting Room 2
Chairpersons
ISTS-2017-d-050/ISSFD-2017-050 ( 9:00 – 9:20 )
OMOTENASHI Trajectory Analysis and Design: Landing Phase
Javier Hernando-Ayuso1, Stefano Campagnola2, Toshinori Ikenaga2, Yusuke Ozawa1, Bruno Sarli2, Shota Takahashi3, Chit Yam2, Tomohiro Yamaguchi2
1The University of Tokyo, Japan, 2JAXA, 3Keio University
ISTS-2017-d-052/ISSFD-2017-052 ( 9:20 – 9:40 )
Flight Control of Flying Test Bed for Future Planetary Landing
Takehiro Higuchi1, Toshiki Tamura2, Seiya Ueno1, Kazuhisa Fujita3, Takashi Ozawa3, Hiroki Takayanagi3
1Faculty of Environment and Information Sciences, Yokohama National University, Japan, 2Graduate School of Environment and Information Sciences, Yokohama National University, 3Japan Aerospace Exploration Agency
ISTS-2017-d-053/ISSFD-2017-053 ( 9:40 – 10:00 )
A Study on Guidance Technique for Precise Lunar Landing
Satoshi Ueda1, Takahiro Ito1, Shin-ichiro Sakai2
1Research Unit I, Research and Development Directorate, JAXA, Japan, 2Department of Spacecraft Engineering, Institute of Space and Astronautical Science (ISAS), JAXA
ISTS-2017-d-054/ISSFD-2017-054 ( 10:00 – 10:20 )
Comparative Analysis of Adaptive and Optimal Control Laws for Manned Lunar Lander
Chengchao Bai1, Jifeng Guo 1, Linli Guo 2, Hongxing Zheng1
1School of Astronautics, Harbin Institute of Technology, China, 2China Academy of Space Technology (CAST)
[d-13] Orbit Dynamics & Control 1

Session Date June 7 (Wed) 9:00 – 10:40
Room Meeting Room 3
Chairpersons
ISTS-2017-d-055/ISSFD-2017-055 ( 9:00 – 9:20 )
Harnessing the Sun’s Gravity for LEO to GEO Transfers
Stijn De Smet1, Jeffrey S Parker2, Daniel J Scheeres1
1Colorado Center for Astrodynamics Research, University of Colorado at Boulder, USA, 2Advanced Space
ISTS-2017-d-056/ISSFD-2017-056 ( 9:20 – 9:40 )
Systematic Study of the Dynamics about and between the Libration Points of the Sun-Earth-Moon system
Bastien Le Bihan1, Josep Joaquim Masdemont2, Gerard Gomez3, Stephanie Lizy-Destrez1
1Departement Conception et Conduite des vehicules Aeronautiques et Spatiaux, ISAE/Supaero, France, 2Institut d’Estudis Espacials de Catalunya & Departament de Matematiques, Universitat Politecnica de Catalunya, 3Institut d’Estudis Espacials de Catalunya & Departament de Matematiques i Informatica, Universitat de Barcelona
ISTS-2017-d-057/ISSFD-2017-057 ( 9:40 – 10:00 )
Assessment of the Gaussian Covariance Approximation over an Earth-Asteroid Encounter Period
Daniel W. Mattern
Flight Dynamics Facility, NASA Goddard Space Flight Center, USA
ISTS-2017-d-058/ISSFD-2017-058 ( 10:00 – 10:20 )
Improved Reference Orbits for the Repeat-Ground-Track Missions EnMAP and Tandem-L
Ralph Kahle, Sofya Spiridonova, Michael Kirschner
German Space Operations Center (GSOC), German Aerospace Center (DLR), Germany
ISTS-2017-d-059/ISSFD-2017-059 ( 10:20 – 10:40 )
Nonlinear Uncertainty Propagation of Orbital Mechanics subject to Stochastic Error in Atmospheric Mass Density
Changyong HE
School of Science, Mathematical & Geospatial Sciences, RMIT University, Australia
[d-14] Attitude / Orbit Dynamics & Control

Session Date June 7 (Wed) 11:00 – 12:40
Room Meeting Room 1
Chairpersons
ISTS-2017-d-060/ISSFD-2017-060 ( 11:00 – 11:20 )
A New Algorithm to Compute the SRP Force and Torque on Generic Spacecraft
Juan Manuel Garcia
GMV GmbH, FDO division, contractor at ESA/ESOC, OPS-GFS, Germany
ISTS-2017-d-061/ISSFD-2017-061 ( 11:20 – 11:40 )
Optimal Design of Advanced Reflectivity Control Device for Solar Sails Considering Polarization Properties of Liquid Crystal
Hirokazu Ishida1, Toshihiro Chujo1, Osamu Mori2, Junichiro Kawaguchi2
1Department of Aeronautics and Astronautics, The University of Tokyo, Japan, 2Institute of Space and Astronautical Science(ISAS), JAXA
ISTS-2017-d-062/ISSFD-2017-062 ( 11:40 – 12:00 )
On-orbit Estimation of Optical Property by Precomputed Tensor Method for High-fidelity SRP Model
Satoshi Ikari1, Kakeru Tokunaga1, Takahiro Ito2, Takaya Inamori3, Ryu Funase1, Shinichi Nakasuka1
1Department of Aeronautics and Astronautics, The University of Tokyo, Japan, 2JAXA, 3Department of Micro-Nano System Engineering, Nagoya University
ISTS-2017-d-063/ISSFD-2017-063 ( 12:00 – 12:20 )
Dynamics and Control of Modular and Extended Space Structures in Cislunar Environment
Andrea Colagrossi, Michèle Lavagna
Department of Aerospace Science and Technology, Politecnico di Milano, Italy
ISTS-2017-d-064/ISSFD-2017-064 ( 12:20 – 12:40 )
Estimation of Shape and Optical Parameters of Spinning Solar Sail Equipped with Reflectivity Control Devices
Akihiro Ishikawa
Department of Aeronautics and Astronautics, University of Tokyo, Japan
[d-15] Guidance, Navigation and Control (Landing) 2

Session Date June 7 (Wed) 11:00 – 12:40
Room Meeting Room 2
Chairpersons
ISTS-2017-d-065/ISSFD-2017-065 ( 11:00 – 11:20 )
Position and Displacement Estimation Using Crater-based Line Segments for Pinpoint Lunar Landing
Kazuki Kariya1, Takayuki Ishida2, Shujiro Sawai2, Seisuke Fukuda2
1Department of Space and Astronautical Science, SOKENDAI(The Graduate University for Advanced Studies), Japan, 2JAXA
ISTS-2017-d-066/ISSFD-2017-066 ( 11:20 – 11:40 )
A Study of Terrain Feature Matching for Lunar Landing Navigation
Yasuhiro Katayama, Shigehito Shimizu, Misuzu Haruki, Shuhei Shigeto, Isao Kawano, Kazuhisa Kazuhisa
Research and Development Directorate, Japan Aerospace Exploration Agency, Japan
ISTS-2017-d-067/ISSFD-2017-067 ( 11:40 – 12:00 )
The robust spacecraft location estimation algorithm toward the misdetection crater and the undetected crater in SLIM
Haruyuki Ishii1, Akinori Murata1, Fumito Uwano1, Takato Tatsumi1, Yuta Umenai1, Kazuma Matsumoto1, Keiki Takadama1, Hiroyuki Kamata2, Takayuki Ishida3, Seisuke Fukuda4, Shujiro Sawai4, Shinichiro Sakai4
1The University of Electro-Communications, Japan, 2Meiji University, 3JAXA, 4JAXA, ISAS
ISTS-2017-d-068/ISSFD-2017-068 ( 12:00 – 12:20 )
Autonomous Navigation for Pinpoint Lunar Soft Landing
Chengchao Bai1, Jifeng Guo 1, Linli Guo 2, Hongxing Zheng1
1School of Astronautics, Harbin Institute of Technology, China, 2China Academy of Space Technology
ISTS-2017-d-069/ISSFD-2017-069 ( 12:20 – 12:40 )
Evaluation of Landing Stability of Two-step Landing Method for Small Lunar-planetary Lander
Shunpei Morikawa
Department of Engineering, Shizuoka University, Japan
[d-16] Orbit Dynamics & Control 2

Session Date June 7 (Wed) 11:00 – 12:00
Room Meeting Room 3
Chairpersons
ISTS-2017-d-071/ISSFD-2017-071 ( 11:00 – 11:20 )
Orbit Uncertainty Propagation around Non-Spherical Bodies Using the Dromo Formulation
Javier Hernando-Ayuso1, Claudio Bombardelli2
1Department of Aeronautics and Astronautics, The University of Tokyo, Japan, 2Space Dynamics Group, Technical University of Madrid
ISTS-2017-d-073/ISSFD-2017-073 ( 11:20 – 11:40 )
Moon Mission Lifetime Analysis of a 2U CubeSat Equipped with Pulsed Plasma Thrusters; The Aoba-VELOX IV Mission Case
Jose Rodrigo Cordova Alarcon1, Necmi Cihan Orger1, Sangkyun Kim1, Tran Quang Vinh2, Lim Wee Seng2, Bui Tran Duy Vu2, Mengu Cho1
1Laboratory of Spacecraft Environment Interaction Engineering, Kyushu Institute of technology, Japan, 2Nanyang Technology Institute
ISTS-2017-d-074/ISSFD-2017-074 ( 11:40 – 12:00 )
A Look at the Capture Mechanisms of the “Temporarily Captured Asteroids” of the Earth
Hodei Urrutxua1, Claudio Bombardelli2
1Astronautics Group, University of Southampton, UK, 2Space Dynamics Group, Technical University of Madrid
[d-17] Attitude Determination

Session Date June 7 (Wed) 16:00 – 17:40
Room Meeting Room 1
Chairpersons
ISTS-2017-d-075/ISSFD-2017-075 ( 16:00 – 16:20 )
Study on an Advanced Attitude Determination Algorithm for the ERG Spacecraft
Halil Ersin Soken, Shin-ichiro Sakai, Kazushi Asamura, Yosuke Nakamura, Takeshi Takashima
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan
ISTS-2017-d-076/ISSFD-2017-076 ( 16:20 – 16:40 )
Labelling technique for the fast Star Identification
Sangkyun Kim, Mengu Cho
Laboratory of Spacecraft Environmental Interaction Engineering, Kyushu Institute of Technology, Japan
ISTS-2017-d-077/ISSFD-2017-077 ( 16:40 – 17:00 )
Non-Traditional Robust UKF Against Attitude Sensors Faults
Demet Cilden Guler1, Halil Ersin Soken2, Chingiz Hajiyev1
1Istanbul Technical University, Turkey, 2JAXA
ISTS-2017-d-078/ISSFD-2017-078 ( 17:00 – 17:20 )
Spinning Spacecraft Attitude Filtering with Spin Parameters: Performance Evaluation with Real Data
Halil Ersin Soken1, Jozef C. van der Ha2, Shin-ichiro Sakai1
1Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan, 2Satellite Mission Design and Operations
ISTS-2017-d-079/ISSFD-2017-079 ( 17:20 – 17:40 )
Regularized particle filter with roughening for gyros bias and at titude estimation using simulated measurements
William Reis Silva1, Roberta Veloso Garcia2, Hélio Koiti Kuga1, Maria Cecília Zanardi3
1Division of Fundamental Sciences, Technological Institute of Aeronautics (ITA), Brazil, 2Sao Paulo University (USP), 3Federal University of ABC (UFABC),
[d-18] Guidance, Navigation and Control (Ascent/Descent/Deorbit)

Session Date June 7 (Wed) 16:00 – 17:40
Room Meeting Room 2
Chairpersons
ISTS-2017-d-080/ISSFD-2017-080 ( 16:00 – 16:20 )
Method of safe descent in case of off-nominal on-board situation on Russian perspective manned spacecraft “Federation”
Alexey Yu Kutomanov, Vladimir N Pochukaev
Mission Control Centre, TSNIImash, Russia
ISTS-2017-d-081/ISSFD-2017-081 ( 16:20 – 16:40 )
Flight Control Stability of Multi-Hierarchy Dynamic Inversion for Winged Rocket
Hiroshi Yamasaki, Koichi Yonemoto, Takahiro Fujikawa, Kento Shirakata, Hayato Tobiyama
Mechanical and Control Engineering, Kyushu Institute of Technology, Japan
ISTS-2017-d-082/ISSFD-2017-082 ( 16:40 – 17:00 )
Deorbit Maneuver Strategy For The Three THEMIS Probes
Sabine Frey1, Vassilis Angelopoulos2, Manfred Bester1
1Space Sciences Laboratory, University of California, Berkeley, USA, 2ESS/IGP, University of California, Los Angeles
ISTS-2017-d-083/ISSFD-2017-083 ( 17:00 – 17:20 )
A New Approach to Robust Adaptive Control with an Application to Ascent Flight Control of Launch Vehicle
Yuki Aoyagi
Department of Aeronautics and Astronautics, The University of Tokyo, Japan
ISTS-2017-d-084/ISSFD-2017-084 ( 17:20 – 17:40 )
The Study on Performance of MEMS IMU for Launch Vehicle under high vibration environment
Eri Shimane1, Shuichi Matsumoto1, Takafumi Moriguchi2, Hiroshi Nishida2, Ryohei Uchino2
1Research Unit IV, Research and Development Directorate, Japan Aerospace Exploration Agency, Japan, 2Sumitomo Precision Products
[d-19] Orbit Dynamics & Control 3

Session Date June 7 (Wed) 16:00 – 17:20
Room Meeting Room 3
Chairpersons
ISTS-2017-d-085/ISSFD-2017-085 ( 16:00 – 16:20 )
Study on Low-Thrust Stationkeeping on Geostationary Orbit
Toshinori Ikenaga, Masayoshi Utashima, Yu Nakajima, Toru Yamamoto, Tadahiko Sano, Noriyasu Inaba
Japan Aerospace Exploration Agency, Japan
ISTS-2017-d-086/ISSFD-2017-086 ( 16:20 – 16:40 )
Predictive Autonomous Orbit Control Method for Low Earth Orbit Satellites
Jerome Thomassin1, Maxime Ecochard2, Nicolas Bataille1, Guillaume Azema2
1Department of Space Mechanics, CNES, France, 2Thales Services
ISTS-2017-d-087/ISSFD-2017-087 ( 16:40 – 17:00 )
De-Orbiting Timing for Spacecraft in Geostationary Transfer Orbits to Exploit Luni-Solar Perturbations
Yue Wang, Shijie Xu
Department of Aerospace Engineering, School of Astronautics, Beihang University, China
ISTS-2017-d-088/ISSFD-2017-088 ( 17:00 – 17:20 )
Analysis of the Eccentricity Vector in Low Earth Orbits as Planar Rigid Body Motion
Javier Sanchez, Petr Kuchynka
Flight Dynamics Division, GMV at ESA/ESOC, Germany
[d-20] Formation Flying & Satellite Constellations 1

Session Date June 8 (Thu) 9:00 – 10:20
Room Meeting Room 1
Chairpersons
ISTS-2017-d-090/ISSFD-2017-090 ( 9:00 – 9:20 )
Maneuver Optimization and Collision Probability Estimation Using Separated Representations
Marc Balducci1, Brandon Jones2
1CCAR, University of Colorado – Boulder, USA, 2University of Texas at Austin
ISTS-2017-d-091/ISSFD-2017-091 ( 9:20 – 9:40 )
SAOCOM-CS: Flight Dynamics operational approach to a highly demanding formation
Itziar Barat1, Miguel Martín Serrano2, Bram De Vogeleer3, Berthyl Duesmann1, Cecilia Mezzera1
1Earth Observation System Analysis Office, European Space Agency, Netherlands, 2Earth Observation Mission Support Section, European Space Agency, 3Mission Analysis section, European Space Agency
ISTS-2017-d-092/ISSFD-2017-092 ( 9:40 – 10:00 )
Operational Flight Dynamics System for PROBA-3 Formation Flying Mission
Pablo Garcia, Catherine Praile, Jesús Robles, Ana Lola López
Flight Dynamics and Operations, GMV, Spain
ISTS-2017-d-093/ISSFD-2017-093 ( 10:00 – 10:20 )
Performance of Contactless Micro Vibration Isolator Using Flux Pinning Effect
Takuma Shibata1, Shin-ichiro Sakai2
1Department of Space and Astronautical Science, SOKENDAI [The Graduate University For Advanced Studies], Japan, 2Japan Aerospace Exploration Agency (JAXA)/ Institute of Space Astronautical Science
[d-21] Orbit Determination 1

Session Date June 8 (Thu) 9:00 – 10:40
Room Meeting Room 2
Chairpersons
ISTS-2017-d-094/ISSFD-2017-094 ( 9:00 – 9:20 )
MONTE for Orbit Determination
Jonathon J Smith
Mission Design and Navigation Software Group, California Institute of Technology / Jet Propulsion Laboratory, USA
ISTS-2017-d-095/ISSFD-2017-095 ( 9:20 – 9:40 )
Multi-arc Orbit Determination to determine Rosetta trajectory and 67P physical parameters
Bernard GODARD1, Frank Budnik2, Gabriele Bellei3, Pablo Muñoz4, Trevor Morley1
1Telespazio VEGA Deutschland GmbH, Germany, 2European Space Agency, 3Deimos Space GmbH, 4GMV
ISTS-2017-d-096/ISSFD-2017-096 ( 9:40 – 10:00 )
Shadow Navigation Support at JPL for the Rosetta Landing on Comet 67P/Churyumov-Gerasimenko
Stephen B Broschart1, Shyam Bhaskaran1, Julie Bellerose1, Ann Dietrich2, Dongsuk Han1, Robert J Haw1, Nickolaos Mastrodemos1, William M Owen, Jr.1, Brian Rush1, David Surovik3
1Jet Propulsion Laboratory, California Institute of Technology, USA, 2University of Colorado – Boulder, 3Rutgers University
ISTS-2017-d-097/ISSFD-2017-097 ( 10:00 – 10:20 )
A Quasi-Kinematic Orbit Determination Method for Deep Space Probes
Hiroshi Takeuchi, Tomohiro Yamaguchi, Makoto Yoshikawa, Tsutomu Ichikawa, Naoko Ogawa, Kazutaka Nishiyama, Takanao Saiki, Yuichi Tsuda
ISAS, JAXA, Japan
ISTS-2017-d-098/ISSFD-2017-098 ( 10:20 – 10:40 )
Orbit determination for Long-term prediction of Solar Power Sail Demonstrator IKAROS
Sho Taniguchi1, Takafumi Ohnishi1, Osamu Mori2, Hideki Kato2, Hiroshi Takeuchi2, Atsushi Tomiki2, Yuya Mimasu2, Naoko Ogawa2, Jun Matsumoto2, Taichi ITO2, Tsutomu Ichikawa2, Makoto Yoshikawa2, Shota Kikuchi3, Yosuke Kawabata3
1TECHNICAL COMPUTING SOLUTIONS UNIT, Fijitsu Limited., Japan, 2Japan Aerospace Exploration Agency., 3University of Tokyo.
[d-22] Trajectory Design & Optimization 3

Session Date June 8 (Thu) 9:00 – 10:40
Room Meeting Room 3
Chairpersons
ISTS-2017-d-099/ISSFD-2017-099 ( 9:00 – 9:20 )
Low-Thrust Geostationary Orbit Transfer Optimization to Reduce Space Radiation Damage in Solar Cells
Alexander E. Starchenko
S.P. Korolev Rocket Space Corporation “Energia”, Moscow Institute of Physics and Technology, Russia
ISTS-2017-d-100/ISSFD-2017-100 ( 9:20 – 9:40 )
Optimised GTO-GEO Transfer using Low-Thrust Propulsion
Marilena Di Carlo, Massimiliano Vasile
Department of Mechanical and Aerospace Engineering, University of Strathclyde, UK
ISTS-2017-d-101/ISSFD-2017-101 ( 9:40 – 10:00 )
Minimum Time Orbit Raising of Geostationary Spacecraft by Optimizing Feedback Gain of Steering-law
Kenji Kitamura1, Katsuhiko Yamada2, Takeya Shima1
1Advanced Technology R&D Center, Mitsubishi Electric Corporation, Japan, 2Graduate School of Engineering, Osaka University
ISTS-2017-d-102/ISSFD-2017-102 ( 10:00 – 10:20 )
Operational Concept for Orbit Raising with Low Thrust
Frederik Johannes de Bruijn, Juan Carlos Bastante
Mission Analysis, OHB System, Germany
ISTS-2017-d-103/ISSFD-2017-103 ( 10:20 – 10:40 )
Indirect Optimization of End-of-Life Disposal for Galileo Constellation Using Low Thrust Propulsion
Juan Luis Gonzalo1, Francesco Topputo2, Roberto Armellin3
1Technical University of Madrid (UPM), School of Aerospace Engineering (ETSIAE), Spain, Spain, 2Politecnico di Milano, Italy, 3Surrey Space Centre, United Kingdom
[d-23] Formation Flying & Satellite Constellations 2

Session Date June 8 (Thu) 11:00 – 12:00
Room Meeting Room 1
Chairpersons
ISTS-2017-d-104/ISSFD-2017-104 ( 11:00 – 11:20 )
Optimal Configurations for Nanosatellite Formation Flying in Binary Asteroid Environment
Andrea Capannolo, Michèle Lavagna, Fabio Ferrari, Paolo Lunghi
Department of Aerospace Science and Technology, Politecnico di Milano, Italy
ISTS-2017-d-105/ISSFD-2017-105 ( 11:20 – 11:40 )
Relative Spiral Trajectories for Low-Thrust Formation Flying
Matthew Willis1, Simone D’Amico2
1Mechanical Engineering, Stanford University, USA, 2Aeronautics and Astronautics, Stanford University
ISTS-2017-d-106/ISSFD-2017-106 ( 11:40 – 12:00 )
Optimal Trajectory Design of Formation Flying based on Attractive sets
Motoki Yamane
Aeronautics and Astronautics, Kyushu University, Japan
[d-24] Orbit Determination 2

Session Date June 8 (Thu) 11:00 – 12:40
Room Meeting Room 2
Chairpersons
ISTS-2017-d-107/ISSFD-2017-107 ( 11:00 – 11:20 )
Radar Observations of Spacecraft in Lunar Orbit
Marina Brozovic1, Ryan S Park1, Joseph G McMichael1, Jon D Giorgini1, Martin A Slade1, David S Berry1, Joseph S Jao1, Frank D Ghigo2, Patrick A Taylor3, Edgard Rivera-Valentin3
1Jet Propulsion Laboratory/California Institute of Technology, USA, 2Green Bank Observatory, 3Arecibo Observatory/Universities Space Research Association
ISTS-2017-d-108/ISSFD-2017-108 ( 11:20 – 11:40 )
Orbit Determination Adaptations for the Cassini Grand Finale
Zahi Tarzi, Julie Bellerose, Duane Roth, Rodica Ionasescu, Dylan Boone, Kevin Criddle
California Institute of Technology, Jet Propulsion Laboratory, USA
ISTS-2017-d-109/ISSFD-2017-109 ( 11:40 – 12:00 )
Resolution of Orbit Determination Prediction Instabilities at Titan During Cassini’s Solstice Mission
Dylan R Boone, Julie Bellerose
Mission Design and Navigation Section, Jet Propulsion Laboratory / California Institute of Technology, USA
ISTS-2017-d-110/ISSFD-2017-110 ( 12:00 – 12:20 )
50,000 Laps Around Mars: Navigating the Mars Reconnaissance Orbiter Through The Extended Missions (January 2009 – March 2017)
Premkumar Ramaswamy Menon, Stuart Demcak, Sean Wagner, David Jefferson, Eric Graat, Kyong J Lee, William Schulze
Mission Design & Navigation Section, Jet Propulsion Laboratory, NASA, USA
ISTS-2017-d-111/ISSFD-2017-111 ( 12:20 – 12:40 )
Method for differential phase delay calculation from radio images and its experimental verification
Huan ZHOU1, Yong Huang2, Haitao Li1, Dezhen Xu1
1Beijing Institute of Tracking and Telecommunications Technology, China, 2Shanghai Astronomical Observatory, Chinese Academy of Sciences
[d-25] Trajectory Design & Optimization 4

Session Date June 8 (Thu) 11:00 – 12:40
Room Meeting Room 3
Chairpersons
ISTS-2017-d-112/ISSFD-2017-112 ( 11:00 – 11:20 )
Approximate Two-Point Boundary Value Problem Solutions to Low Thrust Trajectory by Superposition
Ming Tony Shing1, Chit Hong Yam2, Albert Wai Kit Lau1
1Department of Physics, Hong Kong University of Science and Technology, Hong Kong, 2ispace inc., Tokyo, Japan
ISTS-2017-d-113/ISSFD-2017-113 ( 11:20 – 11:40 )
Low-Thrust Trajectory Optimization with Dualized Collocation
Nathan L. Parrish, Daniel J. Scheeres
Colorado Center for Astrodynamics Research, University of Colorado, Boulder, USA
ISTS-2017-d-114/ISSFD-2017-114 ( 11:40 – 12:00 )
A Minimum-Fuel Low-Thrust Rendez-vous solved with the Switching Systems Theory
Clement Gazzino1, Christophe Louembet1, Denis Arzelier1, Luca Cerri2, Christelle Pittet2
1LAAS-CNRS, University of Toulouse, France, 2CNES, Centre Spatial de Toulouse, Toulouse
ISTS-2017-d-115/ISSFD-2017-115 ( 12:00 – 12:20 )
Open Source Implementation of A Fast and Precise N-body Low-Thrust Propagator
Weichen Xiao1, Wenhan Chiu1, Chit Hong Yam2
1Department of Physics, The Hong Kong University of Science and Technology, Hong Kong, 2ispace inc., Japan
ISTS-2017-d-116/ISSFD-2017-116 ( 12:20 – 12:40 )
Unified Formulation for Element-Based Indirect Trajectory Optimization
Juan Luis Gonzalo1, Claudio Bombardelli1, Francesco Topputo2
1Technical University of Madrid (UPM), School of Aerospace Engineering (ETSIAE), Spain, Spain, 2Politecnico di Milano, Italy
[d-26] Formation Flying & Satellite Constellations 3

Session Date June 8 (Thu) 14:00 – 15:20
Room Meeting Room 1
Chairpersons
ISTS-2017-d-117/ISSFD-2017-117 ( 14:00 – 14:20 )
Rendezvous control of spacecrafts via constrained optimal control using generating functions
Kenji Fujimoto2, Dijian Chen1
1Department of Mechanical Science and Engineering, Nagoya University, 2Department of Aeronautics and Astronautics, Kyoto University, Japan
ISTS-2017-d-118/ISSFD-2017-118 ( 14:20 – 14:40 )
Attitude and Orbit Coupled Tumbling Space Debris Tracking Control
Shuquan Wang, Lingchao Zhu
Technology and Engineering Center for Space Utilization, Chinese Academy of Sciences, China
ISTS-2017-d-119/ISSFD-2017-119 ( 14:40 – 15:00 )
Angles-Only Relative Orbit Determination during the AVANTI experiment
Jean Sebastien Ardaens, Gabriella Gaias
GSOC, DLR, Germany
ISTS-2017-d-120/ISSFD-2017-120 ( 15:00 – 15:20 )
Effect of observation by angle only navigation to plan non-cooperative approach for ADR
Masayuki Ikeuchi
Safety and Mission Assurance Department, JAXA, Japan
[d-27] Orbit Determination 3

Session Date June 8 (Thu) 14:00 – 15:00
Room Meeting Room 2
Chairpersons
ISTS-2017-d-122/ISSFD-2017-122 ( 14:00 – 14:20 )
On-board Orbit Determination for a Deep Space CubeSat
Boris SEGRET1, Daniel Hestroffer2, Gary Quinsac3, Jordan Vannitsen4, Jiun-Jih Miau4, Jyh-Ching Juang4, Benoît Mosser1
1LabEx ESEP, Observatory of Paris, France, France, 2IMCCE, Observatory of Paris, France, 3Paris Sciences Lettres, Observatory of Paris, France, 4National Cheng Kung University, Taiwan
ISTS-2017-d-123/ISSFD-2017-123 ( 14:20 – 14:40 )
A Study of the Navigation for a Spacecraft by Using the Reduced order Filter
Tsutomu Ichikawa
Japan Aeospace Exploration Agency (JAXA), Japan
ISTS-2017-d-124/ISSFD-2017-124 ( 14:40 – 15:00 )
The analysis of OD accuracy and orbit maintenance strategy of Chang’E-4 relay satellite
Cheng Cheng, Fan Min, Chen Shaowu, Li Zan, Hao Wanhong
Beijing Institute of Tracking and Telecommunications Technology, China
[d-28] Trajectory Design & Optimization 5

Session Date June 8 (Thu) 14:00 – 15:40
Room Meeting Room 3
Chairpersons
ISTS-2017-d-126/ISSFD-2017-126 ( 14:00 – 14:20 )
A Smoothed Eclipse Model for Solar Electric Propulsion Trajectory Optimization
Jonathan David Aziz1, Jeffrey S Parker1, Daniel J Scheeres1, Jacob A Englander2
1University of Colorado Boulder, USA, 2NASA Goddard Space Flight Center
ISTS-2017-d-127/ISSFD-2017-127 ( 14:20 – 14:40 )
Robust Differential Dynamic Programming for Low-Thrust Trajectory Design: Approach with Robust Model Predictive Control Technique
Naoya Ozaki1, Stefano Campagnola2, Ryu Funase1
1Department of Aeronautics and Astronautics, University of Tokyo, Japan, 2ISAS/JAXA
ISTS-2017-d-128/ISSFD-2017-128 ( 14:40 – 15:00 )
Initial Results of a New Method for Optimizing Low-thrust Gravity-assist Missions
Volker Maiwald
German Aerospace Center (DLR), Institute of Space Systems, Germany
ISTS-2017-d-129/ISSFD-2017-129 ( 15:00 – 15:20 )
Design and Validation of Ultra Low Thrust Transfers to the Sun-Earth Saddle Point with Application to LISA Pathfinder Mission Extension
Francesco Topputo1, Diodene Alessandro Dei Tos1, Masaki Nakamiya1, Mirco Rasotto2, Florian Renk3
1Politecnico di Milano, Italy, 2Dinamica Srl, 3European Space Agency
ISTS-2017-d-130/ISSFD-2017-130 ( 15:20 – 15:40 )
Solar Power Sail Trajectory Design for Jovian Trojan Exploration
Takanao Saiki, Jun Matsumoto, Osamu Mori, Junichiro Kawaguchi
Japan Aerospace Exploration Agency, Japan
[d-29] Formation Flying & Satellite Constellations 4

Session Date June 8 (Thu) 16:00 – 17:00
Room Meeting Room 1
Chairpersons
ISTS-2017-d-131/ISSFD-2017-131 ( 16:00 – 16:20 )
Robust Spacecraft Swarm Design using Generalized E/I-Vector Separation
Adam Koenig, Simone D’Amico
Stanford University, Department of Aeronautics and Astronautics, Space Rendezvous Laboratory, USA
ISTS-2017-d-132/ISSFD-2017-132 ( 16:20 – 16:40 )
Satellite Constellations for Altimetry
Alain LAMY, Josiane Costeraste
Flight dynamlics department (DCT/SB/MS), CNES, France
ISTS-2017-d-134/ISSFD-2017-134 ( 16:40 – 17:00 )
Galileo Extended Slots Characterisation and relation with the Nominal Constellation
Andres Ayala1, Ruben Castro2, Nityaporn Sirikan3, Daniel Blonski4, Daniel Navarro4
1GMV at ESTEC/ESA/OPS-GN, Netherlands, 2WGS at ESTEC/ESA/OPS-GN, 3ESTEC/ESA/NAV-NMD, 4ESTEC/ESA/NAV-NMS
[d-30] Orbit Determination 4

Session Date June 8 (Thu) 16:00 – 17:20
Room Meeting Room 2
Chairpersons
ISTS-2017-d-135/ISSFD-2017-135 ( 16:00 – 16:20 )
Deep-Space Navigation Using Optical Communications Systems
Tomas Jorge Martin-Mur, Sarah Elizabeth McCandless
Jet Propulsion Laboratory, California Institute of Technology, USA
ISTS-2017-d-136/ISSFD-2017-136 ( 16:20 – 16:40 )
The effect of solution technique on the autonomous orbit determination accuracy of Lagrangian navigation satellite system
Youtao Gao1, Bingyu Jin1, Tanran Zhao1, Bo Xu2
1Astronautics, Nanjing University of Aeronautics and Astronautics, China, 2Astronomy and Space Science, Nanjing University
ISTS-2017-d-138/ISSFD-2017-138 ( 16:40 – 17:00 )
Simplified Covariance Estimation and Target Observation Management Method for On-Board Optical Navigation of Deep Space Probe
Yosuke Kawabata1, Takanao Saiki2, Yasuhiro Kawakatsu2
1Department of Advanced Energy, The University of Tokyo, Japan, 2ISAS, JAXA
ISTS-2017-d-139/ISSFD-2017-139 ( 17:00 – 17:20 )
Autonomous Orbit Determination of Multiple Spacecraft Using Active Sensing of Satellite-to-Satellite Tracking
Kota Kakihara
Department of Aeronautics and Astronautics, The University of Tokyo, Japan
[d-31] Orbit Determination 5

Session Date June 9 (Fri) 14:00 – 15:40
Room Meeting Room 2
Chairpersons
ISTS-2017-d-140/ISSFD-2017-140 ( 14:00 – 14:20 )
Generalized Image Navigation and Registration Method Based on Kalman Filter
Handol KIM2, Ahmed Kamel1, Dochul Yang2, Chul-Min Park3, Jin Woo4
1Kamel Engineering Services (KES) , 2Korea Aerospace Research Institute (KARI), Korea, 3Korea Aerospace Industries, ltd. (KAI), 4Korea Meteorological Administration (KMA)
ISTS-2017-d-141/ISSFD-2017-141 ( 14:20 – 14:40 )
Satellite Autonomous Navigation for Korea Regional Navigation Satellite System with No Ground Links
Hyungjik Oh1, Young-Rok Kim2, Chandeok Park1
1Department of Astronomy, Yonsei University, Korea, 2Korea Aerospace Research Institute
ISTS-2017-d-142/ISSFD-2017-142 ( 14:40 – 15:00 )
Dual-Satellite Geolocation: Simultaneous Ephemeris Correction and Source Localization
Jeroen L. Geeraert, Jay W. McMahon
Colorado Center for Astrodynamics Research, University of Colorado at Boulder, USA
ISTS-2017-d-143/ISSFD-2017-143 ( 15:00 – 15:20 )
Filter Tuning Using the Chi-Squared Statistic
Tyler Bruce Lilly-Salkowski
Flight Dynamics Facility, NASA, USA
ISTS-2017-d-144/ISSFD-2017-144 ( 15:20 – 15:40 )
Generalised Polynomial Chaos Based Particle Filter for Orbit Determination
YANG YANG1, Yang Yang2, Kefei Zhang1, Yanlong Bu3
1School of Science, RMIT University, Australia, Australia, 2Space Environment Research Centre (SERC) Limited, Australia, 3Aerospace Flight Dynamics Laboratory, Beijing Aerospace Control Centre, China
[d-32] Mission Analysis & Design 1

Session Date June 9 (Fri) 14:00 – 15:40
Room Meeting Room 3
Chairpersons
ISTS-2017-d-145/ISSFD-2017-145 ( 14:00 – 14:20 )
Advanced methods of low cost mission design for Jovian moons exploration
Alexey Grushevskii, Yui Golubev, Victor Koryanov, Andrey Tuchin, Denis Tuchin
Russian Academy of Science, Keldysh Institute of Applied Mathematics, Russia
ISTS-2017-d-146/ISSFD-2017-146 ( 14:20 – 14:40 )
Solar Probe Plus: Primary and Backup Launch Windows
Yanping Guo
Johns Hopkins University Applied Physics Laboratory, USA
ISTS-2017-d-147/ISSFD-2017-147 ( 14:40 – 15:00 )
Solar Orbiter Trajectory Profile and Navigation Challenges
Jose Manuel Sanchez Perez1, Frank Budnik2
1Ground Systems Engineering – Mission Analysis Section, European Space Agency, Germany, 2Flight Dynamics Division, European Space Agency
ISTS-2017-d-148/ISSFD-2017-148 ( 15:00 – 15:20 )
AIDA: Measuring Asteroid Binary System parameters and DART-Imparted Deflection using the AIM Spacecraft
Julie Bellerose, Shyamkumar Bhaskaran, Steven Chesley
Jet Propulsion Laboratory, Caltech, USA
ISTS-2017-d-149/ISSFD-2017-149 ( 15:20 – 15:40 )
Guidance Navigation and Control Challenges for the ESA Asteroid Impact Mission
Massimo Casasco, Jesus Gil Fernandez, Guillermo Ortega, Ian Carnelli
European Space Agency, Netherlands
[d-33] Attitude Control 1

Session Date June 9 (Fri) 14:00 – 15:20
Room Multi-purpose Room
Chairpersons
ISTS-2017-d-150/ISSFD-2017-150 ( 14:00 – 14:20 )
LMI-based Mixed H2 /Hinfinity Control with Regional Constraints for Spacecraft Attitude Tracking
Takahiro Sasaki, Takashi Shimomura, Sayaka Kanata
Department of Aerospace Engineering, Osaka Prefecture University, Japan
ISTS-2017-d-151/ISSFD-2017-151 ( 14:20 – 14:40 )
Fast slew maneuvers for the High-Torque-Wheels BIROS satellite
Paul Acquatella
DLR, German Aerospace Center, Institute of System Dynamics and Control, Germany
ISTS-2017-d-152/ISSFD-2017-152 ( 14:40 – 15:00 )
Single-Axis Pointing of Underactuated Spacecraft with Residual Angular Momentum
Alessandro Zavoli1, Fabrizio Giulietti2, Giulio Avanzini3, Guido De Matteis1
1Departemnt of Mechanical & Aerospace Engineering, Sapienza – Università di Roma, Italy, 2Department of Industrial Engineering, Università di Bologna , 3Department of Engineering, Università del Salento
ISTS-2017-d-153/ISSFD-2017-153 ( 15:00 – 15:20 )
Model Error Compensator for Attitude Control of 2-Wheel Spacecraft with On-line FRIT based Tuning
Hiroaki Endou, Kazuma Sekiguchi, Kenichiro Nonaka
Tokyo City University, Japan
[d-34] Orbit Determination 6

Session Date June 9 (Fri) 16:00 – 16:40
Room Meeting Room 2
Chairpersons
ISTS-2017-d-155/ISSFD-2017-155 ( 16:00 – 16:20 )
Orbit determination for the MICROSCOPE mission: specificities and performance
David PASCAL1, John Moyard1, Flavien Mercier1, Pierre-Yves Guidotti2, Romain Mathieu3, Thomas Junique3
1Flight Dynamics, CNES, France, 2Project Management, CNES, 3Radio-frequency and navigation, CNES
ISTS-2017-d-156/ISSFD-2017-156 ( 16:20 – 16:40 )
Optical Tracking Extended Network in Support to Operational Flight Dynamics and Conjunction Analysis for Meteosat
Stefano Pessina, Milan Klinc
EUMETSAT, Germany
[d-35] Mission Analysis & Design 2

Session Date June 9 (Fri) 16:00 – 17:40
Room Meeting Room 3
Chairpersons
ISTS-2017-d-158/ISSFD-2017-158 ( 16:00 – 16:20 )
Mission Design Problems for Spectrum-Roentgen-Gamma Project
Natan Eismont, Ravil Nazirov, Vadim Arefiev
Department of Space flight dynamics, Space Research Institute of the Russian Academy of Sciences, Russia
ISTS-2017-d-159/ISSFD-2017-159 ( 16:20 – 16:40 )
EQUULEUS Mission Analysis: Design of the Transfer Phase
Kenta Oshima1, Stefano Campagnola2, Chit Hong Yam2, Yuki Kayama3, Yasuhiro Kawakatsu2, Naoya Ozaki3, Quentin Verspieren3, Kota Kakihara3, Kenshiro Oguri3, Ryu Funase3
1Waseda University, Japan, 2JAXA, 3The University of Tokyo
ISTS-2017-d-072/ISSFD-2017-072 ( 16:40 – 17:00 )
Systematic Computation and Stationkeeping Analysis of Quasi Halo Orbits in High-Fidelity Model for 6U CubeSat EQUULEUS
Kenshiro Oguri1, Kota Kakihara1, Stefano Campagnola2, Naoya Ozaki1, Kenta Oshima3, Tomohiro Yamaguchi2, Ryu Funase1
1The University of Tokyo, Japan, 2JAXA, 3Waseda University
ISTS-2017-d-160/ISSFD-2017-160 ( 17:00 – 17:20 )
Design and Analysis of a CubeSat Lunar far-side Positioning Mission
Hongru Chen1, Lei Liu2, Yazhe Meng1, Zhenyu Xu1
1Technology and Engineering Center for Space Utilization, Chinese Academy of Sciences, China, 2Beijing Aerospace Control Center
ISTS-2017-d-161/ISSFD-2017-161 ( 17:20 – 17:40 )
SIRIUS-DV: The new Flight Dynamics algorithms for the future CNES missions
Ivan Llamas1, Jean-Jacques Wasbauer2, Yannick Tanguy2, Michel Lacotte2
1Flight Dynamics and Operations, GMV, Spain, 2CNES
[d-36] Attitude Control 2

Session Date June 9 (Fri) 16:00 – 17:40
Room Multi-purpose Room
Chairpersons
ISTS-2017-d-162/ISSFD-2017-162 ( 16:00 – 16:20 )
Experimental Study on Line-of-Sight (LOS) Attitude Control Using Control Moment Gyros under Micro-Gravity Environment
Hirohisa Kojima, Kana Hiraiwa, Yasuhiro Yoshimura, Koki Hidaka
Department of Aerospace Engineering, Tokyo Metropolitan University, Japan
ISTS-2017-d-163/ISSFD-2017-163 ( 16:20 – 16:40 )
Attitude Control using three Control Moment Gyros
Sho Nonomura1, Andrew William Meldrum2, Katsuhiko Yamada1, Yasuhiro Shoji1
1Graduate School of Engineering, Osaka University, Japan, 2School of Engineering, Osaka University
ISTS-2017-d-164/ISSFD-2017-164 ( 16:40 – 17:00 )
Conceptual Study of 6 DOF Precision Control of Payload Using 6 Axis Hybrid Actuator
Norimasa Yoshida1, Seiichi Shimizu2, Kazuhide Kodeki2
1Department of Aerospace Engineering, Osaka Prefecture University, Japan, 2Advanced Technology R&D Center, Mitsubishi Electric Corp.
ISTS-2017-d-165/ISSFD-2017-165 ( 17:00 – 17:20 )
Singularity Avoidance/Passage Steering Logic for a Variable-speed Double-gimbal Control Moment Gyro Based on Inverse Kinematics
Shota Kawajiri1, Saburo Matunaga2
1Department of Mechanical and Aerospace Engineering, Tokyo Institute of Technology, Japan, 2Department of Mechanical Engineering, Tokyo Institute of Technology
ISTS-2017-d-166/ISSFD-2017-166 ( 17:20 – 17:40 )
Optimal Attitude Control for Spacecraft Using two Variable-Speed Control Moment Gyros
Daiki Higashiyama
Graduate School of Engineering, Osaka university, Japan
[e-1] Plasma Flows (1)

Session Date June 7 (Wed) 11:00 – 12:00
Room Meeting Room 15
Chairpersons
2017-e-01 ( 11:00 – 11:20 )
Study on Side Force Control for High-Angle-of-Attack Slender Body Using Plasma Actuator and Minute Bump
Rei Fujieda, Tomotaka Suzuki, Hiroyuki Nishida
Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology, Japan
2017-e-02 ( 11:20 – 11:40 )
Computational studies of body force production process and performance improvement in a dielectric-barrier-discharge plasma actuator
Shintaro Sato, Masayuki Takahashi, Naofumi Ohnishi
Department of Aerospace Engineering, Tohoku University, Japan
2017-e-03 ( 11:40 – 12:00 )
The Effect of Voltage Frequency on Thrust Production of Multi-Electrode Plasma Actuator
Takashi Matsuno1, Ai Fukuda1, Hiromitsu Kawazoe1, Kumi Nakai2, Hiroyuki Nishida3
1Department of Mechanical and Aerospace Engineering, Tottori University, Japan, 2Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology, 3Institute of Engineering, Tokyo University of Agriculture and Technology
[e-2] Plasma Flows (2)

Session Date June 8 (Thu) 9:00 – 10:40
Room Meeting Room 15
Chairpersons
2017-e-05 ( 9:00 – 9:20 )
New Magnetic Field Setup for Electromagnetic Flow Control of Lifting Reentry Vehicle
Hirotaka Otsu
Department of Mechanical and Systems Engineering, Ryukoku University, Japan
2017-e-06 ( 9:20 – 9:40 )
Experimental Investigation of the Role of an Insulating Boundary in the Electrodynamic Force Generation in a Rarefied Arc Flow
Naoki Fukuda1, Takuma Toyodome1, Hiroshi Katsurayama1, Kentaro Tomita2, Makoto Matsui3, Yasuo Katoh1
1Graduate School of Sciences and Technology for Innovation, Yamaguchi University, Japan, 2Interdisciplinary Graduate School of Engineering Sciences, Kyushu University, 3Graduate School of Integrated Science and Technology, Shizuoka University
2017-e-07 ( 9:40 – 10:00 )
Electron Density Measurement by Mach-Zehnder Interferometer Using CO2 Laser for an Atmospheric Pressure Plasma
Takafumi Yamada
Department of Engineering, Shizuoka University, Japan
2017-e-08 ( 10:00 – 10:20 )
Temperature Estimations of SiC Ablations with Several Kinds of Narrow Band-pass Filters
Makoto Hashimoto1, Nurul Malisa1, Masato Funatsu2, Gen Morioka3, Masahiro Ozawa4
1Department of Mechanical Science and Technology, School of Science and Technology, Gunma University, Japan, 2Division of Mechanical and Science, Graduate School of Science and Technology, Gunma University, 3Mitsubishi Electric Engineering Co., Ltd., 4Chuo Engineering Co., Ltd.
2017-e-09 ( 10:20 – 10:40 )
Numerical Estimation of Laser-Ablation Propulsion Performance in Supersonic Flight for Donut-Mode Laser Guided Spherical Capsule Launch System
Chongfa Xie, Duc Thuan Tran, Koichi Mori
Department of Aerospace Engineering, Nagoya University, Japan
[e-3] Atmospheric Entry (1)

Session Date June 8 (Thu) 11:00 – 12:20
Room Meeting Room 15
Chairpersons
2017-e-10 ( 11:00 – 11:20 )
Temperature-controlled Material Probe for High-enthalpy Flows
Bartomeu Massuti-Ballester, Adam S. Pagan, Georg Herdrich
Institute of Space Systems, University of Stuttgart, Germany
2017-e-11 ( 11:20 – 11:40 )
Development and Demonstration of Ablation Sensor Unit for Light-weight Ablator
Kazuhisa Fujita1, Toshiyuki Suzuki1, Takeharu Sakai2, Yuki Danzuka3, Kenta Iwamoto2, Takashi Ozawa1, Naomi Takizawa1, Yuichi Ishida1, Yasuhide Watanabe1
1Japan Aerospace Exploration Agency, Japan, 2Tottori University, 3Nagoya University
2017-e-12 ( 11:40 – 12:00 )
One-dimensional Ablation Analysis of Lightweight CFRP Ablators with Coking
Sumio Kato1, Shoichi Matsuda1, Naoyuki Shimada3, Shunsuke Sakai2, Keiichi Okuyama4, Bianca Szasz4, Takayuki Shimoda5
1Mechanical Systems Engineering, Univrsity of the Ryukyus, Japan, 2Student, Mechanical Systems Engineering, Graduate School of Engineering and Science,Univrsity of the Ryukyus, 3Asahi Kinzoku Kogyo Inc., 4Department of Applied Science for Integrated System Engineering, Kyushu Institute of Technology , 5Thermal Systems and Fluid Dynamics Group, ISAS, JAXA
2017-e-13 ( 12:00 – 12:20 )
Thermal Response Analysis Of Porous Carbon-based Non-Ablative Heat shield In An Arcjet Flow Condition
Takeharu Sakai1, Takumi Horiuchi2, Hiroki Fukui2, Yuuichi Ishida3, Toshiyuki Suzuki3, Kazuhisa Fujita3
1Department of Mechanical and Aerospace Engineering, Tottori University, Japan, 2Department of Aerospace Engineering, Nagoya University, 3JAXA
[e-4] Atmospheric Entry (2)

Session Date June 8 (Thu) 14:00 – 15:40
Room Meeting Room 15
Chairpersons
2017-e-14 ( 14:00 – 14:20 )
Visualization of Wake Flows of Supersonic Mars Entry Capsule with Light Gus Gun
Satoshi Nomura1, Kao Ito2, Shiogo Matsuyama1, Kazuhisa Fujita1
1JAXA, Japan, 2Yokohama National University
2017-e-15 ( 14:20 – 14:40 )
Numerical Analysis of Flow Conditions Generated by Hyper Velocity Expansion Tube
Tohru Yamada
Graduate School of Integrated Science and Technology, Shizuoka University, Japan
2017-e-16 ( 14:40 – 15:00 )
VUV Spectrum Measurements behind Strong Shock Wave for Hypervelocity Earth Reentry
Taito Kawakami
Shizuoka university, Japan, Japan
2017-e-17 ( 15:00 – 15:20 )
Aerodynamic characteristics of Hyflex lifting body in shock tunnel HIEST
Hide Tanno, Tomoyuki Komuro, Kazuo Sato, Katsuhiro Itoh
Kakuda Space Center, Japan Aerospace Exploration Agency, Japan
2017-e-18 ( 15:20 – 15:40 )
Simulation of Ionization and Electronic Excitation in Hypersonic Shock Tube Flows Using DSMC
Takashi Ozawa1, Satoshi Nomura1, Sayaka Nishimura2, Taito Kawakami2, Kazuhisa Fujita1
1Research and Development Directorate, Japan Aerospace Exploration Agency, Japan, 2Department of Engineering, Shizuoka University
[e-5] Aerodynamic decelerator, Balloon (1)

Session Date June 8 (Thu) 16:00 – 17:20
Room Meeting Room 15
Chairpersons
2017-e-19 ( 16:00 – 16:20 )
Aerothermodynamic Studies on Low-Ballistic-Coefficient Mars Aerocapture Vehicle with Drag Modulation and Ion Thruster
Kojiro Suzuki
Graduate School of Frontier Sciences, The University of Tokyo, Japan
2017-e-20 ( 16:20 – 16:40 )
The thermal-durability evaluation of inflatable structure for a deployable aeroshell using ICP heater
Kazushihe Matsumaru1, Mayuko Tanaka2, Osamu Imamura3, Kazuhiko Yamada4
1Department of Mechanical engineering, Nihon University, Japan, 2Department of Applied Mechanics, Waseda University, Tokyo, 3Department of Sustainable Engineering, Nihon University, 4The Institute of Space and Astronautical Science, JAXA
2017-e-21 ( 16:40 – 17:00 )
Aeroshell Configuration for Flexible Capsule for Martian Atmospheric Entry
Yasumasa Watanabe1, Kojiro Suzuki2
1Department of Aeronautics and Astronautics, The University of Tokyo, Japan, 2Department of Advanced Energy, The University of Tokyo
2017-e-22 ( 17:00 – 17:20 )
Coupled Analysis of Aerodynamics, Deformation and Motion for Mars Probe with Flexible Surface in Upper Atmosphere
Kakeru Tokunaga
Department of Aeronautics and Astronautics, University of Tokyo, Japan
[e-6] Aerodynamic Decelerator, Balloon (2)

Session Date June 9 (Fri) 9:00 – 10:20
Room Meeting Room 15
Chairpersons
2017-e-23 ( 9:00 – 9:20 )
Flight Test of Supersonic Parachute Using JAXA’s Research Helicopter
Toshiyuki Suzuki1, Hiroki Takayanagi1, Takashi Ozawa1, Satoshi Nomura1, Hiroka Inoue1, Naomi Takizawa1, Kazuhisa Fujita1, Yoshinori Minami1, Hirokazu Adachi1, Yoshihisa Aoki1, Toshio Fukui1, Toshiaki Daibo1, Takashi Mugitani1, Taro Tsukamoto1, Shinji Ishimoto1, Takehiro Kumagai2, Hirofumi Shirouzu2, Koji Ohga2
1Research and Development Directorate, Japan Aerospace Exploration Agency, Japan, 2Aeronautical Technology Directorate, Japan Aerospace Exploration Agency
2017-e-25 ( 9:20 – 9:40 )
Wind Tunnel Tests on Pressure Oscillation in Supersonic Parachutes
Kazuki Mizuta
Department of Mechanical Engineering, Shizuoka University, Japan
2017-e-26 ( 9:40 – 10:00 )
Analytical Study on Transient Behavior to Dive into Gliding Flight of Parafoil-type Vehicle
Takahiro Moriyoshi1, Hiroki Kanemaru1, Hisashi Nagano2, Kazuhiko Yamada3, Hiroyuki Nishida1
1The Graduate School of Engineering, Tokyo University of Agriculture and Technology, Japan, 2School of Fundamental Science and Engineerring, Waseda University, 3ISAS, JAXA
2017-e-27 ( 10:00 – 10:20 )
A High-Speed Flight Experiment System with Combination of a High Altitude Balloon and a Rocket Booster for Flight Demonstration of Technologies needed for Spaceplane
Yusuke Maru1, Shujiro Sawai1, Harunori Nagata2, Nobutaka Bando1, Shin-ichiro Sakai1, Tetsuo Yoshimitsu1, Ken Goto1, Hikaru Eguchi3
1Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan, 2Hokkaido University, 3The Graduate University for Advanced Studies
[e-7] Aerodynamics (1)

Session Date June 9 (Fri) 11:00 – 12:00
Room Meeting Room 15
Chairpersons
2017-e-29 ( 11:00 – 11:20 )
Aerodynamic Analysis on Flight Vehicle with Protuberant Devices
Toshiaki Harada1, Keiichi Kitamura1, Sotoshi Nonaka2
1College of Engineering Science, Yokohama National University, Japan, 2The Institute of Space and Astronautical Science, JAXA
2017-e-31 ( 11:20 – 11:40 )
Experimental Investigation on the Effectiveness of Micro-jets to restrain the base pressure of space vehicles.
musavir bashir
School of Aerospace Engineering, University Sains Malaysia (USM), Malaysia
2017-e-32 ( 11:40 – 12:00 )
Flow Induced Vibrations of Entry Capsule Models
Koju Hiraki1, Kota Tanaka1, Yuma Yanaga1, Harald Kleine2
1Department of Mechanical and Control Engineering, Kyushu Institute of Technology, Japan, 2School of Engineering and Information Technology, University of New South Wales
[e-8] Aerodynamics (2)

Session Date June 9 (Fri) 14:00 – 15:40
Room Meeting Room 15
Chairpersons
2017-e-33 ( 14:00 – 14:20 )
Aeroelastic Analysis for the High Altitude Propeller by Using Fluid-Structural Interaction Method
Zhengyu Qu, Yanchu Yang, Ying Nie
Center for LTA system research and development, Academy of Opto-Electronics, Chinese Academy of Science, China
2017-e-34 ( 14:20 – 14:40 )
Design of an Efficient Propeller for Low-Density Application
Reuben Jikeme Umunna, Koju Hiraki
Kyushu Institute of Technology, Mechanical Engineering, Japan
2017-e-35 ( 14:40 – 15:00 )
Effect of Leading Edge Profile over the Flow Phenomenon of Delta Wing
RAMAKRISHNA MADHIRA1, SENTHIL KUMAR C2
1ASST. PROF., DEPT. OF AERONAUTICAL ENGG., TAGORE ENGINEERING COLLEGE, CHENNAI, INDIA, India, 2ASST. PROF. (SG), DEPT. OF AEROSPACE ENGG., MIT CAMPUS, ANNA UNIVERSITY, CHENNAI, INDIA
2017-e-36 ( 15:00 – 15:20 )
Mach and Reynolds Numbers Effects on Aerodynamics of Delta Wing at Low Reynolds and Subsonic High Mach Numbers Regimes in Experiment of Mars Wind Tunnel
Taku Nonomura, Sintaro Ando, Keisuke Asai
Deparment of Aeospace Engineering, Tohoku University , Japan
2017-e-37 ( 15:20 – 15:40 )
Study on The Interaction Mechanism of Coaxial Jet Exhausted from a body in Hypersonic Flow
Mohammad Saeed Samara1, Yasumasa Watanabe2, Kojiro Suzuki1
1department of advanced energy, university of tokyo, Japan, 2department of aeronautics and astronautics, university of tokyo
[e-9] Computational Fluid Dynamics

Session Date June 9 (Fri) 16:00 – 17:40
Room Meeting Room 15
Chairpersons
2017-e-38 ( 16:00 – 16:20 )
Improvement of the SLAU2 Scheme for a Propagating Intense Shock Wave
Yukiharu Iwamoto1, Masakatsu Murakami2, Hiromichi Toyota1, Xia Zhu1
1Graduate School of Science and Engineering, Department of Engineering for Production and Environment, Ehime University, Japan, 2Institute of Laser Engineering, Osaka University
2017-e-39 ( 16:20 – 16:40 )
On Causal Structures in Fluid Mechanics
TREVOR H MOULDEN
AEROSPACE, UNIVERSITY OF TENNESSEE SPACE INSTITUTE, USA
2017-e-40 ( 16:40 – 17:00 )
Numerical Study of Cryogenic Hydrogen Jet in Crossflow under Supercritical Pressures
Satoshi Kozuka1, Daiki Muto2, Hiroshi Terashima3, Nobuyuki Tsuboi1
1Kyushu Institute of Technology, Japan, 2JAXA, 3Hokkaido University
2017-e-41 ( 17:00 – 17:20 )
The Interfacial Nanobubbles Studied by Molecular Dynamics Simulations
Tsu-Hsu Yen
Marine Science, R.O.C Naval Academy, Taiwan
2017-e-42 ( 17:20 – 17:40 )
Numerical Investigation of the Radiation Transfer in a Laser Sustained Plasma Wind Tunnel with Carbon-dioxide Gas
Ehara Yutaro1, Katsurayama Hiroshi1, Makoto Matsui2, Takeharu Sakai3, Katoh Yasuo1
1Graduate School of Sciences and Tecnology for innovation, Yamaguchi University, Japan, 2Graduate School of Integrated Science and Tecnology, Shizuoka University, 3Graduate School of Engineering, Tottori University
[f-1] Mission1

Session Date June 6 (Tue) 9:00 – 10:20
Room Pearl Room A
Chairpersons
2017-f-001 ( 9:00 – 9:20 )
Space Scout Wasps: Concept of A Distribute Space Awareness System
Wei E1, Cheng Wei1, Sihang Zhang2, Xinwei Wang2, Yang Zhao1
1School of Astronautics and Aeronautics, Harbin Institute of Technology, China, 2Beihang University, China
2017-f-002 ( 9:20 – 9:40 )
Preliminary Structural and System Design for AMMEQ-1: A Step Towards QKD
EuGene Kim1, Xiaofeng Wu1, Trevor Kwan1, Robert Bedington2, Xueliang Bai2, Alex Ling2
1School of Aerospace, Mechanical, Mechatronics Engineering, The University of Sydney, Australia, 2Centre for Quantum Technologies, Singapore
2017-f-003 ( 9:40 – 10:00 )
Space timing reference option for space applications provided by Space Precision Atomic-clock TIming Utility Mission satellite “SPATIUM”
Kateryna Aheieva1, Rahmi Rahmatillah1, Ryotaro Ninagawa1, Hirokazu Masui1, Takashi Yamauchi1, Sangkyun Kim1, Mengu Cho1, Chow Chee Lap2, Tse Man Siu2, Li King Ho2
1Laboratory of Spacecraft Environmental and Interaction Engineering, Kyushu Institute of Technology, Japan, 2Tamasek Lab, Nanyang Technological University
2017-f-004 ( 10:00 – 10:20 )
Precise Location of CubeSats Using Signal Arrival Time Lag
Ernest Teye Matey, BIRDS Project Members, BIRDS Partners, George Maeda, Sangkum Kim, Hirokazu Masui, Mengu Cho
Applied Science for Integrated System Engineering; Laboratory of Spacecraft Environment Interaction Engineering., Kyushu Institute of Technology, Japan
[f-2] Mission2

Session Date June 6 (Tue) 11:00 – 12:20
Room Pearl Room A
Chairpersons
2017-f-005 ( 11:00 – 11:20 )
Development Status of The Civilian Satellite “Dream Sat 01”
Ippei Oshima1, Hideaki Kikuchi2, Hirokazu Tahara3, Ryota Hirai2, Tomoyuki Ikeda4, Ikujiro Ao5, Hiroyuki Iijima5, Shin Takeuchi6, Osamu Konno6, Taizoh Yamamoto7, Naoki Kabaya8, Giichi Sakemi9, Kenji Ishida10, Yu Okumura11, Yuji Nishikawa11, Shouhei Minami11, Kazuhito Miura11, Soopal Hong11, AstreX Kansai Satellite Group2, Dream Satellite Project Team2
1Kobe University, Japan, 2AstreX, 3Osaka Institute of Technology, 4Tokai University, 5KOBE ENGINEERING Co., Ltd., 6Nissin inc., 7YAMAMOTO METAL TECHNOS CO., LTD., 8FUTUREAGRI Co., Ltd., 9Mitsubishi Electric Corporation, 10JAPAN FUTEC Co., Ltd., 11Nichiwa System
2017-f-007 ( 11:20 – 11:40 )
Nano satellite “ITF-2” developed by University of Tsukuba YUI project
Atsushi Yasuda1, Akihiro Nagata2, Hiromasa Watanabe1, Toshihiro Kameda3
1College of Physics, School of Science and Engineering, University of Tsukuba, Japan, 2College of Engineering Systems, School of Science and Engineering, University of Tsukuba, 3Institute of Engineering Mechanics and Energy, University of Tsukuba
2017-f-008 ( 11:40 – 12:00 )
Mission Definition and Preliminary Design of NanoDragon, the first Vietnamese Nanosatellite
Minh Anh Pham
Graduated School of System Design and Management , Keio University, Japan
2017-f-009 ( 12:00 – 12:20 )
Software Demodulation Technique for the Store and Forward System on-board Vietnam’s first Micro-Satellite, MicroDragon
James Harpur, Toshinori Kuwahara, Kazuya Yoshida, Ngo Thanh Cong, Ta Phuong Linh, Nguyen Phuong Mai, Tran Van Ninh, Nguyen Minh Thao
Space Robotics Laboratory, Tohoku University, Japan
[f-3] Mission3

Session Date June 6 (Tue) 14:00 – 15:40
Room Pearl Room A
Chairpersons
2017-f-010 ( 14:00 – 14:20 )
Design and verification of Single Event Latch-up mitigation circuits for On-board Computer subsystem of HORYU-IV satellite
Mohamed Yahia Edries1, Atomu Tanaka2, Hiroshi Fukuda3, Koyo Taniwaki2, HORYU-IV Team2, Hirokazu Masui2, Koichi Takamiya4, Mengu Cho2
1National Authority for Remote Sensing and Space Sciences (NARSS), Space Sciences and Strategic Studies Division, Egypt, Egypt, 2Kyushu Institue of Technology, Departmet of Applied Science for Integrated Systems Engineering, Japan, 3Kyushu Institue of Technology, Departmet of Electrical Engineering, Japan, 4Kyoto University Research Reactor Institute, Japan
2017-f-011 ( 14:20 – 14:40 )
System Design of Multi-purpose Space Environment Utilization Experiment Satellite “TeikyoSat-4”
Yonosuke Yamazaki, Masaaki Kawamura
Departmemt of Aerospace engineering, Teikyo Univirsity, Japan
2017-f-012 ( 14:40 – 15:00 )
CuPA – A Turnkey CubeSat Solution for Precision Agriculture in Indian Sub-Continent
Siddhesh Ravindra Naik, Siddhesh Naik
YGNSS Co-Lead, Space Generation Advisory Council, India
2017-f-013 ( 15:00 – 15:20 )
Technology Demonstration Microsatellite “Hibari”: Variable Shape Attitude Control and Its Application to Astrometry of Gravitational Wave Sources
Kyosuke Tawara1, Shohei Harita3, Yoichi Yatsu3, Saburo Matunaga2
1Department of Mechanical and Aerospace Engineering, Tokyo Institute of Technology, Japan, 2Department of Mechanical Engineering, Tokyo Institute of Technology, 3Department of Physics, Tokyo Institute of Technology
2017-f-014 ( 15:20 – 15:40 )
UNISEC-Global Challenge: An approach for contribution to Debris Mitigation – Deorbit Device Competition
Rei Kawashima
UNISEC-Global , Japan
[f-4] BIRDS

Session Date June 6 (Tue) 16:00 – 17:40
Room Pearl Room A
Chairpersons
2017-f-015 ( 16:00 – 16:20 )
Overview of the Joint Global Multi-Nation Birds Satellite Project
Taiwo Raphael Tejumola, BIRDS Project Members, BIRDS Partners, George Maeda, Sangkyun Kim, Hirokazu Mazui, Mengu Cho
Laboratory of Spacecraft Environment Interaction Engineering, Kyushu Institute of Technology, Japan
2017-f-016 ( 16:20 – 16:40 )
Design, Manufacture and Verification of CubeSat Structure for BIRDS Constellation
Ibukun Oluwatobi Adebolu, BIRDS Project Members, BIRDS Partners, George Maeda, Sangkyun Kim, Hirokazu Masui, Mengu Cho
Laboratory of Space Environment interaction Engineering, Kyushu Institute of Technology, Japan
2017-f-017 ( 16:40 – 17:00 )
Design and Verification of BIRDS Project Mission Data Downlink System
Maisun Ibn Monowar1, George Maeda1, Sangkyun Kim1, Hirokazu Masui1, Mengu Cho1, Kaname Kojima2, BIRDS Project Members1, BIRDS Partners1
1Laboratory of Spacecraft Environment Interaction Engineering, Kyushu Institute of Technology, Japan, 2Addnics Corp.
2017-f-018 ( 17:00 – 17:20 )
Challenges in the development of the backplane-type bus for 1U CubeSat
Yasuhiro Tokunaga1, Mengu Cho1, Turtogtokh TUMENJARGAL1, Erdenebaatar Dashdondog1, Ibukun Oluwatobi Adebolu1, George Maeda1, Sangkyun Kim1, Hirokazu Masui1, Takeyuki Handa2, Shinichi Yoshida2
1Department of Applied Science for Integrated System Engineering, Kyusyu Institute of Technology, Japan, 2Sagamitsushin Co.
2017-f-019 ( 17:20 – 17:40 )
Atmospheric Density Modelling via Precise Satellite Tracking of Birds CubeSat constellation
Joseph Neenyi Kojo Krobo Quansah, BIRDS Project Members, BIRDS Partners, George Maeda, Sangkyun Kim, Hirokazu Masui, Mengu Cho
Applied Science for Integrated System Engineering-Laboratory of Spacecraft Environment Interaction Engineering, Kyushu Institute of Technology, Japan
[f-5] Re-entry & Deployment

Session Date June 7 (Wed) 9:00 – 10:20
Room Pearl Room A
Chairpersons
2017-f-021 ( 9:00 – 9:20 )
Re-entry Nano-Satellite with Gossamer Aeroshell and GPS/Iridium deployed from ISS
Kazuhiko Yamada1, Takahiro Moriyoshi2, Kazushige Matsumaru3, Hiroki Kanemaru2, Takahiro Araya4, Kojiro Suzuki5, Osamu Imamura3, Daisuke Akita6, Yasunori Nagata7, Yasuhiro Shoji8, Yusuke Takahashi9, Yasumasa Watanabe5, Takashi Abe1
1Institute of Space and Astronautical Science, Japan Aerospace Exploration Agensy, Japan, 2Tokyo University of Agriculture and Technology, 3Nihon University, 4Tokyo University of Science, 5The University of Tokyo, 6Tokyo Institute of Technology, 7Okayama University, 8Osaka University, 9Hokkaido University
2017-f-022 ( 9:20 – 9:40 )
SIMON, an Electric Propulsion CubeSat Test Bed for CAPE
Daniel Andre Galla
KSat e.V., University of Stuttgart, Germany
2017-f-023 ( 9:40 – 10:00 )
Development of CubeSat OrigamiSat-1 for Space Demonstration of Deployable Membrane Structure Technologies
Hiraku Sakamoto1, Hiroki Nakanishi1, Masahiko Yamazaki2, Yasuyuki Myazaki2, Hiroshi Furuya1, Mitsushige Oda1, Akihito Watanabe3, Kazuki Watanabe4, Ayako Torisaka Kayaba5
1Tokyo Institute of Technology, Japan, Japan, 2Nihon University, Japan, 3Sakase Adtech, Japan, 4WEL Research, Japan, 5Tokyo Metropolitan University, Japan
2017-f-024 ( 10:00 – 10:20 )
Development of Internal Antenna Deployment Mechanism for a CubeSat
Raihana Shams Islam Antara, BIRDS Project Members, BIRDS Partners, George MAEDA, Sangkyun KIM, Hirokazu Masui, Mengu CHO
Laboratory of Spacecraft Environment Interaction Engineering Kyushu Institute of Technology, Kitakyushu, Japan., Japan
[f-6] Constellations

Session Date June 7 (Wed) 11:00 – 12:40
Room Pearl Room A
Chairpersons
2017-f-025 ( 11:00 – 11:20 )
Innovative Approach to Data Gathering in Remote Areas Using Constellations of Store & Forward Communication Cubesats
Quentin Verspieren, Toshihiro Obata, Shinichi Nakasuka
Intelligent Space Systems Laboratory, The University of Tokyo, Japan
2017-f-026 ( 11:20 – 11:40 )
Need of Small satellite constellation to study Ionosphere precursor due to earthquake
Koichiro Oyama
Institute of Space and Plasma Sciences, National Cheng Kung University, Taiwan
2017-f-027 ( 11:40 – 12:00 )
CUBESAT CONSTELLATION SYSTEM FOR AGRICULTURE APPLICATION IN INDIA
MUHAMMAD SHADAB KHAN, ZAINAB SIDDIQUI
Space Generation Advisory Council, India
2017-f-028 ( 12:00 – 12:20 )
Feasibility analysis of fractioned cubesats formation for Moon observations
Diogene Alessandro Dei Tos, Daniele Filippetto, Aureliano Rivolta
Department of Aerospace Science and Technology, Politecnico di Milano, Italy
2017-f-029 ( 12:20 – 12:40 )
The DLR Small-Satellite Constellation FireBIRD
Winfried Halle
Institut of Optical Sensor System , DLR, Germany
[f-7] STARS-E

Session Date June 7 (Wed) 16:00 – 17:20
Room Pearl Room A
Chairpersons
2017-f-030 ( 16:00 – 16:20 )
Velocity control applied to tether reel mounted on STARS-E
atsushi bito, masahiro nohmi
Department of engineering, University of Shizuoka, Japan
2017-f-031 ( 16:20 – 16:40 )
Attitude Control Method with RW and Magnetic Torque for Orbital Elevator Satellite STARS-E
Keisuke Takaya, Masahiro Nohmi
Department of engineering, University of Shizuoka, Japan
2017-f-032 ( 16:40 – 17:00 )
Design of the Communication Antenna for the STARS-E Climber
Tomohiro Kakuta
Department of precision Machinery Engineering, Nihon University, Japan
2017-f-033 ( 17:00 – 17:20 )
A Study of the STARS-E Climber’s EPS and Electrical Components for Mission Success
Darren Raymond Coste
Department of Precision Machinery Engineering, University of Nihon, Japan
[f-8] Infrastructure

Session Date June 8 (Thu) 9:00 – 10:20
Room Pearl Room A
Chairpersons
2017-f-034 ( 9:00 – 9:20 )
Integrated Ground Network Technologies – KSAT Lite Small Antenna Network
Kenneth Olafsson, Martin Krynitz
Satellite Operations, KSAT – Kongsberg Satellite Services AS, Norway
2017-f-035 ( 9:20 – 9:40 )
Advantages of a Cubesat Receiving Station located in the south of the Indian Ocean
Vincent Dinnat
Lycee Bois d’Olives, Reunion
2017-f-036 ( 9:40 – 10:00 )
Advanced Small Satellites Launch Options Research
Elena Valerevna Petrakova, Valery Petrovich Panasenkov
Aerospace Engineering, Moscow Aviation Institute (National Research University), Russia
2017-f-037 ( 10:00 – 10:20 )
Aggregated Preference Value Analysis on Small Satellite Launch Opportunities
Mengying Zhang, Qin Xu
School of MACE, The University of Manchester, UK
[f-9] Beyond Earth

Session Date June 8 (Thu) 11:00 – 12:40
Room Pearl Room A
Chairpersons
2017-f-038 ( 11:00 – 11:20 )
Thinking outside the “Cube”
Alex da Silva Curiel, Nikki Jahn, Anita Bernie, Luis Gomes, Martin Sweeting
Surrey Satellite Technology Ltd., UK
2017-f-039 ( 11:20 – 11:40 )
Making Small Lunar Missions Viable
Alex da Silva Curiel1, Jonathan Friend1, Chris Saunders1, Susan Jason1, Martin Sweeting1, Matt Cosby2, Berhard Hufenbach3, James Carpenter3, Richard Fisackerly3
1Surrey Satellite Technology Ltd., UK, 2Goonhilly Earth Station Ltd., 3European Space Agency
2017-f-040 ( 11:40 – 12:00 )
Spacecraft In The Shot
Jessie M Kawata, Jonathon Joseph Smith
NASA Jet Propulsion Laboratory / Caltech , USA
2017-f-041 ( 12:00 – 12:20 )
A CubeSat Project to Observe the Beaming Structures of Jupiter’s Radio Emissions
Lkhagvadorj Sukhtsoodol1, Yusei Nakayama1, Ryunosuke Fujita1, Mizuki Ando2, Kai Chiang Eric Tan2, Kazumasa Imai1, Nobuto Hirakoso2, Taku Takada1, Kentarou Kitamura3
1Electrical Engineering and Information Science, National Institute of Technology, Kochi College, Japan, 2National Institute of Technology, Gunma College, 3National Institute of Technology, Tokuyama College
2017-f-042 ( 12:20 – 12:40 )
Development of Binary Black Hole Observation Satellite ‘‘ORBIS’’
Jun Matsushima1, Shogo Asano1, Masahiro Kaku1, Toshihiro Kanda1, Mayu Banno1, Hirohisa Asano1, Yuya Kobayashi1, Natsumi Kimura1, Norio Yamashita1, Yuichiro Ezoe2, Kumi Ishikawa3, Masaki Numazawa2, Kazuma Takeuchi2, Masaru Terada2, Daiki Ishi2, Yusuke Noda2, Maiko Fujitani2, Naoki Isobe4, Hiroshi Nakajima5, Norihide Miyamura6
1Department of Aerospace Engineering, Tokyo Metropolitan University, Japan, 2Department of Physics, Tokyo Metropolitan University, 3Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 4School of Science, Tokyo Institute of Technology, 5Graduate School of Science, Osaka University, 6Department of Interdisciplinary Science and Engineering, Meisei University
[f-10] EQUULEUS

Session Date June 8 (Thu) 14:00 – 15:40
Room Pearl Room A
Chairpersons
2017-f-043 ( 14:00 – 14:20 )
Mission to Earth-Moon Lagrange Point by a 6U CubeSat: EQUULEUS
Ryu Funase1, Naoya Ozaki1, Shintaro Nakajima1, Kenshiro Oguri1, Kota Miyoshi2, Stefano Campagnola2, Hiroyuki Koizumi1, Yuta Kobayashi2, Taichi Ito2, Takumi Kudo1, Yuki Koshiro1, Shunichiro Nomura1, Akifumi Wachi1, Masashi Tomooka1, Ichiro Yoshikawa1, Hajime Yano2, Shinsuke Abe3, Tatsuaki Hashimoto2, EQUULEUS Project Team1
1The University of Tokyo, Japan, 2Japan Aerospace Exploration Agency, 3Nihon University
2017-f-044 ( 14:20 – 14:40 )
Mission Analysis for EQUULEUS and OMOTENASHI
Stefano Campagnola1, Naoya Ozaki2, Javier Hernando1, Kenta Oshima1, Tomohiro Yamaguchi1, Toshinori Ikenaga3, Chit Hong Yam1, Kenshiro Oguri2, kota kakihara2, shota takahashi1, yusuke ozawa1, luca ferella1, ryu funase2, tatsuaki hashimoto1
1Department of Space Flight Systems, JAXA/ISAS, Japan, 2Intelligent Space Systems Laboratory, The University of Tokyo, 3Research and Development Directorate, Tsukuba, JAXA
2017-f-045 ( 14:40 – 15:00 )
Fundamental Ground Experiment of a Water Resistojet Propulsion System: AQUARIUS Installed on a 6U CubeSat: EQUULEUS
Jun Asakawa1, Hiroyuki Koizumi1, Naoki Takeda2, Keita Nishii2, Masaya Murohara1, Ryu Funase1, Kimiya Komurasaki1
1Department of Aeronautics and Astronautics, The University of Tokyo, Japan, 2Department of Advanced Energy, The University of Tokyo
2017-f-046 ( 15:00 – 15:20 )
Initial Design of EQUULEUS Attitude Determination and Control System: How to Design an ADCS with High Reliability for a Deep Space CubeSat
Shunichiro Nomura, Ryohei Takahashi, Mikihiro Ikura, Kenshiro Oguri, Toshihiro Obata, Satoshi Ikari, Ryu Funase
Department of Aeronautics and Astronautics, University of Tokyo, Japan
2017-f-047 ( 15:20 – 15:40 )
Thermal Design and Analysis for a 6U Deep Space CubeSat EQUULEUS under Tightly-Coupled Spacecraft Resource Constraints
Yuki Koshiro, Naoya Ozaki, Akihiro Ishikawa, Ryu Funase
Department of Aeronautics and Astronautics, The University of Tokyo, Japan
[f-11] Components

Session Date June 8 (Thu) 14:00 – 15:40
Room Meeting Room 7
Chairpersons
2017-f-048 ( 14:00 – 14:20 )
Development of Ceramic BGA Package for Space-use
Koichi Shinozaki1, Toshiyuki Yamada1, Noriko Yamada1, Koichi Suzuki1, Masao Nakamura2, Yoshihiro Tokue3
1Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA), Japan, 2Nippon Avionics Co., Ltd., 3Avionics Fukushima Co., Ltd.
2017-f-049 ( 14:20 – 14:40 )
One-chip plasma wave observation system
Takahiro Zushi1, Hirotsugu Kojima1, Yoshiya Kasahara2, Tsubasa Takahashi2, Mitsunori Ozaki2, Satoshi Yagitani2, Yuya Tokunaga2
1Kyoto University, Japan, 2Kanazawa University
2017-f-050 ( 14:40 – 15:00 )
A Sensor Package for Space Weather Global Monitoring Based on Micro Satellite Constellation
Tsutomu Nagatsuma1, Atsushi Kumamoto2, Mitsunori Ozaki3, Kentarou Kitamura4, Yoshifumi Saito5, Takeshi Takashima5, Masahito Nose6, Jun-ichi Kurihara7, Hirotsugu Kojima8, Keigo Ishizaka9, Ayako Matsuoka5, Reiko Nomura5, Tetsuro Ishida7, Yukihiro Takahashi7
1Space Environment Laboratory, Applied Electromagnetic Research Institute, National Institute of Information and Communications Technology, Japan, 2Graduate School of Science, Tohoku University, 3Faculty of Electrical and Computer Engineering, Institute of Science and Engineering, Kanazawa Univeristy, 4Tokuyama College of Technology, 5Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 6Graduate School of Science, Kyoto University, 7Graduate School of Science, Hokkaido University, 8Research Institute for Sustainable Humanosphere, Kyoto University, 9Faculty of Engineering, Toyama Prefectural University
2017-f-051 ( 15:00 – 15:20 )
Compact and Light-weight X-ray Telescope for the ORBIS Microsatellite Mission
Kumi Ishikawa1, Yuichiro Ezoe2, Kazuma Takeuchi2, Masaru Terada2, Kasumi Nakamura2, Masaki Numazawa2, Maiko Fujitani2, Daiki Ishi2, Kazuhisa Mitsuda1
1ISAS/JAXA, Japan, 2Tokyo Metropolitan University
2017-f-052 ( 15:20 – 15:40 )
First High Resolution High Speed CubeSat of Turkey
alim rustem aslan1, ALIME YANARTAS YILDIRIM2, MURAT SUER3, ERDINC YAKUT3, BOGAC KARABULUT1, MUSTAFA ERDEM BAS4, MEHMET SEVKET ULUDAG1, MUSTAFA KARATAS1, OZGUN SARI2, SIBEL TURKOGLU1, ENES ERDOGAN3, CANSU CENIK1, ALIM ASLAN5
1ISTANBUL TECHNICAL UNIVERSITY Faculty of Aeronautics and Astronautics Dept. of Astronautical Eng , Turkey, 2ASELSAN Co ANKARA TURKEY, 3GUMUSH SPACE LTD ISTANBUL TURKEY, 4ERTEK SPACE LTD ISTANBUL TURKEY, 5AMSAT-TR TURKEY
[f-12] Lunar & Deep Space Missions

Session Date June 8 (Thu) 16:00 – 18:00
Room Pearl Room A
Chairpersons
2017-f-053 ( 16:00 – 16:20 )
Nano Moon Lander: OMOTENASHI
Tatsuaki Hashimoto, Tetsuya Yamada, Junji Kikkuchi, Masatsugu Otsuki, Toshinori Ikenaga
Japan Aerospace Exploration Agency, Japan
2017-f-054 ( 16:20 – 16:40 )
OMOTENASHI Trajectory Analysis and Design: Earth-Moon Transfer Phase
Yusuke Ozawa1, Shota Takahashi2, Javier Hernand Ayuso3, Stefano Campagnola4, Toshinori Ikenaga4, Tomohiro Yamaguchi4, Bruno Sarli4
1University of Tokyo, Graduate School of Frontier Science, Department of Advanced Energy, Japan, 2Keio University, Faculty of Science and Technology, Department of Mechanical Engineering, 3University of Tokyo, Graduate School of Engeeniring, Department of Aeronautics and Astonautics, 4JAXA
2017-f-055 ( 16:40 – 17:00 )
Development of Crushable Shock Absorption Structure for OMOTENASHI Semi-hard Impact Probe
Tetsuya Yamada1, Hideyuki Tanno2, Tatsuaki Hashimoto1
1ISAS/JAXA, Japan, 2JAXA
2017-f-056 ( 17:00 – 17:20 )
Attitude Control System for Small and Micro Class Spacecrafts on Deep-Space and Lunar Missions
Amin Ali Mody
Department of Aerospace Engineering, SRM University, India
2017-f-057 ( 17:20 – 17:40 )
An Investigation On Feasibility Of Interplanetary Magnetic Attitude Control For Nanosatellites
Tushar Sharma
Electrical and Electronics Engineering, SRM University, Chennai, India
2017-f-058 ( 17:40 – 18:00 )
Comparative Analysis of Control Moment Gyros and Reaction Wheels for Micro-class Low Lunar Orbiters
Tushar Sharma
Electrical and Electronics Engineering, SRM University, Chennai, India
[f-13] Thruster

Session Date June 8 (Thu) 16:00 – 17:40
Room Meeting Room 7
Chairpersons
2017-f-059 ( 16:00 – 16:20 )
Qualification Model Development of CubeSat RF lon Propulsion System “BIT-3”
Michael Tsay, John Frongillo, Jurg Zwahlen, Joshua Model
Electrothermal Propulsion Group, Busek Co. Inc., USA
2017-f-060 ( 16:20 – 16:40 )
The HDCGJ – A Cold Gas Propulsion System for Delivering Continuous Thrusting to Small Satellites via Supercritical Evaporation
Ralf C. Boden1, Ryota Koyama1, Hiroshi Igoh2, Shunichi Okaya2, Jun’ichiro Kawaguchi2
1Department of Aeronautics and Astronautics, The University of Tokyo, Japan, 2Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
2017-f-061 ( 16:40 – 17:00 )
Design and Verification of Ultrasonic Motor Based Single-Axis Attitude Control System for Nano-Satellites
xun sun, Yijun Huang, Xiaofeng Wu
AMME, the University of Sydney, Australia
2017-f-062 ( 17:00 – 17:20 )
Research and Development of the Osaka Institute of Technology 2nd PROITERES Nano-Satellite with High-Power Pulsed Plasma Thrusters for Powered Flight
Ryuta Yagi1, Tsubasa Yamauchi1, Hiroki Fujita1, Kaisei Kajihara1, Hirokazu Tahara1, Kyoko Takada1, Tomoyuki Ikeda2
1Department of Mechanical Engineering, Osaka Institute of Technology, Japan, 2Tokai University
2017-f-063 ( 17:20 – 17:40 )
Thrust Regulation for a Tethered Space-Tug based on the Rigid-Flexible Coupling Multibody Model
Rui Zhong, Shijie Xu
School of Astronautics, Beihang University, China
[f-14] Attitude Determination

Session Date June 9 (Fri) 9:00 – 10:40
Room Pearl Room A
Chairpersons
2017-f-064 ( 9:00 – 9:20 )
An Algorithm for Automation of Attitude Determination and Control Process of A Low Earth Orbit NanoSatellite
Sibel Turkoglu, Alim Rustem Aslan
Faculty of Aeronautics and Astronautics, Istanbul Technical University, Turkey
2017-f-065 ( 9:20 – 9:40 )
Pseudo-Linear Kalman Filter for Spinning Nanosatellite Attitude Estimation
Halil Ersin Soken1, Osama Khurshid2, Jorma Selkäinaho2, Esa Kallio2, Arto Visala2
1Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan, 2Aalto University
2017-f-066 ( 9:40 – 10:00 )
Design and Implementation of an Attitude Determination Module with Real-Time Sensor Calibration for Small-Satellite Systems including performance Verification using DIWATA-1 Flight Data
Ariston Nicolas Gonzalez, Yuji Sakamoto, John Leur Labrador, Kazuya Yoshida, Toshinori Kuwahara
Department of Aerospace Engineering, Tohoku University, Japan
2017-f-067 ( 10:00 – 10:20 )
Orbit and Attitude Determination for a LEO Satellite via TAM and Rate-Gyro Measurements
Murat BAGCI
Department of Space Sciences , Turkish Air Force Academy, Turkey
2017-f-068 ( 10:20 – 10:40 )
A sun vector determination with use of insufficient data from sensors
Dmytro Faizullin1, Koju Hiraki1, Mengu Cho2
1Kyushu Institute of Technology, Mechanical engineering, Japan, 2Kyushu Institute of Technology, Applied Science for Integrated System Engineering
[f-15] Design

Session Date June 9 (Fri) 9:00 – 10:20
Room Meeting Room 1
Chairpersons
2017-f-069 ( 9:00 – 9:20 )
Application of Design Structure Matrix (DSM) for Nano-satellite Systems Design and Management
Mohammed Khalil Ibrahim, Yasuyuki Miyazaki
Aerospace Engineering Department, College of Science and Technology, Nihon University, Japan
2017-f-070 ( 9:20 – 9:40 )
A System Engineering Approach to The Harness Routing Process of Microsatellites
Manh Duc Nguyen
Graduate School of System Design and Management, Keio University, Japan
2017-f-071 ( 9:40 – 10:00 )
An Adaptive Framework for Fault Detection, Isolation and Recovery Design of Micro Satellite Bus System by Considering Whole Life Cycle of Satellite Development
Minh Anh Pham
System Design and Management , Keio University, Japan
2017-f-073 ( 10:00 – 10:20 )
Thermal Design of Micro- and Nano- satellites in Non-sun-synchronous Orbit
Delburg Panes Mitchao1, Tsuyoshi Totani2, Masashi Wakita2, Harunori Nagata2
1Graduate School of Engineering, Hokkaido University, Sapporo, Hokkaido, 060-8628 Japan, Japan, 2Faculty of Engineering, Hokkaido University, Sapporo, Hokkaido, 060-8628 Japan
[f-16] Disturbance and Utilization

Session Date June 9 (Fri) 11:00 – 12:20
Room Pearl Room A
Chairpersons
2017-f-074 ( 11:00 – 11:20 )
Observer-based Disturbance Estimation for a Small Satellite Inertial Pointing using Magnetic Torquers
Jongbum Kim, Hyochoong Bang
Department of aerospace engineering, Korea Advanced Institute of Science and Technology, Korea
2017-f-075 ( 11:20 – 11:40 )
Vibration suppression for a deep-space microsatellite during attitude and orbital maneuvers
Amin Ali Mody
Department of Aerospace Engineering, SRM University, India
2017-f-076 ( 11:40 – 12:00 )
Magnetic torque caused by shape magnetic anisotropy in nano-satellites
Takaya Inamori1, Mana Nagao1, Yutaka Terao2, Nobutada Sako3
1Department of space engneering, Nagoya University, Japan, 2Tokyo University, 3Canon Electronics Inc.
2017-f-077 ( 12:00 – 12:20 )
Detailed Analysis of Aerodynamic Effect on Small Satellites
Kikuko Miyata1, Rei Kawasima2, Takaya Inamori1
1Department of Aerospace Engineering, Nagoya University, Japan, 2Department of Aeronautics and Astronautics, University of Tokyo
[f-17] Test

Session Date June 9 (Fri) 11:00 – 12:40
Room Meeting Room 1
Chairpersons
2017-f-078 ( 11:00 – 11:20 )
The development of support system for Radiation Resistance Test
Akihiro Nagata1, Atsushi Yasuda2, Hiromasa Watanabe2, Toshihiro Kameda3
1College of Engineering Systems, University of Tsukuba, Japan, 2College of Physics, University of Tsukuba, 3Institute of Engineering Mechanics and Energy, University of Tsukuba
2017-f-079 ( 11:20 – 11:40 )
Evaluation of Structural Thermal Model of a Small Spacecraft Using CFRP
yutaro ogata, takumi iso, masaaki kawamura
University of Teikyo , Japan
2017-f-080 ( 11:40 – 12:00 )
Development of thermal vacuum testing method for multiple Nano satellites
Naoki Nakamura, BIRDS Project Members, BIRDS Partners, George Maeda, Sangkyun Kim, Hirokazu Masui, Mengu Cho
Department of Applied Science for Integrated System Engineering, Kyushu institute of technology, Japan
2017-f-081 ( 12:00 – 12:20 )
Development of Structural Thermal Model of Multipurpose Space Environmet Utilization Satellite “TeikyoSat-4”
takumi iso, masaaki kawamura
Department of aerospace engineering, University of Teikyo, Japan
2017-f-082 ( 12:20 – 12:40 )
Design, Development and Testing of Structure and Thermal subsystem of AOBA-VELOX III
Hirokazu Masui1, Kyutech Satellite project project2, Mengu Cho1
1Laboratory of Spacecraft Environment Interaction Engineering , Kyushu Institute of Technology, Japan, 2Kyushu Institute of Technology
[f-18] Attitude Control

Session Date June 9 (Fri) 14:00 – 15:40
Room Pearl Room A
Chairpersons
2017-f-083 ( 14:00 – 14:20 )
Three-axis Active and Fully Magnetic Attitude Control Design for a 1/3U Picosat Platform
Andrea Colagrossi1, Lorenzo Bucci1, Michèle Lavagna1, Guido Parissenti2
1Department of Aerospace Science and Technology, Politecnico di Milano, Italy, 2GP Advanced Projects Srls
2017-f-084 ( 14:20 – 14:40 )
Attitude control for a nanosatellite using only magnetic torquers
Takashi Kimoto, Yasuhiro Shoji, Katsuhiko Yamada
Graduate School of Engineering, Osaka University, Japan
2017-f-085 ( 14:40 – 15:00 )
Active Aerodynamic Pitch Control for Earth Observation Missions in Very Low Earth Orbits
Zhou Hao, Peter C.E. Roberts
School of Mechanical, Aerospace and Civil Engineering, Faculty of Science and Engineering, The University of Manchester, UK
2017-f-086 ( 15:00 – 15:20 )
A Fluid-Dynamic Attitude Control System for TechnoSat
Daniel Noack1, Jonathan Ludwig2, Klaus Brieß1
1Institute of Aeronautics and Astronautics, Technical University of Berlin, Germany, 2Magson GmbH
2017-f-087 ( 15:20 – 15:40 )
Dynamics Analysis of Passive Attitude Control Using Solar Pressure for Micro / Nano Satellites
Hiroki Nakanishi, Ryuhei Takagi, Tsubasa Tsunemitsu, Mitsushige Oda
Department of Mechanical Engineering, Tokyo Institute of Technology, Japan
[f-19] Operation & Verification

Session Date June 9 (Fri) 14:00 – 15:40
Room Meeting Room 1
Chairpersons
2017-f-088 ( 14:00 – 14:20 )
VELOX-II: Summary of One Year in Operation
Shu Ting Goh1, Lip San Lim1, Tran Duy Vu Bui1, Mihindukulasooriya Sheral Crescent Tissera1, Van Hong Phuc Pham1, Rai Abhishek1, Jing Jun Soon1, Jia Min Lew1, Htet Aung1, Guo Xiong Lee1, Jiun Wei Chia1, Kah Wai Chow1, Srivastava Ankit1, Li Deng1, Kay-Soon Low2
1School of Electrical and Electronic Engineering, Nanyang Technological University, Singapore, 2Department of Electrical and Computer Engineering, National University of Singapore
2017-f-089 ( 14:20 – 14:40 )
Development and Flight Operations of Microsatellite Bus System for DIWATA-1
Yuji Sakamoto1, Ariston Gonzalez1, John Leur Labrador1, Gerwin Policarpio Guba1, Harold Bryan Solano Paler1, Toshinori Kuwahara1, Kazuya Yoshida1, Tetsuro Ishida2, Junichi Kurihara2, Yukihiro Takahashi2
1Department of Aerospace Engineering, Tohoku University, Japan, 2Department of Cosmosciences, Hokkaido University
2017-f-090 ( 14:40 – 15:00 )
STARS-C Tether Deployment Mission and Quick Report of Operation Results
Takeru Kumao, Masanori Aiga, Masahito Watahiki, Masahiro Nohmi, Yoshiki Yamagiwa
Department of Engineering, Shizuoka University, Japan
2017-f-091 ( 15:00 – 15:20 )
Orbit Verification Result of De-orbit Mechanism Demonstration CubeSat FREEDOM
Hiroki Uto
Nakashimada Engineering Works, Ltd., Japan
2017-f-092 ( 15:20 – 15:40 )
System Verification of a S-Band Network of Distributed Nanosatellites
Zizung Yoon, Walter Frese, Huu Quan Vu, Klaus Briess
Institute of Aeronautics and Astronautics, Technische Universitaet Berlin, Germany
[f-20] Sensor and Actuator for Attitude Control

Session Date June 9 (Fri) 16:00 – 17:40
Room Pearl Room A
Chairpersons
2017-f-093 ( 16:00 – 16:20 )
Fault Tolerant Circuit Design for Low-cost and Multi-Functional Attitude Sensor Using Real-time Image Recognition
Yuhei Kikuya1, Masanori Matsushita2, Masaya Koga2, Kei Ohta2, Yuki Hayashi1, Takehiko Koike2, Toshiki Ozawa3, Yoichi Yatsu3, Saburo Matunaga1
1Department of Mechanical Engineering, Tokyo institute of technology, Japan, 2Department of Mechanical and Aerospace Engineering, Tokyo Institute of Technology, 3Department of Physics, Tokyo Institute of Technology
2017-f-094 ( 16:20 – 16:40 )
Design and construction of a reaction wheels assembly for the Attitude Control System of nanosatellites 3U CubeSat.
Diego F. Martinez
Departament of Electrical Engineering, National Autonomous University of Mexico, Mexico
2017-f-095 ( 16:40 – 17:00 )
Investigation into Star Tracker Algorithms with Application to High-Precision CubeSats
Joshua Julian Robert Critchley-Marrows, Xiaofeng Wu
School of Aerospace, Mechanical and Mechatronic Engineering, University of Sydney, Australia
2017-f-096 ( 17:00 – 17:20 )
Design of Magnetic Actuators and Testbench for Control Attitude System for 3U Nanosatellite
Daniel Alejandro Angulo Angeles
Engineering School, National Autonomous University of Mexico, Mexico
2017-f-097 ( 17:20 – 17:40 )
Star tracker in the loop test bench for microsatellite AOCS design and validation
Hao-Chi Chang1, Yu-Yung Lian1, Kuo-Liang Wu2, Hung-Yuan Chang2, Chen-Tsung Lin2
1Navigation Sensors Subsystem Department, Flight Control Division, National Space Organization, Taiwan, 2Components and Flight Test Department, Flight Control Division, National Space Organization
[f-21] Evaluation Software

Session Date June 9 (Fri) 16:00 – 17:40
Room Meeting Room 1
Chairpersons
2017-f-098 ( 16:00 – 16:20 )
Static Closed Loop Simulation for Ground-Target Tracking Control of Microsatellite “RISESAT”
Shinya Fujita, Yuji Sato, Toshinori Kuwahara, Yuji Sakamoto, Kazuya Yoshida
department of aerospace engineering, tohoku university, Japan
2017-f-099 ( 16:20 – 16:40 )
Development of an Improved Micro-satellite Simulator Environment for Attitude Determination and Control System Verification through DIWATA-1 Flight Data Analysis
John Leur Delos Santos Labrador, Ariston Nicolas Gonzalez, Yuji Sakamoto, Toshinori Kuwahara, Kazuya Yoshida
Department of Aerospace Engineering, Tohoku University, Japan
2017-f-100 ( 16:40 – 17:00 )
Software Development for Galassia CubeSat – Design Implementation and In-Orbit Validation
Hassan Ali Askari, Han Ee Wei, Ajie Nayaka Nikicio, Cher Hiang Goh, Sha Luo, Hwee Choo Liaw
Electrical and Computer Engineering, National University of Singapore, Singapore
2017-f-101 ( 17:00 – 17:20 )
Modelling and Simulation of Hardware Components to Facilitate Lean Development of Nanosatellites
Jyh-Ching Juang, Yun-Peng Tsai
Department of Electrical Engineering, National Cheng Kung University, Taiwan
2017-f-102 ( 17:20 – 17:40 )
Development and Ground Evaluation of Fast Tracking Algorithm for Star Trackers
Yuji Sato, Toshinori Kuwahara, Shinya Fujita, Yuji Sakamoto, Kazuya Yoshida
Department of Aerospace Engineering, Tohoku University, Sendai, Japan, Japan
[g-1] Space Transportation (1)

Session Date June 7 (Wed) 11:00 – 12:20
Room Meeting Room 7
Chairpersons
2017-g-01 ( 11:00 – 11:20 )
Aerodynamics Caused by Rolling Rates of a Small-scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology
Kazuhide Mizobata1, Yukiya Ishigami1, Masaaki Miura1, Kazuyuki Higashino1, Takakage Arai2
1Aerospace Plane Research Center, Muroran Institute of Technology, Japan, 2Osaka Prefecture University
2017-g-02 ( 11:20 – 11:40 )
Drag Reduction on the Basis of the Area Rule of the Small-scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology
Yuki Yamazaki, Kazuhide Mizobata, Kazuyuki Higashino
Aerospace Plane Research Center, National University Corporation Muroran Institute of Technology, Japan
2017-g-03 ( 11:40 – 12:00 )
Aerodynamic Derivatives with respect to pitching and yawing rates of a Small-scale Supersonic Flight Experiment Vehicle
Keisuke Shiono1, Koji Shirakata1, Yukiya Ishigami1, Masaaki Miura1, Kazuhide Mizobata1, Kazuyuki Higashino1, Takakage Arai2
1Aerospace Plane Research Center, National University Corporation Muroran Institute of Technology, Japan, 2Osaka Prefecture University
2017-g-04 ( 12:00 – 12:20 )
Design and Experiment of Guidance and Control System for Autonomous Flight toward a Small-scale Unmanned Supersonic Airplane
Masazumi Ueba, Yuuichi Takaku, Kouhei Takahashi, Tomohiro Kamata
Muroran Institute of Technology, Japan
[g-2] Space Transportation (2)

Session Date June 7 (Wed) 16:00 – 17:00
Room Meeting Room 7
Chairpersons
2017-g-06 ( 16:00 – 16:20 )
Reusable Launch Vehicle-Concept of Minimizing Space Transportation Cost
Nadeem Alam
Department of Aeronautical Engineering, Babu Banarasi Das National Institute of Technology and Management , India
2017-g-07 ( 16:20 – 16:40 )
Load Alleviation of of Launch Vehicle Flight Using Angle of Attack Estimator
Widyoutomo Birmiawan Ario1, Yasuhiro Morita2
1Department of Space and Astronautical Science, The Graduate University for Advanced Studies, Japan, 2Japan Aerospace Exploration Agency
2017-g-09 ( 16:40 – 17:00 )
Earth-Venus Express (EVE) Concept: A Transportation Strategy for Project GIVE (Grown in Venus Enclosure)
Huai-Chien Chang1, Akira Tsuchida2
1Consortium of Spacce Settlements, Astronautical Society of Taiwan., Taiwan, 2Vice Chair of IAA Commission IV, Space Systems Operations & Utilization, Member of IAA (International Academy of Astronautics)
[g-3] Space Transportation (3)

Session Date June 8 (Thu) 9:00 – 10:40
Room Meeting Room 14
Chairpersons
2017-g-10 ( 9:00 – 9:20 )
Analysis of Orbital Transfer between the Earth – Mars Orbit using Electric Propulsion based on Direct Collocation Method
Akihito Toba
Department of Engineering, Shizuoka University, Japan
2017-g-11 ( 9:20 – 9:40 )
Current Research and Development activities in the field of Atmospheric Entry at IRS
Georg Herdrich, Bartomeu Massuti-Ballester, Adam Pagan, Stefanos Fasoulas
Institute of Space Systems (IRS), University of Stuttgart, Germany
2017-g-12 ( 9:40 – 10:00 )
Evaluation study on EDL analysis in Mars atmosphere re-entry with high-lift flexible vehicle
Mayuri Sakamoto, Riho Takumi, Masaaki Kawamura
Teikyo University, Japan
2017-g-13 ( 10:00 – 10:20 )
Initial study by the EDL analysis of the “Target Maker” for guidance in Mars Exploration
Riho Takumi, Mayuri Sakamoto, Masaaki Kawamura
Teikyo University, Japan
2017-g-14 ( 10:20 – 10:40 )
Coplanar Aerocapture Reachable Domain
Hongwei Han1, Dong Qiao1, Dong Qiao2
1School of Aerospace Engineering, Beijing Institute of Technology, China, 2Key Laboratory of Autonomous Navigation and Control for Deep Space Exploration,Ministry of Industry and Information Technology
[g-4] Space Transportation (4)

Session Date June 8 (Thu) 11:00 – 12:20
Room Meeting Room 14
Chairpersons
2017-g-15 ( 11:00 – 11:20 )
Subsystem development status of H3 launch vehicle
Hironori Takeda1, Yorichika Mihara1, Osamu Kitayama1, Akihiro Satoh1, Mayuki Niitsu1, Wataru Sarae2, Hiroyuki Ueda2, Akito Hattori2, Kiyoshi Kobayashi2, Hiroyuki Nagata2
1Space systems engineering department, Mitsubishi Heavy Inductries, LTD, Japan, 2Japan Aerospace Exploration Agency
2017-g-16 ( 11:20 – 11:40 )
Hot-fire testing of LE-9 Engine for H3 launch vehicle
Daiki Watanabe2, Tetsuya Fujiwara1, Takashi Tamura1, Tadaoki Onga1, Teiu Kobayashi2, Koichi Okita2
1Liquid Rocket Engine Design Section, Mitsubishi Heavy Industries, LTD, 2Japan Aerospace Exploration Agency, Japan
2017-g-17 ( 11:40 – 12:00 )
Subscale Combustion Testing of Additive Manufacturing Injector
Akane Nagasaki1, Daiki Watanabe1, Takashi Tamura1, Tadaoki Onga1, Yoshio Nunome2, Hideto Kawashima2
1Liquid rocket engine design section, Mitsubushi Heavy Industries, LTD., Japan, 2Japan Aerospace Exploration Agency
2017-g-18 ( 12:00 – 12:20 )
Numerical Analysis of Flame Duct Flowfield affected by Rocket Engine Layout
Seiji Tsutsumi1, Wataru Sarae2, Hiroyuki Ueda2, Akito Hattori2
1Research Unit III, Aerospace Research and Development Directorate, JAXA, Japan, 2Range Technology Development Unit, Space Technology Directorate I, JAXA
[g-5] Space Transportation (5)

Session Date June 8 (Thu) 14:00 – 15:40
Room Meeting Room 14
Chairpersons
2017-g-19 ( 14:00 – 14:20 )
System Analysis of a Scramjet External Nozzle for Space Transportation Use
Tatsushi Isono1, Takahiro Fujikawa2, Takeshi Tsuchiya2, Ryo Mikoshiba3, Akiko Matsuo3, Sadatake Tomioka4
1Department of Aerospace Engineering, Tohoku University, Japan, 2Department of Aeronautics and Astronautics, The University of Tokyo, 3Department of Mechanical Engineering, Keio University, 4Research and Development Directorate, Japan Aerospace Exploration Agency
2017-g-20 ( 14:20 – 14:40 )
Plasma-assisted Aerodynamic Control with Thermoelectric Device for Space Transport
Yasumasa Watanabe1, Kojiro Suzuki2
1Department of Aeronautics and Astronautics, The University of Tokyo, Japan, 2Department of Advanced Energy, The University of Tokyo
2017-g-21 ( 14:40 – 15:00 )
Numerical and Experimental Approaches on Aerodynamic Characteristics of Waverider with Orbiter
Tomoki Uzaki1, Tomoyuki Muta1, Nobuyuki Tsuboi1, Yusuke Maru2, Kazuhisa Fujita2
1Department of mechanical engineering, Kyushu Institute of Technology, Japan, 2JAXA
2017-g-22 ( 15:00 – 15:20 )
CFD Analysis of Aerodynamic Characteristics during the ascent phase of Reusable Sounding Roket
Yoshiki Nishikawa1, Nobuyuki Tsuboi1, Takashi Ito2, Satoshi Nonaka2
1kyushu institute of technology, Japan, 2jaxa
2017-g-23 ( 15:20 – 15:40 )
Numerical study on Heat-Flux Mitigation by MHD flow control on Re-entry Vehicles
PARTHO PRATIM UPADHYAY, Raphael Tietz, Georg Herdrich
AEROSPACE ENGINEERING, INSTITUTE FUER RAUMFAHRTSYSTEME , UNIVERSITAET STUTTGART, Germany
[h-1] Combustion

Session Date June 8 (Thu) 16:00 – 17:20
Room Meeting Room 14
Chairpersons
2017-h-01 ( 16:00 – 16:20 )
Prediction of Limiting Oxygen Concentration of Thin Materials in Microgravity
Shuhei Takahashi, Keisuke Maruta
Department of Mechanical Engineering, Gifu University, Japan
2017-h-02 ( 16:20 – 16:40 )
Flame-spread characteristics of droplet-cloud element with two-droplet interaction at high pressure in microgravity
Kentaro Iwai1, Yasuko Yoshida1, Naoya Motomatsu2, Takehiko Seo1, Masato Mikami1
1Department of Graduate School of Sciences and Technology for Innovation, University of Yamaguchi, Japan, 2Department of Graduate School of Science and Engineering, University of Yamaguchi
2017-h-03 ( 16:40 – 17:00 )
Spontaneous-Ignition Experiments of a Fuel Droplet Pair using Two Michelson Interferometers in Two Directions
Osamu Moriue, Yuuki Takeuchi, Satoshi Takahashi, Masaoki Sugihara
Deprtment of Mechanical Engineering, Kyushu University, Japan
2017-h-04 ( 17:00 – 17:20 )
Effects of Ambient Pressure on Instantaneous Burning Rate of Hydrocarbon Fuel Droplet in High-Temperature Ambience under Microgravity
Shion ANDO
Department of Aeronautics and Astronautics, the University of Tokyo, Japan
[h-2] Fundamental Physics / Short Term Microgravity

Session Date June 9 (Fri) 9:40 – 10:40
Room Meeting Room 14
Chairpersons
2017-h-07 ( 9:40 – 10:00 )
Emulsion Dynamics under Microgravity
Yuji Yamashita1, Yukari Saikawa1, Takahiro Yamazaki1, Takeshi Endo2, Kenichi Sakai2, Hideki Sakai2, Masahiko Abe2, Makoto Natsuisaka3, Kazutami Sakamoto2
1Pharmaceutical Science, Chiba Institute of Science, Japan, 2Tokyo University of Science, 3Japan Aerospace Exploration Agency
2017-h-08 ( 10:00 – 10:20 )
UNMANNED PARABOLIC FLIGHT PLATFORM FOR REDUCED GRAVITY EXPERIMENTS
Marcello Valdatta1, Domantas Brucas2, Ugnius Ragauskas3, Matas Razgunas2, Tautvydas Skipitis3
1University of Bologna /Polaris Services, Italy, 2Space Science and Technology Institute, 3Space Science and Technology Institute / Vilnius Gediminas Technical University
2017-h-09 ( 10:20 – 10:40 )
An Attempt to Acquire Images of Three-Dimensional Magnetic Fields for Education Purposes Under the Microgravity Condition of Parabolic Flight
Tomoya Atsumi1, Marina Tsutsumi1, Ayaka Nakajima2, Yuko Watanabe2
1Department of physics , Tokyo University of Science , Oral, Japan, 2Department of industrial chemistry , Tokyo University of Science , Oral
[h-3] Levitation-1

Session Date June 9 (Fri) 11:20 – 12:40
Room Meeting Room 14
Chairpersons
2017-h-11 ( 11:20 – 11:40 )
Thermophysical and structural study of levitated droplet using electrostatic levitation and scattering devices
Geun Woo Lee
Frontier in Extreme Physics, Korea Research Institute of Standards and Science, Korea
2017-h-12 ( 11:40 – 12:00 )
Thermophysical Properties of Supercooled-liquid Silicon
Junpei OKADA1, Takehiko Ishikawa2, Yuki Watanabe3, Paul Fransois Paradis2, Satoshi Uda1
1Institute for Materials Research, Tohoku University, Japan, 2Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 3Advanced Engineering Services
2017-h-13 ( 12:00 – 12:20 )
Multiple pathways of crystal nucleation in an extremely supersaturated aqueous potassium dihydrogen phosphate (KDP) solution droplet
SOOHEYONG LEE1, Haeng Sub Wi1, Wonhyuk Jo1, Yong Chan Cho1, Hyun Hwi Lee2, Se-Young Jeong3, Geun Woo Lee1
1KOREA RESEARCH INSTITUTE OF STANDARDS AND SCIENCE, Korea, 2Pohang Accelerator Laboratory, 3Department of Cogno-Mechatronics Engineering, Pusan National University
2017-h-14 ( 12:20 – 12:40 )
Electrostatic Levitation for Materials Science Studies on the Ground, in Reduced Gravity, and on a Lunar Outpost
Paul-Francois Paradis1, Takehiko Ishikawa2, Won-Kyu Rhim3, Junpei T. Okada4
1INO, Canada, 2JAXA, 3Caltech, 4Tohoku University
[h-4] Levitation-2

Session Date June 9 (Fri) 14:00 – 15:40
Room Meeting Room 14
Chairpersons
2017-h-15 ( 14:00 – 14:20 )
Status and Prospects of Electrostatic Levitation Furnace (ELF) Experiment in ISS-KIBO
Haruka Tamaru1, Satoshi Yukizono1, Hideki Saruwatari1, Yasuhiro Nakamura1, Takehiko Ishikawa2, Tetsuya Takada3, Yumiko Sakai3
1Human Spaceflight Technology Directorate, Japan Aerospace Exploration Agency, Japan, 2Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 3Space Systems Department, IHI Aerospace Co., Led.
2017-h-16 ( 14:20 – 14:40 )
Measurements of Interfacial Tension between Molten Oxide and Steel Melt using Electrostatic Levitation Furnace (ELF) in ISS (INTERFACIAL ENERGY Project)
Masahito Watanabe1, Toshihiro Tanaka2, Takao Tsukada3, Takehiko Ishikawa4, Haruka Tamaru4
1Department of Physics, Gakushuin University, Japan, 2Osaka University, 3Tohoku University, 4JAXA
2017-h-17 ( 14:40 – 15:00 )
Thermophysical Properties Measurements of Liquid Alloys under Oxygen Influence in ISS (OXYTHERM Project)
Masahito Watanabe1, Shumpei Ozawa2, Juerrgen Brillo3
1Department of Physics, Gakushuin University, Japan, 2Chiba Institute of Technology, 3DLR
2017-h-18 ( 15:00 – 15:20 )
Thermophysical properties of Zr-O liquid alloys measured by electrostatic levitation
Yuji Ohishi1, Toshiki Kondo1, Takehiko Ishikawa2, Junpei T. Okada3, Yuki Watanabe4, Hiroaki Muta1, Ken Kurosaki1, Shinsuke Yamanaka1
1Graduate School of Engineering, Osaka University, Japan, 2Japan Aerospace Exploration Agency, 3Institute for Materials Research, Tohoku University, 4Advanced Engineering Services Co. Ltd.
2017-h-19 ( 15:20 – 15:40 )
Thermophysical Property Measurements of High Temperature Melts using Electrostatic Levitation Method
Takehiko Ishikawa1, Paul-Francois Paradis2, Yuki Watanabe3, Junpei T Okada4
1Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan, 2ino, 3A.E.S. Co. Ltd., 4Tohoku University
[h-5] Levitation-3 /Researches using the ISS

Session Date June 9 (Fri) 16:00 – 17:20
Room Meeting Room 14
Chairpersons
2017-h-20 ( 16:00 – 16:20 )
Contactless coalescence of acoustically levitated droplets under reduced gravity conditions
Ayumu Watanabe1, Motonori Niwa1, Kenji Kobayashi2, Tomohisa Yuasa1, Koji Hasegawa3, Satoshi Matsumoto4, Akiko Kaneko5, Yutaka Abe5
1Graduate School of System and Information Engineering, University of Tsukuba, Japan, 2College of Engineering Systems, University of Tsukuba, 3Department of Mechanical Engineering, Kogakuin Universirty, 4Japan Aerospace Exploration Agency, 5Department of Engineering Mechanics and Energy, University of Tsukuba
2017-h-21 ( 16:20 – 16:40 )
Overview of Space Experiment on Dynamic Surface Deformation Effects in Transition to Oscillatory Marangoni Flow in Liquid Bridge of High Prandtl Number Fluid
Taishi Yano1, Koichi Nishino1, Satoshi Matsumoto2, Ichiro Ueno3, Atsuki Komiya4, Yasuhiro Kamotani5, Nobuyuki Imaishi6
1Yokohama National University, Japan, 2Japan Aerospace Exploration Agency, 3Tokyo University of Science, 4Tohoku University, 5Case Western Reserve University, 6Kyushu University, Japan
2017-h-22 ( 16:40 – 17:00 )
Overview of Boiling Two-Phase Flow Experiment onboard Kibo
Satoshi Matsumoto1, Haruhiko Ohta2, Hitoshi Asano3, Osamu Kawanami4, Ryoji Imai5, Yasuhisa Shinmoto2
1Japan Aerospace Exploration Agency, Japan, 2Kyushu University, 3Kobe University, 4University of Hyogo, 5Muroran Institute of Technology
2017-h-23 ( 17:00 – 17:20 )
Summary of ALLOY SEMICONDUCTOR Project
Yuko Inatomi1, Nirmal Kumar Velu2, Mukannan Arivanandhan2, Takuya Yamamoto3, Xin Jin3, Haryo Mirsandi3, Yasunori Okano3, Yasuhiro Hayakawa2, Takehiko Ishikawa1
1Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency / School of Physical Sciences, SOKENDAI, Japan, 2Research Institute of Electronics, Shizuoka University, 3Department of Materials Engineering Science, Osaka University
2017-h-24 ( 17:20 – 17:40 )
The hardware development for the atomization experiment in microgravity on Kibo
Tatsuya Taguchi1, Yasuhiro Nakamura1, Masao Kikuchi1, Satoshi Matsumoto1, Satoshi Yukizono1, Hidetoshi Nakagami2, Wataru Ono2
1Japan Aerospace Exploration Agency, Japan, 2Chiyoda Corporation
[i-1] Advanced Theraml Control Device

Session Date June 9 (Fri) 9:00 – 10:20
Room Meeting Room 7
Chairpersons
2017-i-01 ( 9:00 – 9:20 )
Numerical Investigation of MEMS-based Black Body System using Thermoelectric Device
BongGeon Aiden Chae, Tae Gyu Kim, Hyun Ung Oh
Department of Aerospace Engineering, Chosun Univerisity, Korea
2017-i-05 ( 9:20 – 9:40 )
Transient Mathematical Modeling of a Loop Heat Pipe with a Thermoelectric Converter
Koki Sato1, Hosei Nagano2, Atsushi Okamoto3, Takeshi Miyakita3, Ryuta Hatakenaka3, Hiroyuki Sugita3
1Department of Aerospace Engineering, Nagoya University, Japan, 2Department of Mechanical Engineering, Nagoya University, 3Japan Aerospace Exploration Agency
2017-i-03 ( 9:40 – 10:00 )
Characteristics of thermophysical properties through metal-insulation transition for future advanced thermal control device
Jihoon Kim1, Daeil Park2, Hosei Nagano2, Sumitaka Tachikawa3
1Department of aerospace engineering, Nagoya University, Japan, 2Department of mechanical engineering, Nagoya University, 3Institute of Space and Astronautical Science, JAXA
2017-i-08 ( 10:00 – 10:20 )
One-dimensional Ablation and Thermal Response Program for Re-entry Analysis
Viola Renato1, Thomas Scanlon1, Richard Brown2
1Department of Mechanical and Aerospace Engineering, University of Strathclyde , UK, 2Sophrodyne Ltd
[i-2] Thermal Control System

Session Date June 9 (Fri) 11:00 – 12:20
Room Meeting Room 7
Chairpersons
2017-i-06 ( 11:00 – 11:20 )
Thermal Analysis and Design of Nano-satellite Systems
Mohammed Khalil Ibrahim, Daiki Kousaka, Yasuyuki Miyazaki
Aerospace Engineering Department, College of Science and Technology, Nihon University, Japan
2017-i-02 ( 11:20 – 11:40 )
Numerical Investigation of Transient Behavior of Loop Heat Pipes
Takuya Adachi, Hiroki Nagai
Institute of Fluid Science, Tohoku University, Japan
2017-i-07 ( 11:40 – 12:00 )
Design of Two-Phase Mechanically Pumped Fluid Loop with Large Isothermal Evaporator using Porous Wick Structure
Kenichi Sakamoto1, Takurou Daimaru1, Hiroki Nagai1, Eric Sunada2, Pradeep Bhandari2, Benjamin Furst2, Stefano Cappucci3
1Tohoku University, Japan, 2Jet Propulsion Laboratory, 3Polytechnic University of Turin
2017-i-11 ( 12:00 – 12:20 )
A multi-nodes model for the thermal performance of stratospheric airship
Liu Qiang, Yang Yan Chu, Zhang Tai Hua, Cai Jing Jing, Cui Yan Xiang
Academy of Opto-Electronics, Chinese Academy of Sciences, China
[i-3] Theraml Design for Future Spacecraft

Session Date June 9 (Fri) 14:00 – 15:00
Room Meeting Room 7
Chairpersons
2017-i-04 ( 14:00 – 14:20 )
Sensitivity Analysis of Thermal Performance to Flow Resistance of Check Valves in Oscillating Heat Pipe
Nao Inoue1, Takurou Daimaru1, Hiroki Nagai1, Makiko Ando2, Kousuke Tanaka2, Atsushi Okamoto2, Hiroyuki Sugita2, Daichi Isohata3
1Tohoku University, Japan, 2JAXA, 3Waseda University
2017-i-10 ( 14:20 – 14:40 )
Thermal based Path Planning using Solar Orientation for a Lunar Micro Rover
Hugo Tibor Mateo Zuliani, Takuto Oikawa, Kazuya Yoshida
Department of Aerospace Engineering, Tohoku University, Japan, Japan
2017-i-09 ( 14:40 – 15:00 )
Toward Uncertainty Quantification in Satellite Thermal Design
Hiroshi Kato, Makiko Ando, Moriyasu Fukuzoe
Japan Aerospace Exploration Agency, Japan
[j-1] Antennas and Stations

Session Date June 6 (Tue) 16:00 – 17:40
Room Meeting Room 15
Chairpersons
2017-j-01 ( 16:00 – 16:20 )
NEW RECEIVING GROUND ANTENNA FOR SATELLITES USING ACTIVE PHASED ARRAY ANTENNA
Nobuyuki Kaya, Rie Nakayama
Advanced Microwave Arrays , Japan
2017-j-02 ( 16:20 – 16:40 )
On board precise photogrammetric measurement of large reflector surface shape and precise beam formation for mobile communication satellite
Maki Akioka, Amane Miura, Teruaki Orikasa, Hiroyuki Tsuji, Morio Toyoshima, Masaki Satoh, Yoshiyuki Fujino
Wireless network research center, National Institute of Information and Communications Technology, Japan
2017-j-03 ( 16:40 – 17:00 )
Novel Satellite Antenna Pattern Compensation Method using Two Dimensional Least Square Method and Quadratic Function
Yoshiyuki Fujino, Masaki Sato, Amane Miura, Teruaki Orikasa, Maki Akioka
National Institute of Information and Communications Technology, Japan
2017-j-04 ( 17:00 – 17:20 )
Ground Station Performance Influenced by Cable Wrapping System
Tomoaki Toda1, Koji Yuchi2, Takashi Uchimura2, Kenji Numata2
1Department of Spacecraft Engineering, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan, 2GREAT Project Team, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
2017-j-05 ( 17:20 – 17:40 )
JAXA NEW DEEP SPACE GROUND STATION
Koji Yuchi, Kenji Numata, Takashi Uchimura, Tomoaki Toda, Masato Tsuboi, Yasuhiro Murata, Atsushi Tomiki, Fusaichi Nonaka, Tohru Ohnishi
GREAT Project Team, Japan Aerospace Exploration Agency, Japan
[j-2] Hardware Implimentation and Broadcasting

Session Date June 7 (Wed) 9:00 – 10:40
Room Meeting Room 14
Chairpersons
2017-j-06 ( 9:00 – 9:20 )
High power high efficient compact GaN amplifies for the solid-state radar.
Daisuke Hayashi1, Ryoko Kishikawa2, Shigeo Kawasaki3
1Koden Electronics Co., Ltd., Japan, 2SOKENDAI, 3JAXA
2017-j-07 ( 9:20 – 9:40 )
Newly developed 20W class on-board X-band GaN Solid State Power Amplifier
Mitsuhiro Nakadai, Masanobu Yajima
Research and Development Directorate, Japan Aerospace Exploration Agency, Japan
2017-j-08 ( 9:40 – 10:00 )
100W C-band GaN Solid State Power Amplifier with 50% PAE for Satellite Use
Masayuki Kido, Shingo Kawasaki, Atsushi Shibuya, Kenichi Yamada, Takahito Ogasawara, Toshimitsu Suzuki, Shinji Tamura, Kiyohaharu Seino, Akihiro Ichikawa, Akira Tsuchiko
Space System & Electronic Engineering Department, Mitsubishi Electric TOKKI Systems Corporation, Japan
2017-j-09 ( 10:00 – 10:20 )
APSK Transmission Experiments for Proto-type Equalization Using Satellite Characteristics over Satellite Channel
Masaaki Kojima, Yoichi Suzuki, Yuki Koizumi, Kyoichi Saito, Shoji Tanaka
NHK Science & Technology Research Laboratories, Japan
2017-j-10 ( 10:20 – 10:40 )
Satellite Broadcast Receiving System for Right- and Left-hand Circular Polarization in 12-GHz Band
Atsushi Iwasaki, Masafumi Nagasaka, Susumu Nakazawa, Shoji Tanaka
Science & Technology Research Laboratories, Japan Broadcasting Corporation, Japan
[j-3] WINDS and Next Systems

Session Date June 7 (Wed) 11:00 – 12:40
Room Meeting Room 14
Chairpersons
2017-j-11 ( 11:00 – 11:20 )
A study of ACM for power and bandwidth limited channel in satellite communication system
Mitsugu Ohkawa, Hiromitsu Wakana, Amane Miura
Space Communications Laboratory, Wireless Networks Reseach Center, National Institute of Information and Communications Technology, Japan
2017-j-12 ( 11:20 – 11:40 )
Experimental Evaluation of Non-linear Distortion Compensation Using the WINDS Satellite
Masanobu Yajima1, Mitsuhiro Nakadai1, Yoshiyuki Tashima2
1Research and Development Directorate, Japan Aerospace Exploration Agency, Japan, 2Space Engineering Development Co., Ltd.
2017-j-13 ( 11:40 – 12:00 )
High Speed Transmission for Ka-Band Aeronautical Satellite Communications Using WINDS
Tomoshige Kan, Takashi Takahashi, Norihiko Katayama, Toshio Asai, Kazuyoshi Kawasaki, Maki Akioka, Morio Toyoshima
Space Communications Laboratory, National Institute of Information and Communications Technology, Japan
2017-j-14 ( 12:00 – 12:20 )
Conceptual Design for Next Engineering Test Satellite
Kentaro Nishi, Kunitoshi Nishijo, Satoru Ozawa, Tadahiko Sano, Yasushi Hatooka
Research and Development Directorate, JAXA, Japan
2017-j-15 ( 12:20 – 12:40 )
Research Plan of R&D of Bandwidth-on-Demand High Throughput Satellite Communications System
Amane Miura1, Maki Akioka1, Naoko Yoshimura1, Kazunori Okada1, Kenji Suzuki1, Hiromitsu Wakana1, Shinichi Yamamoto11, Takashi Takahashi1, Kazuyoshi Kawasaki1, Tomoshige Kan1, Shinichi Kozono1, Toshihiro Kubooka1, Testuharu Fuse1, Hiroo Kunimori1, Morio Toyoshima1, Kazuma Kaneko2, Hiroki Nishiyama2, Nei Kato2, Eiichi Sakai3, Terumi Sunaga3
1Wireless Networks Research Center, NICT, Japan, 2Tohoku University, 3Mitsubishi Electric Corp
[j-4] Navigation and Applications

Session Date June 7 (Wed) 16:00 – 17:40
Room Meeting Room 14
Chairpersons
2017-j-16 ( 16:00 – 16:20 )
Precision Navigation Achieved by ASTRO-H Spaceborne GPS Receiver
Yu Nakajima1, Toru Yamamoto1, Yoshinori Kondoh1, Koji Yamanaka1, Kyohei Akiyama2, Mina Ogawa3, Susumu Kumagai4, Satoko Kawakami4, Masaru Kasahara4
1Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency, Japan, 2Flight Dynamics Team, Japan Aerospace Exploration Agency, 3ASTRO-H Project Team, Japan Aerospace Exploration Agency, 4Space Engineering Division, NEC Space Technologies, Ltd.
2017-j-17 ( 16:20 – 16:40 )
Combination Design of GNSS and GIS Implemented to Disaster Management System for Early Evacuation
Akihiko Nishino, Madoka Nakajima, Naohiko Kohtake
System Design and Management, Keio University, Japan
2017-j-18 ( 16:40 – 17:00 )
Stochastic Constellation Replenishment Planner
Federico Letterio1, Gonzalo Vicario1, Javier Martin1, Mauro Federici2, Daniel Navarro3
1Flight Systems, Deimos Space SLU, Spain, 2Flight Systems, Deimos Space UK, 3ESA/ESTEC
2017-j-19 ( 17:00 – 17:20 )
Environmental-data Collection System for Satellite-to-Ground Station Optical Communications
Kenji Suzuki, Dimitar Kolev, Alberto Carrasco Casado, Morio Toyoshima
Space Communications Laboratory, National Institute of Information and Communications Technology(NICT), Japan
2017-j-20 ( 17:20 – 17:40 )
Differential connected element interferometry (D-CEI) by using Beidou GEO satellites
SHAOWU CHEN, Haitao Li
the 2nd laboratory, Beijing Institute of Tracking and Telecommunications Technology, China
[j-5] Microsat

Session Date June 8 (Thu) 9:00 – 10:40
Room Meeting Room 7
Chairpersons
2017-j-21 ( 9:00 – 9:20 )
Updates on the Design and Implementation of the Philippine’s
Diwata-2 Amateur Radio Payload
Mary Ann Zabanal Constante, Joel Joseph Marciano, Marc Caesar Talampas, Adrian Salces, Izrael Zenar Bautista, Patth Rick Ramirez, Leonard Bryan Paet, Janette Salvatus, Edgar Paolo Violan, Aristotle Lopez, Orville Labbao
PHL-Microsat – University of the Philippines, Philippines
2017-j-22 ( 9:20 – 9:40 )
Self-Powered Beacon Development for Satellite Communication Loss Prevention
Rahmi Rahmatillah, Mengu Cho
Applied Science for Integrated System Engineering, Kyushu Institute of Technology, Japan
2017-j-23 ( 9:40 – 10:00 )
A Study on Laser Communication System Between Nano-Satellite and Ground Including Pointing, Acquisition and Tracking Control
Atsushi Kaji1, Shin Satori2, Koji Kumura1, Toshiki Nakamura1, Motoharu Taketsu1, Tomonori Ito2
1Department of Future Industry, Happy Science University, Japan, 2Hokkaido Satellite Corp. Ltd
2017-j-24 ( 10:00 – 10:20 )
Design of a MEMS-Mirror-based Laser Pointing Control System of Optical Transponder for Micro-satellites
Shunsuke Kawasaki, Toshinori Kuwahara, Masafumi Hiraoka, Toshiyuki Mogi, Daichi Morita, Shota Suzuki, Kazushi Fukuda, Yuji Sato, Yuji Sakamoto, Kazuya Yoshida
Department of Aerospace Engineering, Tohoku University, Japan
2017-j-25 ( 10:20 – 10:40 )
Tracking Control System Design and Evaluation of a Small Mobile Optical Ground Station for Satellite-to-Ground Optical Communication
Masafumi Hiraoka, Toshinori Kuwahara, Yuji Sato, Shinya Fujita, Kazufumi Fukuda, Shouta Suzuki, Shunsuke Kawasaki, Daichi Morita, Toshiyuki Mogi, Kazuya Yoshida
Department of Aerospace Engineering, Tohoku University, Japan
[k-1] ISS and Near Earth Missions

Session Date June 6 (Tue) 16:00 – 17:40
Room Meeting Room 8
Chairpersons
2017-k-01 ( 16:00 – 16:20 )
Technology of payloads maintenance aboard the ISS Russian Segment
Igor V. Sorokin
Space Stations Utilization Center, S.P. Korolev Rocket and Space Corporation Energia, Russia
2017-k-02 ( 16:20 – 16:40 )
The First Year In-Orbit Operation of the Tanpopo Mission onboard the ISS and Initial Results of Its Post-Retrieval Sample Analyses for Captured Microparticles
Hajime Yano1, Satoshi Sasaki2, Jun-ya Imani3, Daiki Horikawa4, Kazuyoshi Arai5, Masumi Higashide6, Eiichi Imai7, Yukihiro Ishibashi8, Yuko Kawaguchi9, Yoko Kebukawa10, Hajime Mita11, Kyoko Okudaira12, Takashi Ozawa6, Makoto Tabata13, Naomi Takizawa6, Masaru Tomita4, Yuichi Yaguchi12, Hirofumi Hashimoto1, Kensei Kobayashi10, Akihiko Yamagishi9, the Tanpopo Initial Sample Analysis and Curation Team1
1Department of Interdisciplinary Space Science, JAXA/Institute of Space and Astronautical Science, Japan, Japan, 2Tokyo University of Technology, Japan, 3Tokyo University of Agriculture and Technology, Japan, 4Keio University, Japan, 5Hosei University, Japan, 6Research and Development Directorate, JAXA, Japan, 7Nagaoka University of Technology, Japan, 8Kyushu University, Japan, 9Tokyo University of Pharmacy and Life Sciences, Japan, 10Yokohama National University, Japan, 11Fukuoka Institute of Technology, Japan, 12University of Aizu, Japan, 13Chiba University, Japan
2017-k-03 ( 16:40 – 17:00 )
Results from the Tanpopo Capture Panels: Using Silica Aerogel for Retrieving Cosmic Dust from Low-Earth Orbits
Makoto Tabata1, Hirofumi Hashimoto2, Daiki Horikawa3, Eiichi Imai4, Junya Imani5, Yukihiro Ishibashi6, Yuko Kawaguchi7, Yoko Kebukawa8, Kensei Kobayashi8, Hajime Mita9, Kyoko Okudaira10, Satoshi Sasaki11, Shin-ichi Yokobori7, Hajime Yano2, Akihiko Yamagishi7
1Chiba University, Japan, 2Japan Aerospace Exploration Agency, 3Keio University, 4Nagaoka University of Technology, 5Tokyo University of Agriculture and Technology, 6Kyushu University, 7Tokyo University of Pharmacy and Life Sciences, 8Yokohama National University, 9Fukuoka Institute of Technology, 10University of Aizu, 11Tokyo University of Technology
2017-k-04 ( 17:00 – 17:20 )
Preliminary Report of Tanpopo: Astrobiology Exposure and Micrometeoroid Capture Experiments at ISS
Akihiko Yamagishi1, Hirofumi Hashimoto2, Hajime Yano2, Shin-ichi Yokobori1, Kensei Kobayashi3, Hajime Mita4, Hikaru Yabuta5, Masumi Higashide6, Makoto Tabata7, Hideyuki Kawai7, Eiichi Imai 8
1Department of Applied Life Science, Tokyo University of Pharmacy and Life Sciences, Japan, 2ISAS/JAXA, Japan, 3Yokohama National University, Japan, 4Fukuoka Institute of Technology, Japan, 5Osaka University, Japan, 6JAXA, Japan, 7Chiba University, Japan, 8Nagaoka University of Technology, Japan
2017-k-05 ( 17:20 – 17:40 )
Experimental Verification Strategy of Navigation Involved Contact Dynamics under Micro Gravity
Hiroki Kato, Daichi Hirano, Mari Nishiyama, Ippei Takahashi
Research Unit II, Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA), Japan
[k-2] Small Bodies and Dust Explorations (1)

Session Date June 7 (Wed) 9:00 – 10:40
Room Meeting Room 8
Chairpersons
2017-k-06 ( 9:00 – 9:20 )
In-Flight Performance of Thermal Infrared Imager on Hayabusa2 and Its Implication to the Observations of Asteroid 162173 Ryugu
Tatsuaki Okada1, Tetsuya Fukuhara2, Satoshi Tanaka1, Makoto Taguchi2, Takehiko Arai3, Hiroki Senshu4, Hirohide Demura5, Yoshiko Ogawa5, Toru Kouyama6, Ryosuke Nakamura6, Naoya Sakatani7, Jun Takita8, Tomohiko Sekiguchi9, Sunao Hasegawa1, Tsuneo Matsunaga3, Takeshi Imamura8, Takehiko Wada1, Jorn Helbert10, Thomas G. Mueller11, Axel Hagermann12
1Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan, 2Graduate School of Science, Rikkyo University, 3National Institute for Environmental Studies, 4Planetary Exploration Research Center, Chiba Institute of Technology, 5Research Center for Advanced Information Science and Technology, University of Aizu, 6National Institute of Advanced Industrial Science and Technology, 7Graduate School of Science and Technology, Meiji University, 8Graduate School of Science, The University of Tokyo, 9Hokkaido University of Education, 10Institute for Planetary Research, German Aerospace Center, 11Max-Planck Institute for Extraterrestrial Physics, 12School of Physical Sciences, The Open University
2017-k-07 ( 9:20 – 9:40 )
High-Speed Mobile Optical Orbit Determination System for HAYABUSA2 Capsule Recovery
Kazuhisa Fujita1, Hiroki Takayanagi1, Hiroka Inoue1, Satoshi Nomura1, Toshiyuki Suzuki1, Étienne Houzé2
1Japan Aerospace Exploration Agency, Japan, 2École Polytechnique
2017-k-08 ( 9:40 – 10:00 )
Effects of the Rotation and Interior Density Distribution on the Surface Gravity for Itokawa
Masanori Kanamaru
Department of Earth and Space Science, Graduate School of Science, Osaka University, Japan
2017-k-09 ( 10:00 – 10:20 )
Robust Tracking of Visual Landmarks for Estimating Asteroid Shape and Motion
Kentaro Abe
Department of Aeronautics and Astronautics, Faculity of Engineering, The University of Tokyo, Japan
2017-k-10 ( 10:20 – 10:40 )
AIM: a mission of firsts in deep-space
Ian Carnelli1, Michael Kueppers2, Karim Mellab3, Vasco Pesquita3, Borja Gutierrez3, Massimo Casasco3, Jesus Gil3, Paolo Martino3
1Future preparation and strategic studies, European Space Agency, France, 2ESA-ESAC, 3ESA-ESTEC
[k-3] Small Bodies and Dust Explorations (2)

Session Date June 7 (Wed) 11:00 – 12:35
Room Meeting Room 8
Chairpersons
2017-k-11 ( 11:00 – 11:15 )
Numerical Estimation of Gamma-ray Spectroscopy for Deep Space Microsatellite
Masayuki Naito1, Junya Ishii1, Kouhei Yoshida1, Daisuke Aoki1, Hiroshi Nagaoka2, Eido Shibamura2, Nobuyuki Hasebe2
1Department of Physics, School of Advanced Science and Engineering, Waseda University, Japan, 2Research Institute for Science and Engineering, Waseda Unversity
2017-k-12 ( 11:15 – 11:30 )
Neutron Spectroscopy for Exploration of Near-Earth Asteroids
Junya Ishii2, Daisuke Aoki1, Masayuki Naito1, Hiroshi Nagaoka2, Nobuyuki Hasebe2
1School of Advanced Science and Engineering, Waseda university, Tokyo, Japan, 2Research Institute for Science and Engineering, Waseda University, Tokyo, Japan , Japan
2017-k-13 ( 11:30 – 11:45 )
The cooling system of HPGe gamma-ray spectrometer on a deep space microsatellite
Takuto Adachi, Mana Shikishima, Hiroshi Nagaoka, Masayuki Naito, Eido Shibamura, Nobuyuki Hasebe
School of Advanced Science and Engineering, Waseda University, Japan
2017-k-14 ( 11:45 – 12:05 )
DESTINY + : A Mission Proposal for Technology Demonstration and Exploration of Asteroid 3200 Phaethon
Kazutaka Nishiyama1, Yasuhiro Kawakatsu1, Hiroyuki Toyota1, Ryu Funase2, Tomoko Arai3
1Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan, 2The University of Tokyo, 3Chiba Institute of Technology
2017-k-15 ( 12:05 – 12:20 )
Dust Sensor with Large Sensitive Area Using Multi-Layer Insulation and Piezoelectric Elements.
Masanori Kobayashi, Osamu Okudaira, Kosuke Kurosawa, Takaya Okamoto, Takafumi Matsui
Planetary Exploration Research Center, Chiba Institute of Technology, Japan
2017-k-16 ( 12:20 – 12:35 )
Size and Orbital Distribution of Interplanetary Dusts by MU Radar Meteor Head Echo Observation
Shinsuke Abe1, Johan Kero2, Takuji Nakamura3, Yasunori Fujiwara3, Junichi Watanabe4, Hiroyuki Hashiguchi5
1Nihon University, Japan, Japan, 2Swedish Institute of Space Physics, Sweden, 3National Institute of Polar Research, Japan, 4National Astronomical Observatory of Japan, 5Research Institute for Sustainable Humanosphere, Kyoto University, Japan
[k-4] Exploration for Trojan Asteroids by Solar Power Sail

Session Date June 7 (Wed) 16:00 – 17:40
Room Meeting Room 8
Chairpersons
2017-k-18 ( 16:00 – 16:20 )
Navigation to Jovian Trojan Asteroid using Solar Power Sail-craft and Underground Sampling using Lander
Osamu Mori1, Jun Matsumoto1, Hideki Kato1, Takanao Saiki1, Yuichi Tsuda1, Naoko Ogawa1, Yuya Mimasu1, Junichiro Kawaguchi1, Koji Tanaka1, Hiroyuki Toyota1, Nobukatsu Okuizumi1, Fuyuto Terui1, Shigeo Kawasaki1, Kazutaka Nishiyama1, Satoshi Hosoda1, Kazuhiko Yamada1, Tatsuaki Okada1, Takahiro Iwata1, Ralf Boden2, Toshihiro Chujo2, Yusuke Oki2, Yuki Takao2
1Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan, 2Department of Aeronautics and Astronautics, The University of Tokyo
2017-k-17 ( 16:20 – 16:40 )
Sampling Operation for the Jupiter Trojan Asteroid Exploration
Jun Matsumoto1, Chisato Okamoto2, Yusuke Oki3, Takuma Nakamura4, Jun Aoki5
1Japan Aerospace Exploration Agency, Japan, 2Kobe University, 3The University of Tokyo, 4Aoyama Gakuin University, 5Osaka University
2017-k-19 ( 16:40 – 17:00 )
Two Motors Drive Rotary Sample Conveyance Mechanism
Shuya Kashioka
Department of Space and Astronautical Science, The Graduate University for Advanced Studies, Japan
2017-k-20 ( 17:00 – 17:20 )
Science and Instrumentation for Exploring a Jupiter Trojan Asteroid in the Solar Power Sail Mission
Tatsuaki Okada1, Yoko Kebukawa2, Jun Aoki3, Motoo Ito4, Masatsugu Otsuki1, Chisato Okamoto5, Yusuke Oki6, Jun Matsumoto1, Hajime Yano1, Ryosuke Nakamura7, Takahiro Iwata1, Osamu Mori1, Jean-Pierre Bibring8, Stephan Ulamec9
1Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan, 2Faculty of Engineering, Yokohama National University, 3Graduate School of Science, Osaka University, 4Kochi Core Center, Japan Agency for Marine-Earth Science and Technology, 5Graduate School of Science, Kobe University, 6The University of Tokyo, 7National Institute of Advanced Industrial Science and Technology, 8Institut d’Astrophysique Spatiale, Orsay, 9Deutsches Zentrum für Luft- und Raumfahrt
2017-k-21 ( 17:20 – 17:40 )
Scientific Subjects and Candidate Instruments in the Cruising Phase of the Solar Power Sail
Takahiro Iwata1, Shuji Matsuura2, Kohji Tsumura3, Hajime Yano1, Takayuki Hirai4, Ayako Matsuoka1, Reiko Nomura1, Daisuke Yonetoku5, Takehiro Mihara6, Tatsuaki Okada1, Jun Matsumoto1, Osamu Mori1
1Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan, 2Kwansei Gakuin University, 3Tohoku University, 4Japan Aerospace Exploration Agency, 5Kanazawa University, 6RIKEN
[k-5] Mercurial and Lunar Explorations

Session Date June 8 (Thu) 9:00 – 10:00
Room Meeting Room 8
Chairpersons
2017-k-22 ( 9:00 – 9:20 )
The BepiColombo Spacecraft and its Mission to Mercury
Roger John Wilson, Markus Schelkle
Airbus DS GmbH, Friedrichshafen, Germany
2017-k-23 ( 9:20 – 9:40 )
Japanese Lunar Polar Exploration Lander
Tatsuaki Hashimoto, Takeshi Hoshino, Hisashi Otake, Satoshi Tanaka, Sachiko Wakabayashi, Hitoshi Morimoto, Koichi Masuda, Makiko Ohtake, Masataku Suto, Takanobu Shimada
Japan Aerospace Exploration Agency, Japan
2017-k-24 ( 9:40 – 10:00 )
Skid Sliding System to Travel on Planetary Surface
Hikaru Eguchi1, Yusuke Maru1, Masatsugu Otsuki2, Shunpei Morikawa3, Shujiro Sawai1
1Department of Physical Sciences, The Graduate University of Advanced Studies (SOKENDAI), Japan, 2JAXA, 3Shizuoka University
[k-6] Lunar Science and Utilization

Session Date June 8 (Thu) 11:00 – 12:40
Room Meeting Room 8
Chairpersons
2017-k-27 ( 11:00 – 11:20 )
Development of X-ray Generators for active X-ray Fluorescence Spectroscopy of Future Lunar Landing Mission, and Its Contribution to Lunar Science
Hiroshi Nagaoka1, Nobuyuki Hasebe1, Masayuki Naito2, Eido Shibamura1, Haruyoshi Kuno1, Miho Mizone2, Yoshiki Nabekura2, Kyeong Ja Kim3
1Research Institute of Science and Engineering, Waseda University, Japan, 2Schools of Advanced Science and Engineering, Waseda University, 3KIGAM
2017-k-28 ( 11:20 – 11:40 )
Introduction to the Current Development Status of a Gamma-Ray Spectrometer for the Korea Pathfinder Lunar Orbiter
Kyeong Ja Kim1, Junghun Park1, Yire Choi1, Eung Seok Yi3, Sung-Soon Lee1, Young-Kwang Yeon1, Chang Wan Sun2, K. B. Lee4, Yong-Kwon Kim5, Kyungwook Min6, Kyungin Kang6, Jin Yeon Cho7, Jeong Hun Cha7, Nobuyuki Hasebe8, Richard Elphic9, Peter Englert10, Olivier Gasnault11, Eido Shibamura8, Hiroshi Nagaoka8, Lucy Lim12
1Geological Research Center, Korea Institute of Geoscience and Mineral Resources, Korea, 2University of Science and Technology, 3Chungnam National University, 4Korea Research Institute of Standards and Science, 5Nucare, , 6Korea Advanced Institute of Science and Technology, 7Inha University, 8Waseda University, 9NASA Ames Research Center, 10Quest University, 11IRAP, 12NASA Goddard Space Flight Center
2017-k-29 ( 11:40 – 12:00 )
Concept Study of Human Lunar Exploration Precursor Programme (HLEPP) in Japan Aerospace Exploration Agency
Hirotaka Sawada1, Naoki Sato4, Markus Landgraf2, Martin Picard3, Yuya Mimasu4, Takeshi Hoshino4, Tatsuaki Hashimoto4
1ISAS, Japan Aerospace Exploration Agency, Japan, 2European Space Agency, 3Canadian Space Agency, 4Japan Aerospace Exploration Agency
2017-k-30 ( 12:00 – 12:20 )
Study on sand and volcanic ash solidification technology for in-situ resource utilization
Takeshi Hoshino1, Masaki Ikehara2, Hiroshi Kanamori1, Satoshi Hoshida1, Sachiko Wakabayashi1
1Space Exploration Innovation Hub Center, Japan Aerospace Exploration Agency, Japan, 2MORUTARU MAGIC Co.,Ltd.
2017-k-31 ( 12:20 – 12:40 )
Experimental Study on Vibration Compaction Method for Lunar Base Construction
Sachiko Wakabayashi1, Takeshi Hoshino1, Jun Makabe2
1Japan Aerospace Exploration Agency, Japan, 2Sakai Heavy Industries, LTD.
[k-7] Technologies for Lunar and Planetary Explorations (1) – Landing

Session Date June 8 (Thu) 14:00 – 15:40
Room Meeting Room 8
Chairpersons
2017-k-32 ( 14:00 – 14:20 )
Planetary image recognition using Deep Learning.
Hiya Roy1, Tatsuaki Hashimoto2
1Department of Electrical Engineering and Information Systems, University of Tokyo, Japan, 2Professor, Department of Spacecraft Engineering, Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA).
2017-k-33 ( 14:20 – 14:40 )
Supersonic Retro-Propulsion for Future High-Mass Mars Lander Missions
Marcus Lobbia, Aron Wolf, Charles Whetsel
NASA Jet Propulsion Laboratory, USA
2017-k-34 ( 14:40 – 15:00 )
Hazard Avoidance Control Using Stochastic Optimization for Mars Safe Landing
Ryohei Takahashi
Department of aeronautics and astronautics, University of Tokyo, Japan
2017-k-35 ( 15:00 – 15:20 )
Development and Demonstration of a Flying Test Bed for Planetary Landing
Kazuhisa Fujita1, Hiroki Takayanagi1, Takashi Ozawa1, Toshiyuki Suzuki1, Satoshi Nomura1, Seiya Ueno2, Takehiro Higuchi2, Hiroaki Kobayashi3, Nobutaka Bando4, Naomi Takizawa3
1Research and Development Directorate, Japan Aerospace Exploration Agency, Japan, 2Yokohama National University, 3Aeronautical Technology Directorate, Japan Aerospace Exploration Agency, 4Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
2017-k-36 ( 15:20 – 15:40 )
Planetary Exploration Spacecraft Landing Gear with Three-Dimensional Linear-Rotary-Energy-Conversion Mechanism
Susumu Hara1, Satoshi Saito2, Keisuke Sugita1, Takao Maeda3
1Department of Aerospace Engineering, Graduate School of Engineering, Nagoya University, Japan, 2Department of Mechanical and Aerospace Engineering, School of Engineering, Nagoya University, 3Department of Electrical, Electronic, and Communication Engineering, Faculty of Science and Engineering, Chuo University
[k-8] Technologies for Lunar and Planetary Explorations (2) – Rover and Sampling

Session Date June 8 (Thu) 16:00 – 17:40
Room Meeting Room 8
Chairpersons
2017-k-37 ( 16:00 – 16:20 )
Capability of a Time-of-Flight Camera as an Obstacle Avoidance Sensor for a Moon Exploration Micro Rover
Uno Kentaro1, Louis Jerome Burtz2, Marc Hulcelle3, Kazuya Yoshida1
1Department of Aerospace Engineering, Tohoku University, Japan, 2KK ispace inc., 3École des Mines de Saint-Étienne
2017-k-38 ( 16:20 – 16:40 )
Dynamic Locomotion of a Multi-Legged Planetary Exploration Rover with Isotropic Leg Arrangement
Tomohito Sekiguchi, Saki Omi, Mai Bando, Shinji Hokamoto
Department of aeronautics and astronautics, Kyushu university, Japan
2017-k-39 ( 16:40 – 17:00 )
A Concept of Simple and Light Weight Mars Rover integrated with EDL System
Ichimura Masaaki
Department of International Development Engineering , Tokyo Institute of Technology, Japan
2017-k-40 ( 17:00 – 17:20 )
Electrostatic Sampling and Transport of Water Ice in Space Environment
Hiroyuki Kawamoto
Dept. Applied Mechanics and Aerospace Engineering, Waseda University, Japan
2017-k-41 ( 17:20 – 17:40 )
CONCEPT OF SAMPLE RETURN MISSION FOR MARS SURFACE EXPLORATION
Nadeem Alam
Department of Aeronautical Engineering, Babu Banarasi Das National Institute of Technology and Management , India
[k-9] Martian Airplane

Session Date June 9 (Fri) 9:00 – 10:40
Room Meeting Room 8
Chairpersons
2017-k-42 ( 9:00 – 9:20 )
Flight System of Mars Airplane Balloon Experiment-1 (MABE-1)
Akira Oyama1, Hiroki Nagai2, Hiroshi Tokutake3, Koji Fujita1, Masayuki Anyoji4, Hiroyuki Toyota1, Yu Miyazawa1, Koichi Yonemoto5, Masato Okamoto6, Taku Nonomura7, Masakazu Motoda8, Shinsuke Takeuchi1, Yukio Kamata1, Masatsugu Otsuki1, Keisuke Asai9, Kozo Fujii10
1Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan, 2Institute of Fluid Science, Tohoku University, 3Kanazawa University, 4Kyushu University, 5Kyushu Institute of Technology, 6Kanazawa Institute of Technology, 7Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, currently Tohoku University, 8Aeronautical Technology Directorate, Japan Aerospace Exploration Agency, 9Tohoku University, 10Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, currently Tokyo University of Science
2017-k-43 ( 9:20 – 9:40 )
Evaluation of Aerodynamic Characteristics on Mars Airplane Balloon Experiment-1 (MABE-1)
Masayuki Anyoji1, Masato Okamoto2, Koji Fujita3, Hiroki Nagai4, Akira Oyama3
1Department of Energy and Environmental Engineering, Interdisciplinary Graduate School of Engineering Sciences, Kyushu University, Japan, 2Department of Aeronautics, Kanazawa Institute of Technology, 3Institute of Space and Astronautical Science, JAXA, 4Institue of Fluid Science, Tohoku University
2017-k-44 ( 9:40 – 10:00 )
Flight Control Parameter Design for Mars Airplane Balloon Experiment-1 (MABE-1) Using Evolutionary Computation
Koji Fujita1, Hiroshi Tokutake2, Hiroki Nagai3, Akira Oyama1
1Department of Space Flight System, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan, 2School of Mechanical Engineering, College of Science and Engineering, Kanazawa University, 3Institute of Fluid Science, Tohoku University
2017-k-45 ( 10:00 – 10:20 )
Attitude Estimation using Thermopile Sensors on Mars Airplane Balloon Experiment-1 (MABE-1)
Hiroshi Tokutake1, Koji Fujita2, Akira Oyama2, Hiroki Nagai3
1Kanazawa University, Japan, 2Institute of Space and Astronautical Science, JAXA, 3Institute of Fluid Science, Tohoku University
2017-k-46 ( 10:20 – 10:40 )
Comparison of Thermal Analysis and Flight Test Results on Mars Airplane Balloon Experiment-1 (MABE-1)
Hiroki Nagai1, Yasuyuki Oda1, Koji Fujita2, Akira Oyama2
1Institute of Fluid Science, Tohoku University, Japan, 2Institute of Space and Astronautical Science, JAXA
[k-10] New Views of our Solar System and Knowledges to Support them

Session Date June 9 (Fri) 11:00 – 12:40
Room Meeting Room 8
Chairpersons
2017-k-47 ( 11:00 – 11:20 )
Numerical Simulation of High-Speed Impact on Regolith Using Compressible and Non-Expanding Fluid Model
Kojiro Suzuki
Graduate School of Frontier Sciences, The University of Tokyo, Japan
2017-k-48 ( 11:20 – 11:40 )
Space Weathering Simulation with Sulfur
Sho Sasaki1, Hirokazu Tanaka1, Yasunori Kanamaru1, Mizuki Okazaki1, Takahiro Hiroi2
1Department of Earth and Space Science, Osaka University, Japan, 2Brown University
2017-k-49 ( 11:40 – 12:00 )
LDM (Life Detection Microscope): In situ imaging of living cells on surface of Mars
Akihiko Yamagishi1, Takehiko Satoh2, Atsuo Miyakawa1, Yoshitaka Yoshimura3, Satoshi Sasaki4, Kensei Kobayashi5, Yoko Kebukawa5, Hikaru Yabuta6, Hajime Mita7, Eiichi Imai8, Takeshi Naganuma9, Kazuhisa Fujita11, Tomohiro Usui10
1Department of Applied Life Science, Tokyo University of Pharmacy and Life Sciences, Japan, 2ISAS/JAXA, Japan, 3Tamagawa University, Japan, 4Tokyo University of Technology, Japan, 5Yokohama National University, Japan, 6Osaka University, Japan, 7Fukuoka Institute of Technology, Japan, 8Nagaoka University of Technology, Japan, 9Hiroshima University, Japan, 10Tokyo Institute of Technology, Japan, 11JAXA, Japan
2017-k-50 ( 12:00 – 12:20 )
FLOWING WATER ON MARS – EXTRACTING THE SIGN OF LIFE ON MARS
Nadeem Alam
Department of Aeronautical Engineering, Babu Banarasi Das National Institute of Technology and Management , India
2017-k-51 ( 12:20 – 12:40 )
Designing a Titan Gas and Energy Relay Station (TiGERS): A Concept for Sustaining Deep Space Interplanetary Mission and Beyond
Huai-Chien Chang1, Chun-Chieh Wang2
1Consortium of Spacce Settlements, Astronautical Society of Taiwan., Taiwan, 2Research Assistant, Geomatics Laboratory of National Taipei University of Technology
[k-11] Explorations for Mars and its Moons

Session Date June 9 (Fri) 14:00 – 15:35
Room Meeting Room 8
Chairpersons
2017-k-52 ( 14:00 – 14:20 )
Martian Moons Exploration (MMX) Conceptual Study Results
Yasuhiro Kawakatsu1, Kiyoshi Kuramoto2, Masaki Fujimoto1
1ISAS, JAXA, Japan, 2Hokkaido University
2017-k-53 ( 14:20 – 14:35 )
Near-infrared spectrometer NIRS4/MacrOmega for the Martian moon’s sample return mission MMX
Takeshi Sakanoi1, Takahiro Iwata2, Hiromu Nakagawa1, Jean-Pierre Bibring3, Vincent Hamm3, Cedric Pilorget3, Tomoki Nakamura1, Shohei Aoki4, Sarah Crites2, Yasumasa Kasaba1
1Graduate School of Science, Tohoku University, Japan, Japan, 2JAXA, Japan, 3Institut d’Astrophysique Spatiale, Université Paris-Sud, France, 4Institut d’Aéronomie Spatiale de Belgique, Brussels, Belgium
2017-k-54 ( 14:35 – 14:50 )
Nuclear Spectroscopy for Unveiling the Origin of the Martian Moons
Nobuyuki Hasebe2, Hiroshi Nagaoka1, Masayuki Naito2, Eido Shibamura1, Haruyoshi Kuno1, Sota Shimizu3, Kyeong Ja Kim4, Valery V. Dmitrenko5, Tomoki Nakamura6, Hisashi Otake7
1Research Institute for Science and Engineering, Waseda University, 2Department of Physics, School of Advanced Science and Engineering, Waseda University, Japan, 3Graduate School of Science and Technology, Keio University, 4Planetary Geology Department, Geological Research Division, Korean Institute of Geoscience and Mineral Resources, 5National Research Nuclear University, Moscow Engineering Physics Institute (MEPhI), 6Division of Earth and Planetary Materials Science, Tohoku University, 7Japan Aerospace Exploration Agency (JAXA)
2017-k-55 ( 14:50 – 15:05 )
An ion mass spectrometer for observation of secondary ions from small bodies
Shoichiro Yokota, Ayako Matsuoka, Reiko Nomura, Yoshifumi Saito
ISAS/JAXA, Japan
2017-k-56 ( 15:05 – 15:20 )
NASA Mars 2020 Landed Mission Development
Michael G. Wilson, Jennifer Trosper, Fernando Abilleira
Mars 2020 Project, Jet Propulsion Laboratory / California Institute of Technology, USA
2017-k-57 ( 15:20 – 15:35 )
CONCEPT OF INCREASING THE AMOUNT OF OXYGEN ON MARS WITH HELP OF
ULTRAVOILET LIGHT
Nadeem Alam
Department of Aeronautical Engineering, Babu Banarasi Das National Institute of Technology and Management , India
[k-12] Explorations for Sun, Planets, and Exo-planets

Session Date June 9 (Fri) 16:00 – 17:40
Room Meeting Room 8
Chairpersons
2017-k-58 ( 16:00 – 16:20 )
Experiment SIGNAL Onboard the Interhelioprobe Spacecraft
Nobuyuki Hasebe1, Valery V. Dmitrenko2, Sergey E. Ulin2
1Research Institute for Science and Engineering, Waseda University, Japan, 2National Research Nuclear University, Moscow Engineering Physics Institute (MEPhyI)
2017-k-59 ( 16:20 – 16:40 )
Project GIVE (Grown in Venus Enclosure): An Alternative Solution for Sustaining Spacefaring Civilization
Huai-Chien Chang1, Chun-Chieh Wang2
1Consortium of Spacce Settlements, Astronautical Society of Taiwan., Taiwan, 2Research Assistant, Geomatics Laboratory of National Taipei University of Technology
2017-k-60 ( 16:40 – 17:00 )
The Ganymede Laser Altimeter (GALA) for ESA’s Jupiter Icy Moons Explorer
Hauke Hussmann1, Keigo Enya2, Reinald Kallenbach1, Jun Kimura3, Masanori Kobayashi4, Luisa Lara5, Kay Lingenauber1, Noriyuki Namiki6, Sho Sasaki3, Nicolas Thomas7, Christian Althaus1, Thomas Behnke1, Belinda Borgs1, Judit Jänchen1, Horst-Georg Lötzke1, Karsten Seiferlin7, Alexander Stark1, Gregor Steinbrügge1, Simone del Togno1, Toshihiko Yamawaki2
1DLR Institute of Planetary Research, Berlin, Germany, 2ISAS/JAXA, Japan, 3Osaka University, Japan, 4Chiba Institute of Technology, Japan, 5IAA-CSIC Granada, Spain, 6National Astronomical Observatory, Japan, 7University of Bern, Switzerland
2017-k-61 ( 17:00 – 17:20 )
Overview of SPRITE: Saturn PRobe Interior and aTmosphere Explorer Concept
Marcus Lobbia1, Amy Simon2, Rolf Danner1, David Atkinson1
1NASA Jet Propulsion Laboratory, USA, 2NASA Goddard Space Flight Center
2017-k-62 ( 17:20 – 17:40 )
Twinkle – A new idea for commercial astrophysics mission
Alex da Silva Curiel3, Susan Jason3, Marcell Tessenyi1, Giovanna Tinetti1, Jonathan Tennyson1, Enzo Pascale2, James Williams3, Gavin Johnson3, Simon Prassad3, Amor Vora3, Chris Saunders3, Jonathan Friend3, Martin Sweeting3
1University College London (UCL), 2Cardif University, 3Surrey Satellite Technology Ltd., UK
[m-1] Astrophysics using Balloon and Sounding Rocket

Session Date June 9 (Fri) 9:00 – 10:40
Room Meeting Room 12
Chairpersons
2017-m-01 ( 9:00 – 9:20 )
GRAINE project : analysis status of balloon experiment in 2015
Fukashi Mizutani1, Shigeki Aoki1, Kaname Hamada2, Toshio Hara3, Atsushi lyono4, Hiroaki Kawahara5, Koichi Kodama6, Ryosuke Komatani5, Masahiro Komatsu5, Kenji Kuretsubo1, Toshitsugu Marushima1, Haruka Matsumoto1, Motoaki Miyanishi5, Kunihiro Morishima5, Misaki Morishita5, Naotaka Naganawa5, Mitsuhiro Nakamura5, Toshiyuki Nakano5, Akira Nishio5, Kimio Niwa5, Naoto Otsuka5, Keita Ozaki1, Hiroki Rokujo5, Osamu Sato5, Emi Shibayama1, Atsumu Suzuki7, Satoru Takahashi1, Yurie Tateishi1, Misato Yabu1, Kyohei Yamada1, Saya Yamamoto4, Masahiro Yoshimoto5
1Department of Human Development, Kobe University, Japan, 2ISAS, JAXA, 3Department of Science Development, Kobe University, 4Department of Science, Okayama University of Science, 5Department of Science, Nagoya University, 6Aichi University of Education, 7Department of Science, Kobe University
2017-m-02 ( 9:20 – 9:40 )
MeV Gamma-Ray Observation based on the Ray-Tracing Cameras loaded on Balloons
Atsushi Takada1, Toru Tanimori1, Tetsuya Mizumoto1, Yoshitaka Mizumura1, Shotaro Komura1, Tetsuro Kishimoto1, Taito Takemura1, Yuma Nakamasu1, Kei Yoshikawa1, Tomoyuki Taniguchi1, Yuta Nakamura1, Shunsuke Kurosawa2
1Department of Physics, Kyoto University, Japan, 2Tohoku University
2017-m-03 ( 9:40 – 10:00 )
PoGO+ stratospheric balloon mission from Esrange, Sweden, to Victoria Island, Canada
Mattias Abrahamsson, Christian Lockowandt
Science Services, Swedish Space Corporation, Sweden
2017-m-04 ( 10:00 – 10:20 )
Cryogenic 32×32 CTIA Multiplexer for Far-Infrared Astronomy
Shunsuke Baba1, Koichi Nagase2, Takehiko Wada2, Hirokazu Ikeda2, Yasuo Arai3, Morifumi Ohno4, Takahiro Ishimaru2
1Department of Physics, Graduate School of Science, The University of Tokyo, Japan, 2Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency , 3High Energy Accelerator Research Organization, 4National Institute of Advanced Industrial Science and Technology
2017-m-05 ( 10:20 – 10:40 )
Microgravity experiments to understand cosmic dust formation in the gas outflow from oxygen-rich stars
Yuki Kimura1, Shinnosuke Ishizuka1, Tomoya Yamazaki1, Itsuki Sakon2, Kyoko K Tanaka1, Shinsuke Takeuchi3, Yuko Inatomi3
1Institute of Low Temperature Science, Hokkaido University, Japan, 2The University of Tokyo, 3JAXA/ISAS
[m-2] Engineering of Scientific Balloon and Sounding Rocket System

Session Date June 9 (Fri) 11:00 – 12:20
Room Meeting Room 12
Chairpersons
2017-m-06 ( 11:00 – 11:20 )
Characteristics Evaluation and Performance Improvement Method of Balloon-Borne Telescope Pointing Control System
Toshihiko Nakano1, Makoto Taguchi2, Yasuhiro Shoji3, Mao Takamura2, Daiki Sunaguchi2, Masataka Imai4, Makoto Watanabe5, Yukihiro Takahashi4, Yuji Sakamoto6, Kazuya Yoshida6
1Department of Mechanical Engineering, National Institute of Technology, Oita College, Japan, 2College of Science, Rikkyo University, 3Graduate School of Engineering, Osaka University, 4Graduate School of Science, Hokkaido University, 5Department Applied Physics, Okayama University of Science, 6Graduate School of Engineering, Tohoku University
2017-m-07 ( 11:20 – 11:40 )
A Low Cost Azimuthal control method for Stratospheric Balloon Gondolas
Yasuhiro Shoji
Graduate school of Engineering, Osaka University, Japan
2017-m-08 ( 11:40 – 12:00 )
Skyward Rocksanne Program : students’ sounding rocket as technology demonstrator
Stefano Marino, Davide Benini, Alain Carlucci, Edoardo Contini, Matteo Franceschini, Matteo Grandi, Matteo Michele Piazzolla, Davide Orrù, Silvano Seva, Francesco Tesolin
Politecnico di Milano, Italy
2017-m-09 ( 12:00 – 12:20 )
Post Flight Analysis of Sounding Rocket S-310
Takayuki Yamamoto, Satoshi Nonaka, Shunsuke Sato, Nobuaki Ishii
Japan Aerospace Exploration Agency, Japan
[m-3] Atmospheric Science using Sounding Rocket

Session Date June 9 (Fri) 14:00 – 15:00
Room Meeting Room 12
Chairpersons
2017-m-11 ( 14:00 – 14:20 )
Recent Activity of Japanese Sounding Rocket Experiments for the Thermospheric and Ionospheric Study
Takumi Abe1, Shigeto Watanabe2, Mamoru Yamamoto3, Masa-yuki Yamamoto4
1Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan, 2Hokkaido Information University, 3RISH, Kyoto University, 4Kochi University of Technology
2017-m-12 ( 14:20 – 14:40 )
DC Electric Field Measurements near the Sq Current System by S-310-44 Sounding Rocket
Keigo Ishisaka1, Takumi Abe2, Atsushi Kumamoto3, Makoto Tanaka4, Akimasa Yoshikawa5, Hiroki Matsushita5
1Department of Information Systems Engineering, Toyama Prefectural University, Japan, 2JAXA/ISAS, 3Tohoku University, 4Tokai University, 5Kyushu University
2017-m-13 ( 14:40 – 15:00 )
Neutral Wind Measurements by Sounding Rockets
Shigeto Watanabe1, Takumi Abe2, Hiroto Habu2, Yoshihiro Kakinami3, Masayuki Yamamoto4
1Space Information Center, Hokkaido Information University, Japan, 2JAXA/ISAS, 3National Institute of Technology, Tomakomai College, 4Kochi University of Engineering
[m-4] Next Gerenartion Balloon and Payload System

Session Date June 9 (Fri) 16:00 – 17:40
Room Meeting Room 12
Chairpersons
2017-m-14 ( 16:00 – 16:20 )
A trial of developing unique payload system for small student balloons
Masa-yuki Yamamoto, Takamasa Hiratsuka, Hiroaki Fujitsu
Kochi University of Technology, Japan
2017-m-15 ( 16:20 – 16:40 )
Small Satellite Launch System by Aerial Launch Platform
Ting Ting Qiu1, Hiroki Yanagida1, Yuto Ikeda1, Shin Satori1, Ryuichi Mitsuhashi3, Kazuhisa Chiba4, Tomonori Ito2
1Future Industry, Happy Science University, Japan, 2Hakkaido Satellite Co., Ltd, 3Hokkaido University of Science, 4The University of Electro-Communications
2017-m-16 ( 16:40 – 17:00 )
Study of Designing for Combinated Shape Balloon in Stratosphere
Yanchu Yang, Sheng Wang, Luhua Jiang, Jinggang Miao, Donghui Zhang
Center for LTA system research and development, Academy of Opto-Electronics, Chinese Academy of Science, China
2017-m-17 ( 17:00 – 17:20 )
Design and Ground Test of a 6 Meters Pumpkin Super-pressure Balloon
Zhu Rongchen, Wang Sheng, Yang Yanchu, Liu Qiang
Academy of Opti-electronics, Chinese Academy of Sciences, China
2017-m-18 ( 17:20 – 17:40 )
Development of a New Super-Pressure Balloon with a Net for High-Altitude and Long-duration Flights
Daisuke Akita1, Yoshitaka Saito2, Ken Goto2, Kyoichi Nakashino3, Takuma Matsuo4, Kiyoho Matsushima5, Hiroyuki Hashimoto5, Shigeyuki Shimadu6
1Department of Transdisciplinary Science and Engineering, Tokyo Institute of Technology, Japan, 2JAXA/ISAS, 3Department of Aeronautics and Astronautics, Tokai University, 4Department of Mechanical Engineering, Meiji University, 5Fujikura Parachute Company, Ltd., 6Nakada Industrial Company
[n-1] Earth Observation: Advances in Operations and Data Application

Session Date June 7 (Wed) 16:00 – 17:40
Room Meeting Room 15
Chairpersons
2017-n-01 ( 16:00 – 16:20 )
Ant-colony-based Track Coordination for the Planning of Earth Observation Missions
Yi-Yao Yeh1, Sheng-Yi Li2, Feng-Tai Hwang3
1Department of Information Management , R.O.C. Naval Academy, Taiwan, 2Chung Cheng Institute of Technology, National Defense University, 3National Space Organization (NSPO)
2017-n-02 ( 16:20 – 16:40 )
Heuristic Algorithm for Simultaneous Nadir Overpasses Estimation during Metop-A End of Life Phase
Carlos Vera, Pier Luigi Righetti
Flight Operations Division, EUMETSAT, Germany
2017-n-03 ( 16:40 – 17:00 )
A Graph-Theoretic Approach to Optimal Planning of Satellite Downlink Operation
Kazunori Someya1, Takuto Ishimatsu2, Yosuke Nakamura1, Yuya Kakehashi1, Naoki Ishihama1
1Japan Aerospace Exploration Agency, Japan, 2The University of Tokyo
2017-n-04 ( 17:00 – 17:20 )
The Importance of Earth Observations and Data Collaboration within Environmental Intelligence Supporting Arctic Research
Joseph C Casas
Science and Technology Office, NASA Marshall Space Flight Center, USA
2017-n-05 ( 17:20 – 17:40 )
A Comprehensive Study of Dengue Fever Outbreaks in Taiwan Using Remote Sensing, Unmanned Aerial Vehicles, Big Data, and Open Data
Sumiko Anno1, Ming-An Lee2, Jesse Yang2, Kuan-Tsung Chang3, Yi Chang4, Takeo Tadono5, Yusuke Kobayashi6, Hiroki Kai6, Tamotsu Igarashi6
1Shibaura Institute of Technology, Japan, 2National Taiwan Ocean University, 3Minghsin University of Science and Technology, 4National Cheng- Kung University, 5JAXA, 6RESTEC
[n-2] Earth Observation: Advances in Optical Imagers and Radiometers (1)

Session Date June 8 (Thu) 9:00 – 10:20
Room Meeting Room 11
Chairpersons
2017-n-06 ( 9:00 – 9:20 )
Similarity of the characteristic terrain by various geospatial information - Risk of disaster in Tokyo -
Toshiro Sugimura1, Kuniaki Isobe2, Tetsuji Yamamoto2
1College of Industrial Technology, Nihon University, Japan, 2Think and Earth Science
2017-n-07 ( 9:20 – 9:40 )
Urban Change Monitoring in Developing Countries Based on Deep Learning Technique by Utilizing Time Series Imageries of the SAR and Optical Satellites
Shota Iino, Riho Ito, Tomoyuki Imaizumi, Shuhei Hikosaka
PASCO CORPORATION, Japan
2017-n-09 ( 9:40 – 10:00 )
SLATS and Future Vision – New view positions of Earth Observation-
Hirokazu HOSHINO, Masanori Sasaki
SLATS Project Team, Space Technology Directorate I, Japan Aerospace Exploration Agancy, Japan
2017-n-10 ( 10:00 – 10:20 )
On-board Satellite Imagery Classification using Convolutional Neural Networks
Kei Ohta1, Takehiko Koike1, Yoichi Yatsu3, Saburo Matunaga2
1Department of Mechanical and Aerospace Engineering, Tokyo Institute of Technology, Japan, 2Department of Mechanical Engineering, Tokyo Institute of Technology, 3Department of Physics, Tokyo Institute of Technology
[n-3] Earth Observation: Advances in Optical Imagers and Radiometers (2)

Session Date June 8 (Thu) 11:00 – 12:40
Room Meeting Room 11
Chairpersons
2017-n-11 ( 11:00 – 11:20 )
New technique to take a high-resolution night view of the earth from a micro satellite
DAT QUOC DAO, Shinichiro Haruyama
Keio University, Viet Nam
2017-n-12 ( 11:20 – 11:40 )
Research and Simulation Experiment on Space Based Digital TDI Imaging Technique
Zhuang Xu Xia, Ruan Ning juan, He Jin ping, Liu Yu chen
BISME, BISME, China
2017-n-13 ( 11:40 – 12:00 )
Wavefront correction using deformable mirror for extended scene: experimental results
Norihide Miyamura1, Nobutada Sako2
1Department of Interdisciplinary Science and Engineering, Meisei University, Japan, 2Canon Electronics Inc.
2017-n-14 ( 12:00 – 12:20 )
Aperture Partitioning for Bispectrum Speckle Imaging
Lauren Hayley Schatz1, Thomas R Swindle3, Brandoch Calef2, Steve Jefferies2
1Optical Science, University of Arizona, USA, 2Boeing Company, 3Airforce Maui Optical and Supercomputing Laboratory
2017-n-15 ( 12:20 – 12:40 )
Overview of Advanced optical satellite
Haruyoshi Katayama, Eri Kato, Tomoya Niwa, Hidenori Watarai, Masakazu Sagisaka
Space Technology Directorate I, Japan Aerospace Exploration Agency, Japan
[n-4] Earth Observation: Advances in Optical Imagers and Radiometers (3)

Session Date June 8 (Thu) 14:00 – 15:40
Room Meeting Room 11
Chairpersons
2017-n-16 ( 14:00 – 14:20 )
Simulated Image Generation for the Advanced Optical Satellite
Takeo Tadono, Mitsunori Ishihara, Ayano Oka, Hidenori Watarai
JAXA, Japan
2017-n-17 ( 14:20 – 14:40 )
Analysis of the land surface temperature characteristics in Tokyo by LANDSAT and high-resolution satellite data
Yasunori Nakayama1, Hideki Hashiba2
1Department of Earth & Environmental Sciences, Nihon University, Japan, 2Department of Civil Engineering, Nihon University
2017-n-18 ( 14:40 – 15:00 )
Mission Planning and System Design of HISA : A Hyperspectral Imagin Satellite for Australian Agriculture
EuGene Kim, Xiaofeng Wu, Warwick Holmes
School of Aerospace, Mechanical, Mechatronics Engineering, The University of Sydney, Australia
2017-n-19 ( 15:00 – 15:20 )
Development of land products using SGLI data
Toshiyuki Kobayashi1, Hiroshi Murakami1, Yoshiaki Honda2, Koji Kajiwara2, Yuhsaku Ono2, Masao Moriyama3, Hideki Kobayashi4, Kenlo Nasahara5, Risa Miyazaki1, Masahiro Hori1
1Japan Aerospace Exploration Agency (JAXA), Japan, 2Chiba University, 3Nagasaki University, 4Japan Agency for Marine-Earth Science and Technology (JAMSTEC), 5University of Tsukuba
2017-n-20 ( 15:20 – 15:40 )
GCOM-C data validation plan for land, atmosphere, ocean, and cryosphere
Masahiro Hori1, Hiroshi Murakami1, Risa Miyazaki1, Yoshiaki Honda2, Kenlo Nasahara3, Koji Kajiwara2, Takashi Y. Nakajima4, Hitoshi Irie2, Mitsuhiro Toratani4, Toru Hirawake5, Teruo Aoki6
1Earth Observation Research Center, Japan Aerospace Exploration Agency, Japan, 2Chiba Univ., 3Univ. of Tsukuba, 4Tokai Univ., 5Hokkaido Univ., 6Okayama Univ.
[n-5] Earth Observation: Advances in SARs and Compact Cameras

Session Date June 8 (Thu) 16:00 – 17:40
Room Meeting Room 11
Chairpersons
2017-n-21 ( 16:00 – 16:20 )
The current on-orbit status of the Compact Infrared Camera (CIRC) onboard CALET
Ayaka Kumeta1, Michito Sakai1, Koji Nakau2, Yukinori Nakajima1, Toshiyoshi Kimura1
1Research and Development Directorate , Japan Aerospace Exploration Agency, Japan, 2Space Technology Directorate I, Japan Aerospace Exploration Agency
2017-n-22 ( 16:20 – 16:40 )
Application Demonstration through System and Algorithm Development for Wildfire Monitoring utilizing CIRC (Compact Infrared Camera)
KOJI NAKAU, Junichiro Ishizawa, Michito Sakai, Ayaka Kumeta, Toshiyoshi Kimura
JAXA, Japan
2017-n-23 ( 16:40 – 17:00 )
Deforestation detection using ALOS-2/PALSAR-2 imagery in “JICA-JAXA Forest Early Warning System in the Tropics (JJ-FAST)”
Masato Hayashi1, Tomohiro Watanabe1, Yutaka Kaneko1, Manabu Watanabe2, Christian Koyama2, Masanobu Shimada2, Takashi Ogawa3, Keiko Ishii3, Tomohiko Higashiuwatoko3, Mari Miura4, Hiroaki Okonogi4, Kanako Adachi4, Kenichi Shishido4
1Japan Aerospace Exploration Agency (JAXA), Japan, 2Tokyo Denki University, 3Remote Sensing Technology Center of Japan (RESTEC), 4Japan International Cooperation Agency (JICA)
2017-n-24 ( 17:00 – 17:20 )
ALOS/PALSAR analysis of surface deformation in the Pacific side of Chiba prefecture
Tomohito Asaka1, Takashi Nonaka2, Hideki Hashiba3, Keishi Iwashita2, Toshiro Sugimura1
1Department of Civil Engineering, College of Industrial Technology, Nihon University, Japan, 2Department of Sustainable Engineering, College of Industrial Technology, Nihon University, 3Department of Civil Engineering, College of Science and Technology, Nihon University
2017-n-25 ( 17:20 – 17:40 )
Robust Approach for Correlated Baseline Data of ALOS time-series Interferometry
Takuma Anahara
Earth Observation Research Center, JAXA, Japan
[n-6] Earth Observation: Advances in Meteorological Instruments

Session Date June 9 (Fri) 9:00 – 10:40
Room Meeting Room 11
Chairpersons
2017-n-26 ( 9:00 – 9:20 )
Prime mission results of the Dual-frequency Precipitation Radar on the Global Precipitation Measurement core spacecraft.
Kinji Furukawa1, Tomomi Nio2, Takuji Kubota3, Riko Oki3, Toshio Iguchi4
1GPM/DPR project team, JAXA, Japan, 2Satellite Applications and Operations Center, JAXA, 3Earth Observation Research Center, JAXA, 4National Institute of Information and Communications Technology
2017-n-27 ( 9:20 – 9:40 )
Drop Size Distribution observed by Dual-frequency Precipitation Radar onboard Global Precipitation Measurement core satellite
Moeka Yamaji1, Takuji Kubota1, Atsushi Hamada2, Yukari Takayabu2, Riko Oki1
1Earth Observation Research Center, Japan Aerospace Exploration Agency, Japan, 2 Atmosphere and Ocean Research Institute, The University of Tokyo
2017-n-28 ( 9:40 – 10:00 )
Quasi-realtime version of the Global Satellite Mapping of Precipitation (GSMaP_NOW) over the Himawari-8 region
Takuji Kubota1, Misako Kachi1, Yoriko Arai2, Moeka Yamaji1, Riko Oki1
1Earth Observation Research Center, Japan Aerospace Exploration Agency, Japan, 2Remote Sensing Technology Center of Japan
2017-n-29 ( 10:00 – 10:20 )
JAXA Himawari Monitor and its Synergies to the Earth Observation Satellites
Misako Kachi, Maki Kikuchi, Mayumi Yoshida, Takashi Nagao, Yukio Kurihara, Hiroshi Murakami
Earth Observation Research Center, Japan Aerospace Exploration Agency, Japan
2017-n-30 ( 10:20 – 10:40 )
Multi Frame Image Processing of Himawari-8/AHI Data
Toshiro Sugimura, Yuuki Uchida, Sadayoshi Aoyama, Tomohito Asaka, Keishi Iwashita
College of Industrial Technology, Nihon University, Japan
[n-7] Earth Observation: Advances in Microwave Radiometers

Session Date June 9 (Fri) 11:00 – 12:20
Room Meeting Room 11
Chairpersons
2017-n-31 ( 11:00 – 11:20 )
Overview and Updates of GCOM-W and AMSR2 for Climate and Water Studies
Misako Kachi1, Takashi Maeda1, Hiroyuki Tsutsui1, Taikan Oki2
1Earth Observation Research Center, Japan Aerospace Exploration Agency, Japan, 2The University of Tokyo
2017-n-32 ( 11:20 – 11:40 )
Precipitable Water Vapor Retrieval over Land from GCOM-W/AMSR2
Masahiro Kazumori
Department of Forecast, Japan Meteorological Agency, Japan
2017-n-33 ( 11:40 – 12:00 )
Current status of the AMSR2 standard product for soil moisture content and snow depth
Tsutsui Hiroyuki, Kachi Misako, Maeda Takashi
Earth Observation Research Center, Japan Aerospace Exploration Agency, Japan
2017-n-35 ( 12:00 – 12:20 )
Study on constructing consistent dataset from multiple space-based microwave radiometers
Keiji Imaoka1, Misako Kachi2
1Media and Information Technology Center, Yamaguchi University, Japan, 2Earth Observation Research Center, Japan Aerospace Exploration Agency
[n-8] Earth Observation: Advances in Spectrometers and Lidars (1)

Session Date June 9 (Fri) 14:00 – 15:40
Room Meeting Room 11
Chairpersons
2017-n-36 ( 14:00 – 14:20 )
Overview and Status of Vegetation Lidar Mission ‘MOLI’
Mitsuhashi Rei1, Jumpei Murooka1, Daisuke Sakaizawa1, Tadashi Imai1, Toshiyoshi Kimura1, Kazuhiro Asai2
1Department of Sensor System Research Group, Japan Aerospace Exploration Agency, Japan, 2Tohoku Institute of Technology
2017-n-37 ( 14:20 – 14:40 )
Imaging spectrometer with an agile pointing system to monitor global and regional greenhouse gas flux and target local emission
Akihiko Kuze, Hiroshi Suto
Earth Observation Research Center, Japan Aerospace Exploration Agency, Japan
2017-n-38 ( 14:40 – 15:00 )
Development of GOSAT Air Pollution Watch
Yoshito Sawada1, Yu Oishi2, Akihide Kamei1, Akihiro Uchiyama1, Tsuneo Matsunaga1
1National Institute for Environmental Studies, Japan, 2Tokai University
2017-n-39 ( 15:00 – 15:20 )
Multi-layer Retrievals of Greenhouse Gases from a Combined Use of TANSO-FTS SWIR and TIR
Nobuhiro Kikuchi1, Akihiko Kuze1, Fumie Kataoka2, Kei Shiomi1, Makiko Hashimoto1, Hiroshi Suto1, Robert Knuteson3, Laure Iraci4, Emma Yates4, Warren Gore4, Tomoaki Tanaka4
1Japan Aerospace Exploration Agency, Japan, 2Remote Sensing Technology Center of Japan, 3University of Wisconsin, 4NASA Ames Research Center
2017-n-40 ( 15:20 – 15:40 )
Investigation of the long-term change of the TANSO-FTS pointing characteristics for a future agile pointing mechanism
Jun Yoshida2, Nobuo Kenmochi1, Hiroshi Sugita1, Yoshifumi Nodomi1, Shingo Obara2, Akira Sasaki2, Akihiko Kuze2
1NEC Corporation, 2JAXA, Japan
[n-9] Earth Observation: Advances in Spectrometers and Lidars (2)

Session Date June 9 (Fri) 16:00 – 16:40
Room Meeting Room 11
Chairpersons
2017-n-41 ( 16:00 – 16:20 )
Characterizing on-orbit electrical performance of TANSO onboard GOSAT using its engineering models in the laboratory
Hiroshi Suto1, Jun Yoshida2, Takahiro Kawashima2, Kei Shiomi1, Akihiko Kuze1
1JAXA, Japan, 2NEC Corporation
2017-n-42 ( 16:20 – 16:40 )
Calibration and validation activities for GOSAT collaborated with OCO-2
Kei Shiomi1, Akihiko Kuze1, Nobuhiro Kikuchi1, Makiko Hashimoto1, Hiroshi Suto1, Fumie Kataoka2, Takahito Igarashi2, Shuji Kawakami1
1Earth Observation Research Center, Japan Aerospace Exploration Agency, Japan, 2Remote sensing Technology Center of Japan
[p-1] Space Life Science (1)

Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 12
Chairpersons
2017-p-01 ( 9:00 – 9:25 )
Voluntary-Vaporization Enhances Cooling Effects for Extravehicular Activity.
Kunihiko Tanaka1, Daiki Nagao2, Kosuke Okada2, Koji Nakamura1
1Graduate School of Health and Medicine, Gifu University of Medical Science, Japan, 2Department of Radiological Technology, Gifu University of Medical Science
2017-p-02 ( 9:25 – 9:50 )
Electrical Stimulation of the Antagonist Muscle Added to Cycling Exercise Interval Training Improves Oxygen Uptake and Muscle Strength
Masayuki Omoto1, Yoshio Takano2, Hiroo Matsuse1, Ryuki Hashida1, Takeshi Nago1, Yoshihiko Tagawa1, Naoto Shiba1
1Department of rehabilitaion, University of Kurume, Japan, 2International University Health and Welfare
2017-p-03 ( 9:50 – 10:15 )
Trial of the stress-related index measurement under the confined environmental stress
Yuichi Oi1, Yasuhito Hirai1, Shotaro Doki2, Yuh Ohtaki3, Daisuke Hori4, Christina Sylvia Andrea3, Shin-ichiro Sasahara1, Tamaki Saito1, Ichiyo Matsuzaki1, Ichiyo Matsuzaki5
1Faculty of medicine, University of Tsukuba, Japan, 2Hospital Bando, 3Graduate School of Comprehensive Human Sciences, University of Tsukuba, 4Department of Environmental and Preventive Medicine, Kanazawa University Graduate School of Medical Sciences, 5International Institute for Integrative Sleep Medicine, University of Tsukuba
2017-p-04 ( 10:15 – 10:40 )
Development of Mouse Habitat Unit for Individual Rearing Used in International Space Station
Yusuke Hagiwara1, Makoto Ohira1, Hiroaki Kodama1, Hirochika Murase1, Toshimasa Ochiai1, Hiroyasu Mizuno2
1Space Systems Engineering Department, Mitsubishi Heavy Industries, Ltd., Japan, 2Japan Aerospace Exploration Agency
[p-2] Space Life Science (2)

Session Date June 6 (Tue) 11:00 – 12:15
Room Meeting Room 12
Chairpersons
2017-p-06 ( 11:00 – 11:25 )
Medical Mycology in Space
Koichi MAKIMURA
Laboratory of Space and Environmental Medicine, Graduate school of Medicine, Teikyo University, Japan
2017-p-07 ( 11:25 – 11:50 )
Is virulence factor of skin microbiota, Malassezia changed in a microgravity environment ? -Malassezia is predominant fungal microbiota in skin of astronauts residing in the ISS-
Takashi Sugita1, Ayumi Watanabe1, Otomi Cho1, Sanae Kurakado1, Noriaki Ishioka2
1Department of Microbiology, Meji Pharmaceutical University, Japan, 2Institute of Space and Astronautical Science, JAXA
2017-p-08 ( 11:50 – 12:15 )
Bacterial Horizontal Gene Transfer Frequencies under Simulated Microgravity
Tomoaki Ichijo1, Takehiko Kenzaka2, Masao Nasu2, Katsuji Tani2
1Graduate School of Pharmaceutical Sciences, Osaka University, Japan, 2Faculty of Pharmacy, Osaka Ohtani University
[p-3] Space Life Science (3)

Session Date June 6 (Tue) 14:00 – 15:40
Room Meeting Room 12
Chairpersons
2017-p-09 ( 14:00 – 14:25 )
Performance evaluation of new devices to synchronize X-ray or heavy-ion irradiation and simulated microgravity for space radiation research
Akihisa Takahashi1, Hiroko Ikeda1, Hikaru Souda1, Anggraeini Puspitasari2, Kathryn D. Held3, Jun Hidema4, Takeshi Nikawa5, Yukari Yoshida1, Tatsuaki Kanai1
1Gunma University Heavy Ion Medical Center, Japan, 2Gunma University Initiative for Advanced Research, 3Massachusetts General Hospital/Harvard Medical School, 4Graduate School of Life Sciences, Tohoku University, 5Institute of Medical Nutrition, Tokushima University Graduate School
2017-p-10 ( 14:25 – 14:50 )
Research on the effects of simulated microgravity on UV sensitivity of plant
Jun Hidema1, Mika Teranishi1, Masanori Izumi1, Sakuya Nakamura1, Akihisa Takahashi2
1Graduate School of Life Sciences, Tohoku University, Japan, 2Gunma University Heavy Ion Medical Center
2017-p-11 ( 14:50 – 15:15 )
Stress-Induced Mitochondrial Fragmentation Impaired Movement in C. elegans
Atsushi Higashitani, Kenta Monma, Surabhi Sudevan, Rui Isaka
Graduate School of Life Sciences, Tohoku University, Japan
2017-p-12 ( 15:15 – 15:40 )
Gravity-induced Re-localization of CsPIN1 for Gravimorphogenesis in Cucumber Seedlings
Hideyuki Takahashi1, Chiaki Yamazaki1, Nobuharu Fujii1, Yutaka Miyazawa2, Motoshi Kamada3, Haruo Kasahara4, Ikuko Osada4, Toru Shimazu5, Yasuo Fusejima5, Akira Higashibata6, Takashi Yamazaki7, Noriaki Ishioka8
1Graduate School of Life Sciences, Tohoku University, Japan, 2Faculty of Science, Yamagata University, 3Advanced Engineering Services Co., Ltd., 4Japan Manned Space Systems Co., 5Japan Space Forum, 6JEM Utilization Center, Japan Aerospace Exploration Agency, 7Graduate School of Medicine, Teikyo University, 8Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
[p-4] Space Life Science (4)

Session Date June 6 (Tue) 16:00 – 17:40
Room Meeting Room 12
Chairpersons
2017-p-13 ( 16:00 – 16:25 )
Water status of plants under low gravity conditions
Yoshiaki Kitaya, Hiroaki Hirai, Ayako Tokuda, Sachiko Yano
Life and Environmental Sciences, Osaka Prefecture University, Japan
2017-p-14 ( 16:25 – 16:50 )
Evaluation of Taste for Super-Dwarf Rice as Space Food
Hiroaki Hirai, Yoshiaki Kitaya
Graduate School of Life and Environmental Sciences, Osaka Prefecture University, Japan
2017-p-15 ( 16:50 – 17:15 )
APPLICATION TO SPACE FOODS OF THE DISASTER FOOD
Naomi Katayama1,2, Yukimi Okano2, Shoko Kondo2, Yui Nakayama2
1Department of Food Science and Nutrition, Nagoya Women’s University, Nagoya, Japan, 2Division of Food Science and Nutrition, Graduate School of Nagoya Women’s University, Nagoya, Japan
2017-p-16 ( 17:15 – 17:40 )
Sensuality test result for application to space foods of the disaster food
Naomi Katayama1,2, Shoko Kondo1, Yui Nakayama1
1Division of Food Science and Nutrition, Graduate School of Nagoya Women’s University, Nagoya, Japan, 2Department of Food Science and Nutrition, Nagoya Women’s University, Nagoya, Japan
[q-1] Space Solar Power System

Session Date June 9 (Fri) 9:00 – 10:00
Room Meeting Room 13
Chairpersons
2017-q-01 ( 9:00 – 9:20 )
Current Status of the development for Future Space Solar Power System
Shoichiro Mihara1, Kazuhiko Maekawa1, Shuji Nakamura1, Kenji Sasaki1, Yukihiro Homma2, Koji Nakayam2, Yuichiro Ozawa3, Kenichi Anma4, Shigeo Kawasaki5, Koji Tanaka5
1Japan Space Systems, Japan, 2Mitsubishi Electric Corporation, 3IHI Aerospace Co.,LTD, 4Mitsubishi Heavy Industry, 5JAXA
2017-q-02 ( 9:20 – 9:40 )
Current Research on Laser Wireless Power Transmission Technology
Hiroaki Suzuki, Kazuhisa Kitakura, Hiroyuki Yoshida
Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency, Japan
2017-q-03 ( 9:40 – 10:00 )
Wireless Power Transmission for Space-based Solar Power with Distributed Electric Grid
Frank Edward Little
Texas A&M University, USA
[q-2] Technology Development for Solar Power Satellite

Session Date June 9 (Fri) 11:00 – 12:00
Room Meeting Room 13
Chairpersons
2017-q-04 ( 11:00 – 11:20 )
Toward a Demonstration of Space Solar
Paul Jaffe
U.S. Naval Research Laboratory, USA
2017-q-05 ( 11:20 – 11:40 )
A Technology for Mass-Produced Array Antennas: Realization of an Arbitrary Field Distribution with Uniform Element Excitation
Tadashi Takano, Kuniaki Shibata, Toshihiro Naganawa, Kenji Saegusa
Department of Electronic Engineering, Nihon University, Japan
2017-q-06 ( 11:40 – 12:00 )
Experiments on Direction Finding and Beam Control System of Multi-Antenna Panel Structure of Power Generation and Transmission System for Solar Power Satellite
Mudassir Raza1, Koji Tanaka2, Koji Takeda3, Misato Yoneyama4, Shotaro Katano1
1Dept. of Space and Astronautical Sciences, SOKENDAI (The Graduate University for Advanced Studies), Japan, 2ISAS/JAXA, 3Delft University of Technology, 4Tokyo University of Science, Suwa
[q-3] Space Power System I

Session Date June 9 (Fri) 14:00 – 15:00
Room Meeting Room 13
Chairpersons
2017-q-08 ( 14:00 – 14:20 )
Applications of Linear Programming Techniques to Satellite Power Management and Scheduling
Joshua Julian Robert Critchley-Marrows, Martin Isacsson, Anges Gårdebäck
KTH Royal Technology Institute, Australia
2017-q-09 ( 14:20 – 14:40 )
Sensor-Less Control for Switch-Regulated Energy Harvester using Alternate State-Estimators
Yuta Yamamoto, Yushin Hara, Kanjuro Makihara
Department of aerospace engineering, Tohoku university, Japan
2017-q-10 ( 14:40 – 15:00 )
Dynamic solar simulator for small satellite simulations
Marco Antonio Saavedra Lautensach
Department of electrical engineering, School of Engineering , National Autonomous University of Mexico, Mexico
[q-4] Space Power System II

Session Date June 9 (Fri) 16:00 – 17:20
Room Meeting Room 13
Chairpersons
2017-q-11 ( 16:00 – 16:20 )
Design and Implementation of a High Powered Electrical Power Subsystem for AMMEQ-1, a 3U CubeSat
Trevor Hocksun Kwan1, Xiaofeng Wu1, Eugene Kim1, Robert Bedington2, Xueliang Bai2, Alex Ling2
1School of Aerospace, Mechanical and Mechatronics Engineering, University of Sydney, Australia, 2Centre for Quantum Technologies, Singapore
2017-q-12 ( 16:20 – 16:40 )
Evaluation of orbit data of electrical power system of deep space probe Shinen2
Jesus Gonzalez-Llorente1, Kei-ichi Okuyama1, Bianca Szasz1, Sidi Bendoukha1, Isai Fajardo1, Masanori Nishio2
1Department of Applied Sciences for Integrated Systems Engineering, Kyushu Institute of Technology, Japan, 2Aichi University of Technology
2017-q-13 ( 16:40 – 17:00 )
Power Resource Allocation in Electrically Closed System using Hybrid Control under Multiagent System
Sho Ohtani1, Osamu Mori2
1Department of Aeronautics and Astronautics, University of Tokyo, Japan, 2Japan Aerospace Exploration Agency
2017-q-14 ( 17:00 – 17:20 )
The Failure Rate Calculation Method for High Power Devices in Low Earth Orbit
Erdenebaatar Dashdondog
Kyushu Institute of Technology, Japan
[r-1] Space Environment (Radiation)

Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 13
Chairpersons
2017-r-01 ( 9:00 – 9:20 )
Space radiation measurements using a small deep space probe in the Sun-Earth environment
Isai Fajardo Tapia1, Kei-Ichi Okuyama1, Bianca Adina Szasz1, Sidi Ahmed Bendoukha1, Jesus Gonzalez-Llorente1, Doug Holland2, Prem-kumar Saganti3
1Department of Applied Sciences for Integrated Systems Engineering, Kyushu Institute of Technology, Japan, 2NASA Johnson Space Center, Houston, USA, 3Prairie View A&M University, Prairie View, Texas, USA
2017-r-02 ( 9:20 – 9:40 )
Using Electromagnetic Protection in the Van Allen radiation belt compared with material protection
Shingo Motodani
Mechanical and Aerospace Engineering, University of Kyushu, Japan
2017-r-03 ( 9:40 – 10:00 )
PHITS Simulations for Development of Space Radiation Shielding Materials
Aki Goto, Kazunori Shimazaki, Yugo Kimoto, Haruhisa Matsumoto, Aiko Nagamatsu
Japan Aerospace Exploration Agency, Japan
2017-r-04 ( 10:00 – 10:20 )
The status of the Heavy Ion Telescope on the ISS/JEM-EF
Haruka Ueno, Haruhisa Matsumoto, Kiyokazu Koga
JAXA, Japan
2017-r-05 ( 10:20 – 10:40 )
A Pulsed Supersonic Valve Aimed for Martian Atmospheric Simulation
Ryota Okura1, Minoru Iwata2, Chee Sze Keat3, Kumiko Yokota1, Masahito Tagawa1
1Department of Engineering, University of Kobe, Japan, 2Kyushu Institute of Technology, 3Mechano Transformer Corp.
[r-2] Space Environment (Charging 1)

Session Date June 6 (Tue) 11:00 – 12:40
Room Meeting Room 13
Chairpersons
2017-r-06 ( 11:00 – 11:20 )
Mission results of Arc Event Generator and Investigation Satellite “HORYU-IV”
Hiroshi Fukuda1, HORYU-IV member2, Kazuhiro Toyoda2, Mengu Cho2
1Department of engineering (Electrical and Electronics), Kyushu Institute of Technology, Japan, 2Laboratory of Spacecraft Environment Interaction Engineering, Kyushu Institute of Technology
2017-r-07 ( 11:20 – 11:40 )
Simulation of Lunar Surface Charging, Electric Field and Dust Lofting with Attitude Control of a CubeSat Mission
Necmi Cihan Orger, Jose Rodrigo Cordova Alarcon, Kazuhiro Toyoda, Mengu Cho
Laboratory of Spacecraft Environment Interaction Engineering, Kyushu Institute of Technology, Japan
2017-r-08 ( 11:40 – 12:00 )
Assessment of Spacecraft Surface Charging in Worst GEO Environmental Conditions
Masao Nakamura1, Shinya Nakamura1, Kazuhiro Toyoda2
1Department of Aerospace Engineering, Osaka Prefecture University, Japan, 2Department of Electrical Engineering and Electronics, Faculty of Engineering, Kyushu Institute of Technology
2017-r-09 ( 12:00 – 12:20 )
Comparison Between Surface Charging Event from Michibiki (QZS) Satellite and Space Environment Data from Global MHD Simulation
Tsutomu Nagatsuma1, Haruhisa Matsumoto2, Yasubumi Kubota1, Aoi Nakamizo1, Kiyokazu Koga2
1Space Environment Laboratory, Applied Electromagnetic Research Institute, National Institute of Information and Communications Technology, Japan, 2Japan Aerospace Exploration Agency
2017-r-10 ( 12:20 – 12:40 )
A Simulation of Plasma Layer for Re-entry Radio Blackout Mitigation
Sidi Ahmed Bendoukha, Kei-ichi Okuyama, Szasz Bianca
Department of Applied Sciences and Integrated System Engineering., Kyushu Institute of Technology, Japan
[r-3] Space Environment (Charging 2)

Session Date June 6 (Tue) 14:00 – 15:20
Room Meeting Room 13
Chairpersons
2017-r-11 ( 14:00 – 14:20 )
The relationship between accumulated charge in electron beam irradiated fluorine insulating materials
Masahito Miyoshi
Tokyo City University, Japan
2017-r-12 ( 14:20 – 14:40 )
Development of APD (Avalanche PhotoDiode) type electron measurement unit for space use focused on the satellite charging
Kiyokazu Koga, Haruka Ueno
Research and Development Directorate, Japan Aerospace Exploration Agency, Japan
2017-r-13 ( 14:40 – 15:00 )
Evaluation of electron-emitting film for satellite charging mitigation (ELFs Charm)
Atomu Tanaka1, Jean-Charles Mateo Velez2, Sarah Dadouch2, Teppei Okumura3, Kenji Sakamoto1, Minoru Iwata1, Kazuhiro Toyoda1, Mengu Cho1
1Kyushu institute of technology, Japan, 2ONERA, 3JAXA
2017-r-14 ( 15:00 – 15:20 )
Change of secondary electron emission yield of insulating material by high energy electron beam irradiation
Natsumi Sato
Measurement and Electric Machine Control Laboratory, Tokyo City University, Japan
[r-4] Materials

Session Date June 6 (Tue) 16:00 – 17:40
Room Meeting Room 13
Chairpersons
2017-r-15 ( 16:00 – 16:20 )
Accelerating Effect of Atomic Oxygen-induced Polyimide Degradation due to Simultaneous Collision of Chemically Inert Molecules
Kazuki Kita1, Yusuke Fujimoto1, Yuki Yamasaki1, Minoru Iwata2, Kumiko Yokota1, Masahito Tagawa1
1Department of engineering, University of Kobe, Japan, 2Department of engineering, Kyushu Institute of Technology
2017-r-16 ( 16:20 – 16:40 )
Mass-loss of FEP/Ag Films in Sub-Low Earth Orbit Space Environment
Yusuke Fujimoto1, Kazuki Kita1, Yasuko Koshiba2, Kenji Ishida2, Minoru Iwata3, Kumiko Yokota1, Masahito Tagawa1
1Department of mechanical engineering, University of Kobe, Japan, 2Department of chemical science and engineering, University of Kobe, 3Department of engineering, Kyushu Institute of Technology
2017-r-17 ( 16:40 – 17:00 )
Surface Analysis Results of Atomic Oxygen Protective Coating Film
Miyuki Waki, Yugo Kimoto
Research and Development Directorate, Japan Aerospace Exploration Agency, Japan
2017-r-18 ( 17:00 – 17:20 )
Relationship between electron beam irradiation dose and photoelectron emission characteristics of electron beam irradiated insulating materials
Kotaro Suzuki
Measurement and Electric Machine Control Laboratory, Tokyo City University, Japan
2017-r-19 ( 17:20 – 17:40 )
Recovery of solar absorptance change by the ultraviolet rays in the atmosphere storage
Kazuyuki Mori, Yugo Kimoto
Research and Development Directorate, JAXA, Japan
[r-5] Space Debris (Observation)

Session Date June 7 (Wed) 9:00 – 10:00
Room Meeting Room 13
Chairpersons
2017-r-21 ( 9:00 – 9:20 )
Effective Search Strategy Applicable for Narrow Field-of-view Telescope
Yuki Itaya, Koki Fujita, Toshiya Hanada
Department of Aeronautics and Astronautics, Kyushu University, Japan
2017-r-22 ( 9:20 – 9:40 )
Detection of LEO Objects Using Large CMOS Sensor
Toshifumi Yanagisawa, Hirohisa Kurosaki
Research and Development Directorate, Japan Aerospace Exploration Agency, Japan
2017-r-24 ( 9:40 – 10:00 )
A New Method for the Identification of Objects Detected in Beam-park Experiments
Hai Jiang, Jing Liu, Yang Li, Yao Zhang, Haowen Cheng
National Astronomical Observatories, Chinese Academy of Sciences, China
[r-6] Space Debris (Observation, Rotation, In-situ Measurement)

Session Date June 7 (Wed) 11:00 – 12:40
Room Meeting Room 13
Chairpersons
2017-r-25 ( 11:00 – 11:20 )
Application of Image Restoration in Optical Space Debris Observations
Rongyu Sun
Division of Applied Celestial Mechanics and Space Object and Debris Research, Purple Mountain Observatory, China
2017-r-26 ( 11:20 – 11:40 )
The YORP Effect on Defunct Earth Orbiting Satellites
Daniel Jay Scheeres
Aerospace Engineering Sciences, University of Colorado, USA
2017-r-27 ( 11:40 – 12:00 )
Attitude States of Space Debris determined from Optical Light Curve Observations
Thomas Schildknecht, Jiri Silha, Jean-Noel Pittet, Abdul Rachman
Astronomical Institute, University of Bern, Switzerland
2017-r-28 ( 12:00 – 12:20 )
Measurment of Momentum to Move with Hypervelocity Impacts of Projectile
Koichi Hayashi1, Masahiro Nishida2, Hirohisa Kurosaki3, Toshifumi Yanagisawa3, Masumi Higashide3
1Department of Electronic Mechanical Engineering, National Institute of Technology, Toba College, Japan, 2Nagoya Institute of Technology, 3JAXA
2017-r-29 ( 12:20 – 12:40 )
Estimation of orbital parameters of broken-up objects from in-situ debris measurement
Yutaka Kodama, Koki Fujita, Toshiya Hanada
Aeronautic and astronautic, Kyushu university, Japan
[r-7] Space Debris (Modelling)

Session Date June 7 (Wed) 16:00 – 17:40
Room Meeting Room 13
Chairpersons
2017-r-30 ( 16:00 – 16:20 )
Environmental Estimation on Sub-millimeter-size Debris using In-situ Measurement Data
Masahiro Furumoto1, Shin’ya Nakano2, Koki Fujita1, Toshiya Hanada1
1Department of Aeronautics and Astronautics, Kyushu University , Japan, 2Institute of Statistical Mathematics
2017-r-31 ( 16:20 – 16:40 )
Evaluation of space debris mitigation measures using a debris evolutionary model
Satomi Kawamoto2, Takayuki Hirai1, Shiki Kitajima2, Shuji Abe2, Toshiya Hanada2
1Research and Development Directorate, Japan Aerospace Exploration Agency, 2Kyushu University, Japan
2017-r-32 ( 16:40 – 17:00 )
Spacecraft Break-up Models for the Atmospheric Re-entry from Highly Eccentric and Interplanetary Trajectories
Stijn Jan Jo Lemmens1, Jan Siminski1, Francesca Letizia2, Quirin Funke1, Klaus Merz1
1Space Debris Office, European Space Agency, Germany, 2University of Southampton
2017-r-33 ( 17:00 – 17:20 )
Development of an Orbital Model for Small-Sized Space Debris Considering Electromagnetic Fields around the Earth
Keisuke Akari
Research Institute for Sustainable Humanosphere, Kyoto University, Japan
2017-r-34 ( 17:20 – 17:40 )
Crater Shape and Ejecta Size from Pure Aluminum Due to Hypervelocity Impact
Yushiro Mozaki2, Masahiro Nishida1, Hiroyuki Yamada2
1Department of Mechanical Engineering, Nagoya Institute of Technology, 2Department of Mechanical Engineering, National Defense Academy of Japan, Japan
[r-8] Space Debris (Protection)

Session Date June 8 (Thu) 9:00 – 10:20
Room Meeting Room 13
Chairpersons
2017-r-35 ( 9:00 – 9:20 )
Ballistic Experiment of LPSO-type Magnesium Plate Target
Fumiya Kodama1, Masahiro Nishida1, Kaito Ishida1, Koichi Hayashi2, Yasuhiro Akahoshi3, Kazuyuki Hokamoto4, Tsuyoshi Mayama4, Michiaki Yamasaki4, Yoshihito Kawamura4
1Nagoya Institute of Technology, Japan, 2Toba College, 3Kyushu Institute of Technology, 4Kumamoto University
2017-r-36 ( 9:20 – 9:40 )
Effects of Impact Angles on Ballistic Limit of Ultra-High-Molecular-Weight Polyethylene Fiber Fabrics
Junya Fuchita1, Masahiro Nishida1, Masumi Higashide2
1Department of mechanical engineering, Nagoya Institute of Technology, Japan, 2JAXA
2017-r-37 ( 9:40 – 10:00 )
Possibility of sustained discharge on satellite’s power harness behind the solar array paddle caused by hypervelocity impacts
Takayuki Hirai1, Masumi Higashide1, Hirohisa Kurosaki1, Shirou Kawakita2, Yuki Mando3, Shota Yamaguchi4, Koji Tanaka5
1Research and Development Directorate, Japan Aerospace Exploration Agency, Japan, 2Space Technology Directorate I, Japan Aerospace Exploration Agency, 3The Graduate School of Advanced Technology and Science, University of Tokushima, 4Graduate School of Engineering, Tokai University, 5Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
2017-r-38 ( 10:00 – 10:20 )
Hypervelocity Impact Damage Pattern Recognition in Aluminum Alloy Plates based on D-S Evidence Theory and BP Neural Network
cao wuxiong, pang baojun
School of Aeronautics, Harbin Institute of Technology, China
[r-9] Space Debris (Active Debris Removal 1)

Session Date June 8 (Thu) 11:00 – 12:20
Room Meeting Room 13
Chairpersons
2017-r-39 ( 11:00 – 11:20 )
Research and Development of the Osaka Institute of Technology PROITERES 4th Nano-Satellite for Debris Deorbiting by Electric Propulsion
Kaisei Kajihara, Hiroki Fujita, Tomoaki Hashimoto, Hirokazu Tahara, Kyoko Takada
Department of Mechanical Engineering, Osaka Institute of Technology, Japan
2017-r-40 ( 11:20 – 11:40 )
Quick Reports on on-board demonstration experiment of camera system for autonomous visual guidance for space debris removal
Shinichi Kimura1, Yasuhiro Katayama2, Yuuta Horikawa2
1Department of Electrial Engineering, Tokyo University of Science, Japan, 2Japan Aerospace Exploration Agency
2017-r-41 ( 11:40 – 12:00 )
An Optimal Rendezvous with Multiple Space Debris Utilizing Nodal Regressions for Low Earth Orbits
Koki Fujita1, Ryusuke Harada2, Toshiya Hanada1
1Department of Aeronautics and Astronautics, Kyushu University, Japan, 2Department of Aeronautics and Astronautics, Graduate school of Kyushu University
2017-r-42 ( 12:00 – 12:20 )
Ant Colony Optimization based design of multiple-target active debris removal mission
Tianjiao Zhang, Honxin Shen, Hengnian Li, Jisheng Li
State Key Laboratory of Astronautic Dynamics , Xi’an Satellite Control Center, China
[r-10] Space Debris (Active Debris Removal 2)

Session Date June 8 (Thu) 14:00 – 14:40
Room Meeting Room 13
Chairpersons
2017-r-43 ( 14:00 – 14:20 )
Determination of Fracture Toughness of Hollow Cylindrical Tether at Space Debris Impact
Kazumasa Sasahara1, Shu Kondo1, Yoshiyuki Uwamino1, Sunao Hasegawa2, Kanjuro Makihara1
1Department of Aerospace Engineering, Tohoku University, Japan, 2Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
2017-r-44 ( 14:20 – 14:40 )
Numerical Simulation of Tape Tether Deployment from Storage Container
Hirohisa Kojima1, Pavel M Trivailo2, Takeo Watanabe3, Hironori A Fujii4
1Department of Aerospace Engineering, Tokyo Metropolitan University, Japan, 2Royal Melbourne Institute of Technology, 3Teikyo University, 4TMIT
[r-11] Space Debris (Active Debris Removal 3)

Session Date June 8 (Thu) 16:00 – 17:20
Room Meeting Room 13
Chairpersons
2017-r-46 ( 16:00 – 16:20 )
Deorbiting of Space Debris by Laser Ablation
Toshikazu Ebisuzaki, Satoshi Wada
RIKEN, Japan
2017-r-47 ( 16:20 – 16:40 )
Study on Orbital Remediation Sequence of Space Debris using Laser Ablation
Yuta Kobayashi
Kyoto University, Japan
2017-r-48 ( 16:40 – 17:00 )
Measurement and Reduction of recoil load in debris capture gun
Keno Yoshida1, Yasuhiro Akahoshi1, Takao Koura1, Takahiko Mataki1, Megumi Kageyama1, Yukihito Kitazawa2, Taku Izumiyama2, Satomi Kawamoto3, Hiroyuki Okamoto3
1Department of Mechanical and Control Engineering, Kyushu Institute of Technology, Japan, 2IHI Corporation, Japan, 3JAXA, Japan
2017-r-49 ( 17:00 – 17:20 )
Application of the Spherical Dartboard Method to Active Debris Removal
Ahmed M. Hussein, Mohammed K. Ibrahim
Department of Aerospace Engineering, Cairo University, Egypt, Egypt
[r-12] Space Ddebris (Mitigation, Modelling, Near Earth Objects)

Session Date June 9 (Fri) 9:00 – 10:20
Room Meeting Room 3
Chairpersons
2017-r-50 ( 9:00 – 9:20 )
Accurate Aerodynamic Model for Membranes in Free-Molecular Flow to be Used for Deorbit Device Design
Nobuhiro Funabiki
Department of aeronautics and astronautics, University of Tokyo, Japan
2017-r-52 ( 9:20 – 9:40 )
Study of the effects of the Lorentz force on space objects with high area-to-mass ratio
Kento Hoshi1, Romain Serra2, Massimiliano Vasile2, Hiroshi Yamakawa3
1Department of Electrical Engineering, Graduate School of Engineering, Kyoto University, Japan, 2Department of Mechanical and Aerospace Engineering, University of Strathclyde, 3Research Institute for Sustainable Humanosphere, Kyoto University
2017-r-53 ( 9:40 – 10:00 )
Magnetic Field Effects on Sub-millimeter-sized Debris
Makoto Hanada1, Koki Fujita1, Toshiya Hanada1, Hiroshi Yamakawa2
1Kyushu University, Japan, Japan, 2Kyoto University, Japan
2017-r-54 ( 10:00 – 10:20 )
Rotational Changes of the NEA (Near-Earh Asteroid) 99942 Apophis during the 2029 close encounter with the Earth
Jean SOUCHAY
SYRTE, Observatoire de Paris, France
[r-13] Space Debris (Legal Issue, Collision Avoindace, Operation)

Session Date June 9 (Fri) 11:00 – 12:00
Room Meeting Room 3
Chairpersons
2017-r-55 ( 11:00 – 11:20 )
Political and Legal Challenges for Active Space Debris Removal ~Possible International Steps~
Yu Takeuchi
Space Technology Directorate I, Japan Aerospace Exploration Agency, Japan
2017-r-56 ( 11:20 – 11:40 )
French contribution to EU SST CA service
Francois LAPORTE, Monique MOURY
Operational Flight Dynamics, CNES, France
2017-r-58 ( 11:40 – 12:00 )
Consideration of Collision “Consequence” in Satellite Conjunction Assessment and Risk Analysis
Matthew D Hejduk1, T.S. Kelso2, Lauri K Newman3, Monique Moury4, Francois Laporte4, Chikara Harada5, Sinichi Nakamura5
1Astrorum Consulting LLC, USA, 2Analytical Graphics Inc, 3NASA GSFC, 4CNES, 5JAXA
[t-1] Microsatellite and Software

Session Date June 6 (Tue) 14:00 – 15:20
Room Meeting Room 3
Chairpersons
2017-t-01 ( 14:00 – 14:20 )
OPTELEC: an optimisation software for low-thrust orbit transfers including satellite and operation constraints
Slim Locoche
Department of AOCS / GNC & Flight Dynamics, Airbus Defence and Space, France
2017-t-02 ( 14:20 – 14:40 )
Space System Launch Cost Analysis: A Value-Centric Architecture Based on System Characteristic Space
Qin Xu, Peter Hollingsworth, Katharine Smith
School of Mechanical, Aerospace and Civil Engineering, The University of Manchester, UK
2017-t-04 ( 14:40 – 15:00 )
An Implementation of Bus-Type Architecture with Common Subsystem to Microsatellite ORBIS
Hirohisa ASANO, Hironori Sahara
Department of Aerospace Engineering, Tokyo Metropollitan Univercity, Japan
2017-t-05 ( 15:00 – 15:20 )
Satellite Control System Utilizing Orbit Calculation Package Software ORBITER FORCE
Yoshiyuki Takasugi, Keiko Takahashi, Shinichi Kawazoe, Takafumi Ohnishi, Masaya Kameyama
Fujitsu Limited, Japan, Japan
[t-2] Value Creation and Innovation

Session Date June 6 (Tue) 16:00 – 17:40
Room Meeting Room 3
Chairpersons
2017-t-06 ( 16:00 – 16:20 )
A Methodology to Create Innovative Services for Space Application
Makoto Ioki1, Takeshi Hirose1, Yoshitaka Narita1, Shoji Yoshikawa2, Naoki Imamura2, Kazuhide Kodeki2, Seiichi Shimizu2, Osamu Takahara2, Eiji Yokoyama2
1Graduate School of System Design and Management, Keio University, Japan, 2Advanced Technology R&D Center, Mitsubishi Electric Co.
2017-t-07 ( 16:20 – 16:40 )
A Value-Centric Design and Certification Architecture for Innovative Space Systems
Qin Xu, Peter Hollingsworth, Katharine Smith
School of Mechanical, Aerospace and Civil Engineering, The University of Manchester, UK
2017-t-08 ( 16:40 – 17:00 )
A Concept Design of GSN-based Framework for Managing Satellite Service Creation
MEGUMI YAMAMOTO, NAOHIKO KOHTAKE
Graduate School of System Design and Management, Keio University, Japan
2017-t-09 ( 17:00 – 17:20 )
A Systems Evaluation Framework for Futuristic Aerospace Projects
Nobuaki Minato
Graduate School of Technology Management, Ritsumeikan University, Japan
2017-t-10 ( 17:20 – 17:40 )
Value-Centric/Driven Design – A Framework
Lavanan Vengadasalam, Abdullah Desai, Peter Hollingsworth, Katharine Smith
The University of Manchester, UK, UK
[t-3] Mission Design and Education

Session Date June 7 (Wed) 9:00 – 10:40
Room Meeting Room 12
Chairpersons
2017-t-11 ( 9:00 – 9:20 )
Space Mission Architecture Design Philosophies and Methodologies – A Review
Lavanan Vengadasalam, Peter Hollingsworth, Katharine Smith
The University of Manchester, UK, UK
2017-t-12 ( 9:20 – 9:40 )
The Collocation Stand-Alone Library and Toolkit For NASA Goddard’s General Mission Analysis Toolkit
Jeremy Knittel1, Steve Hughes1, Wendy Shoan1, Youngkwang Kim2
1NASA GSFC, USA, 2Korean Aerospace Research Institute
2017-t-13 ( 9:40 – 10:00 )
Automated Sensitivity Analysis of Interplanetary Trajectories for Optimal Mission Design
Jeremy Knittel1, Jacob Englander1, Bruno Sarli2
1NASA GSFC, USA, 2Catholic University of America
2017-t-14 ( 10:00 – 10:20 )
Competency Evaluation Applied to Human Resource Development Program Designed to Solve Social Issues using Space Applications
Aria Iwasawa1, Naohiko Kohtake1, Masahiro Fukuhara2, Fabien Roudier2
1Graduate School of System Design and Management, Keio University, Japan, 2Institution for a Global Society
2017-t-15 ( 10:20 – 10:40 )
Study on Highly Accurate and Responsive Tracking Antenna Control System for Simultaneous Observations by Unmanned Air Vehicles
Masazumi Ueba, Yuuichi Takaku, Schoichi Kitazawa, Ken Higuchi
Muroran Institute of Technology, Japan
[t-4] Systems Approach

Session Date June 7 (Wed) 11:00 – 12:20
Room Meeting Room 12
Chairpersons
2017-t-16 ( 11:00 – 11:20 )
Integrating Flight Software Apps to the Core Flight System
Mar Cols-Margenet1, Hanspeter Schaub1, Scott Piggott2
1Department of Aerospace Engineering Sciences, University of Colorado Boulder, USA, 2Laboratory for Atmospheric and Space Physics
2017-t-17 ( 11:20 – 11:40 )
Probability Inference Approach for Stochastic Robust Flight Control Design
Taro Tsukamoto
Aeronautical Technology Directorate, JAXA, Japan
2017-t-18 ( 11:40 – 12:00 )
Updates on the Development of the Support Software System for the Philippine’s Microsatellite Operations
Mary Ann Zabanal Constante, Joel Joseph Marciano, Mark Edwin Tupas, Romer Kristi Aranas, Benjamin Joseph Jiao, Kaye Kristine Vergel, Miguel Francisco Felicio, Marc Caesar Talampas, Orville Labbao, John Leur Labrador, Harold Bryan Paler, Ariston Gonzales, Neil Irwin Bernardo
PHL-Microsat – University of the Philippines, Philippines
2017-t-19 ( 12:00 – 12:20 )
Fatigue Life Estimation of launcher Electronic by Integrated Life Prediction Tools of Sherlock
Tae-Yong Park1, Young-Hyeon Jeon1, Jong-Chan Park2, Hyeong-Ahn Kwon3, Hyun-Ung Oh1
1Department of Aerospace Engineering, Chosun Univerisity, Republic of Korea, Korea, 2Korea Aerospace Research Institute (KARI), Republic of Korea, 3Exleet Edge Co. Ltd., Republic of Korea
[t-5] Positioning System

Session Date June 7 (Wed) 16:00 – 17:40
Room Meeting Room 12
Chairpersons
2017-t-20 ( 16:00 – 16:20 )
Spot-based RTK Positioning and User Interface Development for Improvement of Oil Palm Replanting Processes
Akira Kodaka1, Tomoaki Masuma1, Abd Rasid Mohd Najib Bin2, Samad Mohd Na’aim Bin2, Abidin Haryati2, Ko Hamamoto3, Naohiko Kohtake1
1Graduate School of System Design and Management, Keio University, Japan, 2Research & Development and Agri Services Cluster, FGV, 3Earth Observation Research Center, Space Technology Directorate I, JAXA
2017-t-21 ( 16:20 – 16:40 )
Design of GNSS-Based Multi-Hazard Early Warning System for Multiple Countries: Case of Tsunamis and Bushfires in Asia and Oceania Regions
Shota Iino1, Daisuke Iwaizumi2, Tomohiko Hatori1, Naohiko Kohtake3
1PASCO CORPORATION, Japan, 2Acquisition, Technology and Logistics Agency, 3Keio University
2017-t-22 ( 16:40 – 17:00 )
Concept Design of Seamless Location Based Emergency Warning System with GNSS-Based Signals
Akihiro Sato, Madoka Nakajima, Naohiko Kotake
Graduate School of System Design and Management, Keio University, Japan
2017-t-23 ( 17:00 – 17:20 )
System Design and Verification for Improving Simplicity of Developing Indoor-Outdoor Seamless Positioning Environment
kenichi tabata
graduate school of system design and management, Keio university, Japan
2017-t-24 ( 17:20 – 17:40 )
Simulation for GNSS Utilization and DEM Construction in Urban
Masahiko Nagai1, Sakpod Tongleamnak2, Zahid Wani2
1Graduate School of Sciences and Technology for Innovation, Yamaguchi University, Japan, 2Asian Institute of Technology
[t-6] Modeling and Simulation

Session Date June 8 (Thu) 11:00 – 11:40
Room Meeting Room 7
Chairpersons
2017-t-25 ( 11:00 – 11:20 )
Development of Open Model-based Collaboration Tool and Application on Nano-satellite Project
Yohsuke Nambu1, Masashi Miura2, Ryosuke Yoshizawa3, Toshishige Hagihara3, Shunsuke Kimura3, Akira Yumiyama3, Satoru Igarashi3
1Department of Aerospace Engineering, Osaka Prefecture University, Japan, 2Tottori University, 3levii Inc.
2017-t-26 ( 11:20 – 11:40 )
SIRIUS model-driven approach for the design of operational Flight Dynamics Systems
Pamini ANNAT1, Romain BERNARD2, Jesus ESTEBAN DONES3
1CNES, France, 2EXMS, 3THALES
[u-1] Space Education for Children and General Public

Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 11
Chairpersons
2017-u-01 ( 9:00 – 9:20 )
Space Education method to influence school teachers
Osamu Matsubara, Atsushi Muromachi, Ayami Kojima
Space Education Center, Japan Aerospace Exploration Agency (JAXA), Japan
2017-u-02 ( 9:20 – 9:40 )
JAXA Space Education Program for Informal Education -“Aerospace School” and “One Day Aerospace Journalist”-
Keiko Miyata
Space Education Center, Japan Aerospace Exploration Agency, Japan
2017-u-03 ( 9:40 – 10:00 )
Outreach and Public Relations of Hayabusa2 Project
Makoto Yoshikawa, Eri Koyama, Stoshi Hosoda, Yuto Takei, Satoru Nakazawa, Yuichi Tsuda, Azusa Yabe, Takuya Ohkawa
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan
2017-u-04 ( 10:00 – 10:20 )
Space Development Board Game for Learning Public Engagement in Science and Technology
Masashi Miura1, Haruhiko Maenami2
1Department of Engineering, Tottori University, Japan, 2Organization for Regional Industrial Academic Cooperation, Tottori University
2017-u-05 ( 10:20 – 10:40 )
Space Education Program Based on High-Altitude Aerial Shooting from Stratosphere Using
Space Balloon and Virtual Reality Technique
Ryuya Yokoo1, Yusuke Teshima1, Haruya Uchida1, Koya Kuwamura2, Susumu Hara2
1Department of Mechanical and Aerospace Engineering, School of Engineering, Nagoya University, Japan, 2Department of Aerospace Engineering, Graduate School of Engineering, Nagoya University
[u-2] Space Education for Students of Engineering

Session Date June 6 (Tue) 11:00 – 12:40
Room Meeting Room 11
Chairpersons
2017-u-06 ( 11:00 – 11:20 )
Implementation Report of KOSEN Space Camp in 2015 and 2016
Makoto Wakabayashi1, Taku Takada2, Kazumasa Imai2, Yoshihiro Kajimura3, Jun Nakaya4, Kentarou Kitamura5, Yukikazu Murakami6, Fumio Asai7, Masahiro Tokumitsu8, Manabu Shinohara9, Kazuo Shimada10
1National Institute of Technology (NIT), Niihama College, Japan, 2NIT, Kochi College, 3NIT, Akashi College, 4NIT, Gumma College, 5NIT, Tokuyama College, 6NIT, Kagawa College, 7NIT, Nara College, 8NIT, Yonago College, 9NIT, Kagoshima College, 10Human Network KOSEN
2017-u-07 ( 11:20 – 11:40 )
Three-years Results of Space Technology Education Project from a Collaboration with National Technical Colleges for Small Spacecraft Development
Taku Takada1, Kazumasa Imai1, Kentarou Kitamura2, Yukikazu Murakami3, Fumio Asai4, Makoto Wakabayashi5, Yoshihiro Kajimura6, Nobuto Hirakoso7, Manabu Shinohara8, Jun Nakaya9, Masahiro Tokumitsu10, Kazuo Shimada11
1NIT, Kochi College, Japan, 2NIT, Tokuyama College, 3NIT, Kagawa College, 4NIT, Nara College, 5NIT, Niihama College, 6NIT, Akashi College, 7NIT, Gunma College, 8NIT, Kagoshima College, 9NIT, Gifu College, 10NIT, Yonago College, 11Human Network KOSEN
2017-u-08 ( 11:40 – 12:00 )
An Engineering Design Education Program as an Inheritance of Space Technology Education Project
Kentarou Kitamura1, Itsuo Sakuramoto1, Mitsumasa Ikeda1, Taku Takada2, Kazumasa Imai2, Makoto Wakabayashi3, KOSEN Space Collaboration Group4
1Department of Mechanical and Electrical Engineering, National Institute of Technology, Tokuyama College, Japan, 2Department of Social Design Engineering, National Institute of Technology, Kochi College, 3 Department of Electrical Engineering and Information Science, National Institute of Technology, Niihama College, 4KOSEN Space Collaboration Group
2017-u-09 ( 12:00 – 12:20 )
Case Study of University of Tsukuba for Global Space Exploration Engineering Education
Toshihiro KAMEDA1, Akihiro NAGATA2, Atsushi YASUDA3, Hiromasa WATANABE3
1Institute of Engineering Mechanics and Energy, University of Tsukuba, Japan, 2College of Engineering Systems, University of Tsukuba, 3College of Physics, University of Tsukuba
2017-u-10 ( 12:20 – 12:40 )
Space Education Program of the Tokyo University of Science A trial for space education
Hideki Sato, Shinichi Kimura, Ichiro Ueno, Hideyuki Suzuki, Tomoaki Tatsukawa, Kozo Fujii, Makoto Yamamoto, Chiaki Mukai
Tokyo University of Science, Japan
[u-3] Satellites for Space Education

Session Date June 6 (Tue) 14:00 – 15:40
Room Meeting Room 11
Chairpersons
2017-u-11 ( 14:00 – 14:20 )
Introducing CanSat for Project Based Learning of Space Science and Engineering in Nepal
Rakesh Chandra Prajapati1, Sanjeeb Humagain1, Abinish Kumar Dutt2, Saurav Paudel2
1ORION Space, Nepal, 2Kathmandu University
2017-u-12 ( 14:20 – 14:40 )
Capacity Building in Space Technology in the Philippines through the PHL-Microsat
Program
Mary Ann Zabanal Constante, Joel Joseph Marciano, Marc Caesar Talampas, Adrian Salces, Paula Jean Cansino, Patth Rick Ramirez, Izrael Zenar Bautista, Charleston Dale Ambatali, Mar de Guzman, Keziah Bartilad, Janette Salvatus
PHL-Microsat – University of the Philippines, Philippines
2017-u-13 ( 14:40 – 15:00 )
Developing a MicroSat Kit for Space Systems Engineering Education
Minh Anh Pham
System Design and Management , Keio University, Japan
2017-u-14 ( 15:00 – 15:20 )
Scalable Nano-Satellite Platform for Low-Cost Space Education
Toshinori Kuwahara, James Harpur
Department of Aerospace Engineering, Tohoku University, Japan
2017-u-15 ( 15:20 – 15:40 )
Unified Dissemination System of Multiple Satellite Image Data
Toshiaki Iwata, Ryosuke Nakamura, Toru Kouyama, Soushi Kato, Atsushi Oda
National Institute of Advanced Industrial Science and Technology, Japan
[u-4] Competitions and Culture

Session Date June 6 (Tue) 16:00 – 17:20
Room Meeting Room 11
Chairpersons
2017-u-16 ( 16:00 – 16:20 )
Satellite Design Contest in Japan – present and future
Koichiro Oyama1, Takeshi Ori2
1Institute of Space and Plasma Sciences, National Cheng Kung University, Taiwan, 2Japan Space Forum
2017-u-17 ( 16:20 – 16:40 )
Space Architecture Competitions, Which Drive STEAM for NewSpace
Misuzu Onuki1, Akito Sogame2, Yozan Takahashi2
1Space Frontier Foundation, Japan, 2Tokai University
2017-u-18 ( 16:40 – 17:00 )
KOSMOS, an artistic model of the Solar System with same scale for size and distance
Xavier Daniel1, Guy Pignolet2
1Visual Artist, Art, Reunion, 2Reunion Island Space Initiative
2017-u-19 ( 17:00 – 17:20 )
Inter-networking Space Technology and Science : from “National” to “Global-Local”
Guy Pignolet1, Edmond Lauret2, Ryojiro Akiba3
1Reunion Island Space Initiative, Reunion, 2Professional Dreamer, 3HASTIC
[u-5] Rockets for Space Education

Session Date June 7 (Wed) 9:00 – 10:20
Room Meeting Room 15
Chairpersons
2017-u-20 ( 9:00 – 9:20 )
A Study on Development of a Small Hybrid Rocket as an Educational Material
Masaya Nakahara1, Ryouichi Tokigawa1, Keisuke Watada1, Kohki Banden1, Fumiaki Abe1, Kenichi Tokunaga1, Atsushi Ishihara2
1Ehime University, Japan, 2Saitama Institute of Technology
2017-u-21 ( 9:20 – 9:40 )
A Hybrid Rocket for Usual Science Classes in a Public Junior High School
Atsushi Ishihara1, TianWen Zhang1, Brian Teoh Kai Shen1, Masaya Nakahara2
1Department of Mechanical Engineering, Saitama Institute of Technology, Japan, 2Ehime University
2017-u-22 ( 9:40 – 10:00 )
EspaceLab: Fab Lab Aimed Towards Teaching and Community Projects in the Fields of Aerospace, Robotics, and Environmental Sciences
Paul-Francois Paradis1, Benoit Debaque1, Margarida Romero2, Simon Lambert-Girard1
1EspaceLab, Canada, 2Laval University, Teaching and Learning Dept.
2017-u-23 ( 10:00 – 10:20 )
Development of Candy Hybrid Rocket Motor for Undergraduate Space Education
Yutaka Wada1, Yo Kawabata1, Kenji Ogimoto2, Hiroaki Wakayama3, Takao Yanagi4, Seiichi Sakamoto5
1Department of Innovative Mechanical and Electronic Engineering, Chiba Institute of Technology, Japan, 2SOUKI Systems Co. Ltd., 3Wakayama University, 4Hakuhodo DY media partners Inc., 5NAOJ
[v-1] Law and Policy for Space Development

Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 15
Chairpersons
2017-v-01 ( 9:00 – 9:20 )
A Study concerning Legal Challenges for Space Exploration Cooperation
Motoko Uchitomi
Policy Alternatives Research Institute, The University of Tokyo, Japan
2017-v-02 ( 9:20 – 9:40 )
The legal Status of the Hosted Payload
Akiko Watanabe
Independent Researcher, Japan
2017-v-03 ( 9:40 – 10:00 )
The Legality of an International Regime for Space Traffic Management (STM)
Yu Takeuchi
Space Technology Directorate I, Japan Aerospace Exploration Agency, Japan
2017-v-04 ( 10:00 – 10:20 )
The Space Policy of the Carter Administration: A Reconstruction of National Space Policy in the Cold War
Hirotaka Watanabe
Center for the Study of Co* Design & Graduate School of Law and Politics, Osaka University, Japan
2017-v-05 ( 10:20 – 10:40 )
Crafting the Philippines Space Development and Utilization Policy and Creating the Philippine Space Agency: Challenges and Opportunities
Rogel Mari Dionisio Sese
National SPACE Development Program, Philippines
[v-2] Policy for Space Development

Session Date June 6 (Tue) 11:00 – 12:20
Room Meeting Room 15
Chairpersons
2017-v-06 ( 11:00 – 11:20 )
Earthquake Prediction Research as National Space Project
Tetsuya Kodama
Research and Development Directorate, JAXA, Japan
2017-v-08 ( 11:20 – 11:40 )
The Implication of Remote Sensing to the Asian Regional Security
Yasuaki Hashimoto
Policy Studies Department, The National Institute for Defense Studies, Japan
2017-v-09 ( 11:40 – 12:00 )
Space Development Models and Roadmaps Analysis of Asian and African Countries
Feng-Tai Hwang
Division of Systems Engineering, National Space Organization, Taiwan
2017-v-10 ( 12:00 – 12:20 )
The Use of Space Applications in a context of Terrorist Threats
Anne-Sophie Martin
Political Science, University of Rome “La Sapienza”, Italy
[v-3] Economy for Space Development

Session Date June 6 (Tue) 14:00 – 14:40
Room Meeting Room 15
Chairpersons
2017-v-11 ( 14:00 – 14:20 )
NewSpace Innovation Creating the Next-gen Space Economy
Misuzu Onuki
Space Frontier Foundation, Japan
2017-v-12 ( 14:20 – 14:40 )
Marketing for New Satellite Business
Makoto Arai
Space Lab, Dentsu Inc., Japan
[w-1] Safety and Mission Assurance (EEE Parts)

Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 14
Chairpersons
2017-w-01 ( 9:00 – 9:20 )
SEE sensitivity evaluation results of Atom Switch ROM/FPGA
Kozo Takeuchi1, Munehiro Tada2, Toshitsubu Sakamoto2, Hiroyuki Shindou1, Satoshi Kuboyama1, Akinori Takeyama3, Takeuchi Ohshima3, Koichi Suzuki1
1Japan aerospace exploration Agency, Japan, 2NEC, 3National Institutes for Quantum and Radiological Science and Technology
2017-w-02 ( 9:20 – 9:40 )
Development of Rad-Hard Super-Junction Power MOSFETs
Eiichi Mizuta1, Yuki Nakada1, Satoshi Kuboyama1, Masanori Inoue2, Yuji Kumagai2, Koichi Suzuki1
1Japan Aerospace Exploration Agency, Japan, 2Fuji Electric Co., Ltd.
2017-w-03 ( 9:40 – 10:00 )
Approach to high thermal conductive substrate for electronic components
Kazunori Shimazaki, Yuji Yamada, Koichi Suzuki
Research Unit I, Research and Development Directorate, Japan Aerospace Exploration Agency, Japan
2017-w-04 ( 10:00 – 10:20 )
Construction of the measurement equipment and preliminary evaluation for near-magnetic-field effects of high performance space LSIs
Sakamoto Keita, Shindou Hiroyuki, Kuboyama Satoshi, Suzuki Koichi
Research and Development Directorate, JAXA, Japan
2017-w-05 ( 10:20 – 10:40 )
A Proposal for guideline to use the COTS EEEparts for The Scientific Satellites
Kazuhide Noguchi
S&MA(Safety & Missyon Asuurance), JAXA ISAS, Japan
[w-2] Safety and Mission Assurance (Assuarance Technology)

Session Date June 6 (Tue) 11:00 – 12:20
Room Meeting Room 14
Chairpersons
2017-w-06 ( 11:00 – 11:20 )
Preliminary Evaluation of 6 MV Tandem Accelerator in Tsukuba University for Single Event Testing
Akifumi Maru, Hiroyuki Shindou, Koichi Suzuki
Research and Development Directorate Research Unit I, JAXA, Japan
2017-w-07 ( 11:20 – 11:40 )
Preliminary Radiation Test Result for Space Ready Qualification of Lunar Micro Rover
Takuto Oikawa1, Toshiki Tanaka2, Yuto Suebe1, Kentaro Uno1, Hugo Zuliani1, Louis Jerome Burtz2, Kazuya Yoshida1
1Department of Aerospace Engineering, Tohoku University, Japan, 2KK ispace inc.
2017-w-08 ( 11:40 – 12:00 )
Improving activity of clean room for scientific spacecrafts
Matsushi Miura, Fuminari Itou, Ryoji Kobayashi
JAXA, Japan
2017-w-09 ( 12:00 – 12:20 )
Lessons Learned from NASA Space Launch System (SLS) Exploration Mission 1 (EM-1) Payload Safety Review Panel (PSRP) for Secondary Payloads
Takashi Goto1, Masami Miki1, Koji Oga1, Teruhiko Tabuchi2, Toshinori Ikenaga5, Ryu Funase3, Tatsuaki Hashimoto4
1Safety and Product Assurance, Japan Manned Space Systems Corporation, Japan, 2Safety and Mission Assurance, JAXA, 3Department of Aeronautics and Astronautics, University of Tokyo, 4Space and Astronauntical Science, Spacecraft Engimeering, JAXA, 5Research and Development Directorate, JAXA
[w-3] Safety and Mission Assurance (Principles and Standards)

Session Date June 6 (Tue) 14:00 – 15:40
Room Meeting Room 14
Chairpersons
2017-w-11 ( 14:00 – 14:20 )
Principles to develop and operate resilient spacecrafts
Ryoji Kobayashi
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan
2017-w-12 ( 14:20 – 14:40 )
The Utilization of the Metrics of Scales of “Severity” and “Probability” which consist in the Qualitative Risk Matrix
Yasushi Mori
Quality Assurance Department, Mitsubishi Electric Corporation, Kamakura Works, Japan
2017-w-13 ( 14:40 – 15:00 )
Quality Leadership Communication: International Cooperation in IAQG/JAQG
Hiroki Yanagawa
Quality Department, Space Systems Division, Mitsubishi Heavy Industries, Ltd., Japan
2017-w-14 ( 15:00 – 15:20 )
Lessons Learned from ESA/NASA/JAXA Trilateral Efforts for Mutual Recognition of S&MA Standards
Masami Mitsui1, Shuji Araki2, Mieko Matsuda2, Shunsuke Sasaki1, Rafael Prades4, Frank Groen3
1JAMSS, Japan, 2JAXA, 3NASA, 4ESA
2017-w-15 ( 15:20 – 15:40 )
JAXA Design Standards for Space Project
Yuji KADO, Shuji ARAKI, Mieko MATSUDA, Masayuki IKEUCHI
Safety and Mission Assurance Department, JAXA, , Japan
[w-4] Safety and Mission Assurance (Software Assurance)

Session Date June 6 (Tue) 16:00 – 17:20
Room Meeting Room 14
Chairpersons
2017-w-16 ( 16:00 – 16:20 )
A new software IV&V approach based on CAST and Safety-Driven Design
Keita Sakemi1, Michihiro Matsumoto1, Nobuyuki Hoshino1, Hideki Nomoto1, Rihito Aman2, Yamato Fukuta2, Satoru Kitamura2, Takashi Kunifuji2
1Safety and Product Assurance Department, Japan Manned Space Systems Corporation, Japan, 2East Japan Railway Company
2017-w-17 ( 16:20 – 16:40 )
Applying Accident Cases across Domains using STAMPCAST Analysis
Kazuki Kakimoto, Shigeo Yoshikawa, Hideki Nomoto
Dapartment of Safety & Product Assurance, Japan manned space system , Japan
2017-w-18 ( 16:40 – 17:00 )
Transition of Independent Verification and Validation Activity and Refined Concept at the Mature Age
Naoko Okubo, Hiroki Umeda, Yasushi Ueda, Shinji Kawaguchi, Taisuke Kanbe
Research and Development Directorate, Japan Aerospace Exploration Agency, Japan
2017-w-19 ( 17:00 – 17:20 )
Improvement of Software Assurance Activities in Spacecraft Software Development by Value Propagation of Standard Process
Tomohito Yamada, Yuichi Saito, Tsutomu Matsumoto
Research Unit III, Research and Development Directorate, Japan Aerospace Exploration Agency, Japan
Finalist Student Session
[s-1]

Session Date June 8 (Thu) 9:00 – 10:40
Room Meeting Room 12
Chairpersons
2017-s-01-a ( 9:00 – 9:20 )
Analysis of Alternative Liquid Propellants and Propulsion Systems for Micro Launch Vehicles
Francesco Iervese
Politecnico di Milano, Italy
2017-s-02-b ( 9:20 – 9:40 )
Parameter survey on rotating magnetic field acceleration
Takeru Furukawa
Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology, Japan
2017-s-03-b ( 9:40 – 10:00 )
Power Matching between Plasma Source and Electrostatic Acceleration in Helicon Electrostatic Thruster
Yoshiya Nakagawa
Nagoya University, Japan
2017-s-04-c ( 10:00 – 10:20 )
Quasi-static deployment of a membrane structure using electromagnetic force in small-sized satellites
Yamada Yuki
Department of Aerospace Engineering, Nagoya University, Japan
2017-s-05-d ( 10:20 – 10:40 )
Low-Thrust Trajectory Design to Improve Overall Mission Success Probability Incorporating Target Changes in Case of Engine Failures
Akifumi Wachi
Department of Aeronautics and Astronautics, University of Tokyo, Japan
[s-2]

Session Date June 8 (Thu) 11:00 – 12:40
Room Meeting Room 12
Chairpersons
2017-s-06-d ( 11:00 – 11:20 )
An Analytical Solution for Multi-revolution Transfer Trajectory with Periodic Thrust and Non-Singular Elements
Yusuke Ozawa
University of Tokyo, Gradiate School of Frontier Sciences, Department of Advanced Energy, Japan
2017-s-07-d ( 11:20 – 11:40 )
Attitude and Orbit Control of a Spinning Solar Sail by the Vibrational Input on the Sail Membrane
Yuki Takao
Department of Aeronautics and Astronautics, The University of Tokyo, Japan
2017-s-08-d ( 11:40 – 12:00 )
Estimation Algorithm of Relative Position and Attitude during Proximity Rendezvous and Docking Using Multiple Ultra-Wide-Band Devices
Mikihiro Ikura
Department of aeronautics and astronautics, University of Tokyo, Japan
2017-s-09-e ( 12:00 – 12:20 )
Development of Engineering Model Providing Body Force Distribution of Tri-electrode Plasma Actuator
Kumi Nakai
Department of mechanical systems engineering, Tokyo University of Agriculture and Technology, Japan
2017-s-10-e ( 12:20 – 12:40 )
Ballistic Range Experiment of Sphere in Dusty Atmosphere
Chihiro Masaki
Graduate School of Frontier Sciences, Department of Advanced Energy, The University of Tokyo, Japan
[s-3]

Session Date June 8 (Thu) 14:00 – 15:40
Room Meeting Room 12
Chairpersons
2017-s-11-f ( 14:00 – 14:20 )
Orbit Control for Nano-Satellites Using Plasma Drag Force
Shinji Matsuzawa
Department of Aerospace Engineering, Nagoya University, Japan
2017-s-12-f ( 14:20 – 14:40 )
Design and Development of the STARS-E Climber’s Roller
Daichi Murakami
Department of Precision Machinery Engineering, University of Nihon, Japan
2017-s-13-g ( 14:40 – 15:00 )
Analysis of Expander-Cycle Rocket Engine Performance at Varying Mixture Ratios
Matthew Richardson
Department of Aeronautics and Astronautics, University of Tokyo, Japan
2017-s-14-h ( 15:00 – 15:20 )
Laser-induced Spark Ignition for DME-Air Mixtures under Microgravity
Yoshinari Kobayashi
Department of Aeronautics and Astronautics , University of Tokyo, Japan
2017-s-15-k ( 15:20 – 15:40 )
The study of the space based observation of lunar impact flashes
Ryota Fuse
Deportment of Aerospace Engineering, Nihon University, Japan
[s-4]

Session Date June 8 (Thu) 16:00 – 17:40
Room Meeting Room 12
Chairpersons
2017-s-16-q ( 16:00 – 16:20 )
Study of Heater Electric Power Control with Autonomous Dispersed System
keisuke Umeda
Department of Aeronautics and Astronautics, The University of Tokyo, Japan
2017-s-17-r ( 16:20 – 16:40 )
Dynamics and Control of Double-Tethered Space-Tug System after Tether Rupture
Keying Yang
School of Aerospace Engineering, Beijing Institute of Technology, China
2017-s-18-r ( 16:40 – 17:00 )
Analysis for the amount of electron hole pair in Floride polymer irradiated
Shugo Yoshida
Measurement and Electric Machine Control Laboratory, Tokyo City University , Japan
2017-s-19-r ( 17:00 – 17:20 )
Construction of the Carrier Mobility Measurement System by Time of Flight Method using pulsed electron beam for spacecraft materials
Kazuki Kodama
Measurement and Electric Machine Control Laboratory, Tokyo City University, Japan
2017-s-20-t ( 17:20 – 17:40 )
Visualization methods for spacecraft telemetry data using change-point detection and dimensionality reduction
Ryo Sakagami
Department of Aeronautics and Astronautics, The University of Tokyo, Japan
Technical Session Poster
Poster Session
Session Date June 7 (Wed) 14:00 – 15:50
Room Meeting Room 11
2017-a-45p
Super High efficiency Slotless 3-phase Brushless Motors – Deploying this motors to Aerospace –
Kouichi Watanabe, Toyohiko Ota, Akira Okayasu
FM laboratory, Japan; ASIRI, Japan
2017-b-22p
Performance of Microwave Discharge Ion Engine of Variable Magnetic Field Type
Yoshiyuki Takao, Yuki Nakamine, Shinichiro Takasaki
Department of Integrated System Engineering, Faculty of Engineering, Nishinippon Institute of Technology, Japan
2017-b-64p
Thrust-Performance Maximization of Microwave Rocket Sustained by Resonant Magnetic Field
Masayuki Takahashi, Naofumi Ohnishi
Department of Aerospace Engineering, Tohoku University, Japan
2017-b-65p
Thermal Analysis of Steady-State Fully Radiation-Cooled MPD Thrusters Using Permanent Magnets for Manned Mars Exploration
Kengo Chino, Shota Saito, Yoshikazu Sugiyama, Hirokazu Tahara, Kyoko Takada
Department of Mechanical Engineering, Osaka Institute of Technology, Japan
2017-b-66p
Research and Development of Osaka Institute of Technology PROITERES Series Nano-Satellites with Electric Propulsion
Ryota Fujita1, Hiroki Fujita1, Tsubasa Yamauchi1, Kaisei Kajihara1, Ryuta Yagi1, Hirokazu Tahara1, Kyoko Takada1, Tomoyuki Ikeda2
1Department of Mechanical Engineering, Osaka Institute of Technology, Japan, 2Tokai University
2017-b-67p
Impulse Performance of Donut-Spherical Laser Launch System in Stratosphere Air-Pressure Conditions
DUC THUAN TRAN, CHONGFA XIE, KOICHI MORI
Department of Aerospace Engineering, Nagoya University, Japan
2017-b-68p
The Micro-Cathode Arc Thruster for CubeSats
yong cao, Zhi Yang
Department of Mechanical Engineering and Automation, Harbin Institute of Technology (Shenzhen), China
2017-b-69p
Chemically Augmented Arcjet Thrusters
Yuka Arai1, Shoko Shibagaki2, Kai Wada2, Souto Komine1, Miya Isoda1, Mitsutoshi Tsuchiya1, Hideyuki Horisawa3, Tomoaki Ikeda4
1Department of aeronautics and astronautics, Tokai University, Japan, 2Department of mechanical engineering, Tokai University, 3Professor, Department of aeronautics and astronautics, Tokai University, 4Associate professor, Department of aeronautics and astronautics, Tokai University
2017-b-70p
Feasibility Study on Rarefied Propellant Flow Measurement for Electric Propulsion
Yoshinori Nakayama
Department of Aerospace Engineering, National Defense Academy, Japan
2017-b-71p
Characteristics of Helicon Plasma Thruster using Advanced Acceleration Methods
Daisuke Kuwahara1, Shuichi Nishimura2, Takeru Furukawa2, Tomoya Yamase2, Daisuke Arai2, Kosuke Amma2, Yuichi Ishigami2, Hirotaka Horita3, Shunjiro Shinohara1
1Tokyo University of Agriculture and Technology, Institute of Engineering, Division of Advanced Mechanical Systems Engineering, Japan, 2Tokyo University of Agriculture and Technology, Graduate School of Engineering, Department of Mechanical Systems Engineering, 3Tokyo University of Agriculture and Technology, Graduate School of Engineering, Department of Industrial Technology and Innovation
2017-b-72p
Postural Control for Beam-Riding Flight of Microwave Rocket Using External Magnetic Field
Masayuki Takahashi, Naofumi Ohnishi
Department of Aerospace Engineering, Tohoku University, Japan
2017-b-73p
Short-Pulse Operation of a Laser-Assisted Pulsed Plasma Thruster
Hiroaki Kamezaki1, Kota Matsubara1, Kentaro Kato2, Yuji Oigawa1, Hideyuki Horisawa3
1Department of aeronautics and astronautics, Tokai University, Japan, 2Department of Mechanical engineering, Tokai University, 3Professor, Department of aeronautics and astronautics, Tokai University
2017-b-74p
Chemically Augmented Laser-thermal Thrusters
Mitsutoshi Tsuchiya1, Shoko Shibagaki2, Kai Wada2, Souto Komine1, Miya Isoda1, Yuka Arai1, Tomoyuki Ikeda3, Hideyuki Horisawa4
1Department of aeronautics and astronautics, Tokai University, Japan, 2Department of mechanical engineering, Tokai University, 3Associate professor, Department of aeronautics and astronautics, Tokai University, 4Professor, Department of aeronautics and astronautics, Tokai University
2017-b-75p
Development of an Ultraviolet Photon-driven Thruster with Light-emitting Diodes for Micropropulsion Applications
Ryosuke Koyama1, Tomoyuki Ikeda2, Hideyuki Horisawa2
1Department of mechanical engineering, Tokai University, Japan, 2Department of aerospace engineering, Tokai University
2017-b-76p
Preliminary experiment of electric field measurement in applied magnetic field plasma by laser induced fluorescence dip spectroscopy
Makoto Matsui, Arata Kishida
Department of Mechanical Engineering, Shizuoka University, Japan
2017-b-77p
Magnetic field measurement of laser-electromagnetic hybrid thrusters
Yuki Murayama1, Toshiaki Oi1, Kentaro Kato2, Haruhito Kato2, Nao Akashi1, hideyuki Horisawa1
1Department of Aeronautics and Astronautics, Tokai Univercity, Japan, 2Department of Mechanical Engineering, Tokai Univercity
2017-b-78p
Three-Dimensional Full Particle in Cell (PIC) Analyses of Three-Grid Ion Engine Operations
Takatsugu Honda1, Takeshi Miyasaka2, Ryo Kawamura1, Takeshi Hasegawa1, Makoto Asahara2
1Department of Human and Information Systems, Gifu University, Japan, 2Department of Mechanical Engineering, Gifu University
2017-b-79p
Evaluations of Unsteady Ablation and Exhaust Phenomena on Coaxial Pulsed Plasma Thrusters
Takaaki Goto1, Takeshi Miyasaka2, Takahiro Kajiwara1, Yuki Goto1, Koji Nishigaki2, Yoshimasa Matsui2, Makoto Asahara2
1Department of Human and Information Systems, Gifu University, Japan, 2Department of Mechanical Engineering, Gifu University
2017-b-80p
Plasma Profiles in a Two-dimensional Anode-layer-type Hall Thruster
Shigeru Yokota1, Hiroki Nawamoto1, Wataru Shimizu1, Junko Yamasaki1, Kohei Shimamura2
1Department of Engineering Mechanics and Energy, University of Tsukuba, Japan, 2Division of Engineering Mechanics and Energy, University of Tsukuba
2017-b-81p
Two-dimensional Hollow Cathode
Shigeru Yokota1, Moyuru Yonaha2, Junko Yamasaki2, Akira Osada2, Kohei Shimamura1
1Division of Engineering Mechanics and Energy, University of Tsukuba, Japan, 2Department of Engineering Mechanics and Energy, University of Tsukuba
2017-b-82p
Secondary Electron Effect on Potential Structure Downstream of an Ion Thruster in Full Charging State
Takanobu Muranaka1, Kento Hoshi2, Mitsuhiro Isaka1, Hirotsugu Kojima2, Hiroshi Yamakawa2, Satoshi Hosoda3, Kazutaka Nishiyama3
1Department of Electrical and Electronic Engineering, School of Engineering, Chukyo University, Japan, 2Research Institute of Sustainable Humanosphere, Kyoto University, 3Japan Aerospace Exploration Agency
2017-b-83p
Development of 1mN-class Hall Thruster for Small Satellites
Shigeru Yokota1, Yamato Adachi2, Junko Yamasaki2, Kohei Shimamura1
1Division of Engineering Mechanics and Energy, University of Tsukuba, Japan, 2Department of Engineering Mechanics and Energy, University of Tsukuba
2017-b-84p
Cathode Position Effect on Hall Thruster Performance
Shigeru Yokota2, Ken Nakatani2, Junko Yamasaki2, Kohei Shimamura1
1Division of Engineering Mechanics and Energy, University of Tsukuba, 2Department of Engineering Mechanics and Energy, University of Tsukuba, Japan
2017-c-63p
3D Periodic Auxetic Cellular Structures
Li Ma
Center for Composite Materials, Harbin Institute of Technology, China
ISTS-2017-d-167p/ISSFD-2017-167p
Formation Flying in Space-Borne Artificial Magnetic Dipole Field
Yu Cheng1, Gerard Gómez2, Josep J. Masdemont3, Jianping Yuan4
1National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University & Department de Matemàtiques i Informàtica, Universitat de Barcelona, China, 2IEEC & Department de Matemàtiques i Informàtica, Universitat de Barcelona, 3IEEC & Department de Matemàtiques, Universitat Politècnica de Catalunya, 4National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University
ISTS-2017-d-168p/ISSFD-2017-168p
Reducing the Lunisolar Numerical Ephemeris for On-board Applications
Jingshi Tang, Lin Liu, Xiyun Hou
School of Astronomy and Space Science, Nanjing University, China
ISTS-2017-d-170p/ISSFD-2017-170p
Preliminary Design of Transfer Trajectories for Asteroid Exploration Mission
Jin Haeng Choi, Kwangwon Lee, Seung-hee Lee, Chandeok Park
Department of Astronomy, Yonsei University, Korea
ISTS-2017-d-171p/ISSFD-2017-171p
The Orbit Maneuvers for Full-Parameter Reentry of Spacecraft
Gefei Li
Beijing Aerospace Control Centre,Beijing,China, China
ISTS-2017-d-172p/ISSFD-2017-172p
Dynamics and Mission Design for Space Debris Mitigation in the Geostationary Orbits
William Reis Silva1, Maisa de Oliveira Terra1, Claudia Celeste Celestino2, Cristiano Fiorilo de Melo3
1Division of Fundamental Sciences, Technological Institute of Aeronautics (ITA), Brazil, 2Federal University of ABC (UFABC), 3Federal University of Minas Gerais (UFMG)
ISTS-2017-d-173p/ISSFD-2017-173p
Altitude Estimation for Autonomous Vehicles through Wide-Field-Integration of Optic Flow
Ryusuke Nakata, Naoto Kobayashi, Mai Bando, Shinji Hokamoto
Department of Aeronautics and Astronautics, Kyushu University, Japan
ISTS-2017-d-175p/ISSFD-2017-175p
Theoretical analysis on zero propellant maneuver existence conditions
Mo-yao Yu, Ya-zhong Luo, Hai-yang Li
College of Aerospace Science and Engineering, National University of Defense Technology, China
ISTS-2017-d-176p/ISSFD-2017-176p
Autonomous Orbit Determination of Satellites around Triangular Libration Points in the Earth-Moon System
Bin Liu, Xinyun Hou, Jingshi Tang, Lin Liu
School of Astronomy and Space Science, Nanjing University, China
ISTS-2017-d-177p/ISSFD-2017-177p
Escaping from Earth-Moon Halo orbit via the unstable manifolds and lunar flybys
Xiangyu Li, Yuhua Tang, Dong Qiao
School of Aerospace Engineering, Beijing Institute of Technology , China
ISTS-2017-d-178p/ISSFD-2017-178p
SAOCOM-CS: Definition of orbital requirements for tomographic phase
Cecilia Mezzera1, Itziar Barat2, Berthyl Duesmann1, Stefano Tebaldini3, Mario Azcueta3, Bram de Vogeleer4
1European Space Agency, Netherlands, 2Deimos-Space@ESA, 3Politecnico di Milano, 4Ims space consultancy @ESA
2017-e-43p
Spectroscopic measurement of the temperature field modulated by energy deposition method
Kenji Okada1, Shinji Koizumi2, Kohei Suwata3, Takuhiro Kito3, Atsushi Matsuda3
1Department of Mechanical Engineering,Graduate school,University of Meijo, Japan, 2DENSO TECHNO CO., LTD., 3Department of Mechanical Engineering, University of Meijo
2017-e-44p
Aerodynamic and Aerothermoelastic Analysis of Body-Flap in Hypersonic Flow
Lin Huo, Tao Yang
College of Aerospace Science and Engineering, National University of Defense Technology, China
2017-e-45p
Preliminary study of reduction of metallic oxide in moon and other planets by laser and inductively coupled plasmas
Yasuaki Aiba1, Akira Kuwahara2, Ryo Myoen1, Makoto Matsui1
1Department of Engineering, Shizuoka University, Japan, 2Japan Atomic Energy Agency
2017-e-46p
Temperature Measurement by Bremsstrahlung Radiation from Laser Sustained Plasma using Diode Laser
Takahiro Ono, Koji Nishimoto, Makoto Matsui
Department of engineering, Shizuoka University, Japan
2017-e-47p
Modeling of Explosive Detonation by Flyer Impact in Microscale Exploding Foil Initiator System
Kyoungjin Kim1, Kyu-Hyoung Kim2, Seung-gyo Jang3
1Department of Mechanical System Engineering, Kumoh National Institute of Technology, Korea, 2Defense R&D Center, Hanwha Corporation, 3Agency for Defense Development
2017-f-103p
Design and Implementation of Single Event Latch-up Measurement and Self-Recovery System for BIRDS CubeSat
Abdulla Hil Kafi, BIRDS Project Members, BIRDS Partners, George Maeda, Sangkyun Kim, Hirokazu Masui , Mengu Cho
Laboratory of Spacecraft Environment Interaction Engineering, Kyushu Institute of Technology, Japan , Japan
2017-f-104p
Design of Reel-Type Tether-Deployment Mechanism in the Satellite STARS-E for Verifying Space Elevator Technology
Kenji Nakashima1, Yoshiki Yamagiwa1, Masahiro Nohmi1, Yoshio Aoki2
1Department of engineering, University of Shizuoka, Japan, 2Department of science and engineering, University of Nihon
2017-h-25p
Spectral emissivity measurements of molten metals with an Electrostatic Levitation Furnace
Yuki Watanabe1, Haruka Tamaru2, Junpei T Okada3, Takehiko Ishikawa2, Takehiko Ishikawa4
1Advanced Engineering Services Co., Ltd., Japan, 2Japan Aerospace Exploraton Agency, 3Tohoku University, 4SOKENDAI (The Graduate University for Advanced Studies)
2017-j-26p
CONCEPT OF CONTINUOUS SPACE COMMUNICATION USING RELAY STATION
Nadeem Alam
Department of Aeronautical Engineering, Babu Banarasi Das National Institute of Technology and Management , India
2017-j-27p
A Studies on Beam Propagation Simulations for Optical Systems of Free Space Optical Communications
Hiroki Yamashita, Yoshihisa Takayama
Department of Communication Network Engineering, Tokai University, Japan
2017-j-28p
Estimation of data transmission quality under atmospheric effects in free-space laser communication
Eiji Taira, Yosihisa Takayama
Department of Information and Communication , University of Tokai, Japan
2017-j-29p
Studies on optical link establishment by using retro-reflector in free-space optical
Keiji Oda, Keiji Oda, Yoshihisa Takayama
Department of Information and communication engineering , University of Tokai, Japan
2017-j-30p
Studies on measurement accuracy of propagation direction of light and beam wonder by monitoring its scattering
Anzu Sano, Keiji Oda, Yoshihisa Takayama
Department of Communication and engneering, University of Tokai, Japan
2017-j-31p
Considerations of Optical Communication link design between the earth and Mars
Yuta Ishizuka, Yoshihisa Takayama
Department of Information and Communication Technology, Tokai University, Japan
2017-k-63p
Ganymede Laser Altimeter (GALA) for the JUICE mission: Performance model simulation
Hiroshi Araki1, Ko Ishibashi2, Noriyuki Namiki1, Hirotomo Noda1, Gregor Steinbruegge3, Kay Lingenauber3, Hauke Hussmann3, Masanori Kobayashi2, Keigo Enya4, Kazuyuki Touhara4, Masanobu Ozaki4, Takahide Mizuno4, Yoshibumi Saito4, Shouko Oshigami5, Shingo Kashima1, Jun Kimura6, Shingo Kobayashi7, Alexander Stark3, Christian Althaus3, Simone del Togno3
1RISE, National Astronomical Observatory of Japan, Japan, 2PERC, Chiba Institute of Technology, 3Deutsches Zentrum für Luft- und Raumfahrt (DLR), 4ISAS/JAXA, 5Kogakuin University, 6Osaka University, 7National Institute of Radiological Sciences
2017-k-64p
Science Objectives of the Ganymede Laser Altimeter (GALA) for the JUICE mission
Jun Kimura1, Shunichi Kamata2, Koji Matsumoto4, Shoko Oshigami3, Noriyuki Namiki4, Kiyoshi Kuramoto2, Sho Sasaki1, Keigo Enya5, Masanori Kobayashi6, Shingo Kobayashi7, Hiroshi Araki4, Hirotomo Noda4, Ko Ishibashi6, Hauke Hussmann8, Kay Lingenauber8, Yoshifumi Saito5
1Department of Earth and Space Science, Osaka University, Japan, 2Hokkaido University, 3Kogakuin University, 4National Astronomical Observatory Japan, 5JAXA, 6Chiba Institute of Technology, 7National Institute of Radiological Sciences, 8German Aerospace Center
2017-k-65p
Optical/Structural/thermal design for the receiver part of the Ganymede Laser Altimeter (GALA) for the JUICE mission
Keigo Enya
ISAS, JAXA, Japan
2017-m-19p
DC electric field measurement in the mid-latitude ionosphere by S-520-26 sounding rocket
Atsushi Yamamoto
Department of information system engineering, Toyama Prefectural University, Japan
2017-m-20p
Analysis of propagation characteristic of MF band radio waves observed by S-301-40 sounding rocket
Oka Daiki
Department od information system engineering, Toyama prefectural university, Japan
2017-n-43p
Aerosol retrieval from ADEOS-2 to GCOM/SGLI
Masayoshi Yasumoto2, Itaru Sano3, Makiko Nakata1, Sonoyo Mukai2
1Faculty of Applied Sociology, Kindai University, 2The Kyoto College of Graduate Studies for Informatics, Japan, 3Faculty of Science and Engineering, Kindai University
2017-n-44p
Evaluation of Availability of Measurements for Rice Paddy Using RedEdge Band
Mitsunori Ishihara1, Kenlo Nasahara2, Takeo Tadono1
1Japan Aerospace Exploration Agency, Japan, 2University of Tsukuba
2017-q-15p
DEVELOPMENT OF NEXT GENERATOIN LITHIUM-ION CELLS FOR SPACECRAFT
Makoto Kawase1, Hitoshi Naito1, Yuki Nakajima1, Chisa Yamada1, Masazumi Segawa2, Hiroaki Kusawake1
1Research and Development Directorate, Japan Aerospace Exploration Agency, Japan, 2GS Yuasa Technology Ltd, Japan
2017-q-16p
A primary study of windmill structure for planetary exploration
Kanata Ogiso1, Hideto Mashidori2
1Department of Mechanical Engineering, Toyohashi University of Technology, Japan, 2Aerospace Engineering Course, Tokyo Metropolitan College of Industrial Technology
2017-q-17p
Pseudo-Resonator Method for Power Delivery through Metal Barriers based on Magnetic Resonance Coupling
Kohei Shimamura, Keisuke Ohno, Shigeru Yokota
University of Tsukuba, Japan
2017-q-18p
Wireless power tramsmission for the small space satellite via Magnetic resonant coupling
Kohei Shimamura, Naoki Kuwabara, Keisuke Ohno, Shigeru Yokota
University of Tsukuba, Japan
2017-q-19p
A 94 GHz rectifier and a waveguide-to-microstrip transducer development towards wireless power transmission
Kohei Shimamura2, Kosumo Matsui1, Waku Hatakeyama1, Yuki Okamoto1, Ayako Mizushima1, Hiroyuki Koizumi1, Kimiya Komurasaki1
1The University of Tokyo, 2University of Tsukuba, Japan
2017-r-60p
Unfording analysis for space webs with pseudo-flexural elements
Chen Qing quan, Zhang qing bin, Tang Qian gang, Feng Zhi wei, Ge Jian quan, Peng Wu yu, Zhang Bin, Gao Qing yu, Wang Yong
College of Aerospace Science and Engineering, National University of Defense Technology, China
2017-r-61p
A Flexible Arm Joint and An End-effector for Space Debris Capture
Shin-Ichiro Nishida, Daisuke Uenaka, Atsufumi Shimizu, Shintaro Nakatani
Department of Mechanics and Aerospace Engineering, Tottori University graduate school, Japan
2017-r-62p
Investigation of impulse characteristics by repetitive laser ablation for space debris deorbiting
Hisashi Tsuruta1, Yusuke Katagiri1, Oskar Dondelewski2, Bin Wang1, Akihiro Sasoh1
1Department of Aerospace Engineering, Nagoya University, Japan, 2Imperial College London
2017-r-63p
The Analytical Solution for Geosynchronous Objects
SHENGXIAN YU, Changyin Zhao
Division of Applied Celestial Mechanics and Space Object & Debri Research, Purple Mountain Observatory, CAS, China
2017-r-64p
Examination of Retro-reflective Marker for Docking Interface of On-orbit Service
Ippei Takahashi, Hiroki Kato, Satoshi Suzuki, Toru Yamamoto
Research and Development Directorate, Japan Aerospace Exploration Agency, Japan
2017-r-65p
Graphical Methodology for the Preliminary Design of an Ion-Beam Shepherd Mission Using Operational Envelopes
Hodei Urrutxua1, Claudio Bombardelli2
1Astronautics Group, University of Southampton, UK, 2Space Dynamics Group, Technical University of Madrid
2017-r-66p
Development of a Twine Gripper for Debris-Capture
Hiroki Nakanishi, Keisuke Taga, Takaya Ozawa, Mitsushige Oda
Department of Mechanical Engineering, Tokyo Institute of Technology, Japan
2017-r-67p
Simulation of Space Nets with Nonlinear Material Behaviour, Capturing Space Debris
Pavel M. TRIVAILO1, Hirohisa Kojima2
1School of Engineering, RMIT University, Australia, Australia, 2Department of Aerospace Engineering, TMU University, Japan
2017-r-68p
3D hybrid Particle-In-Cell Simulation of the Magnetic Shield for Protecting a Spacecraft from Cosmic Radiation
Kouki Fukui1, Daiki Tanaka2, Yoshihiro Kajimura2
1Advanced Course of Mechanical and Electronic System Engineering, National Institute of Technology, Akashi College, Japan, 2Department of Electrical and Computer Engineering, National Institute of Technology, Akashi College
2017-r-69p
Forecasting Solar Activity from Background and Sunspot Magnetic Field Variations Using Neural Networks
Alejandro Macario Rojas, Katharine Lucy Smith
School of Mechanical, Aerospace and Civil Engineering, University of Manchester, UK
2017-r-70p
On-orbit Results of the Photoelectron Current (PEC) Measurement System On-board Horyu-IV Satellite
Essien Sampson Ewang, Kazuhiro TOYODA, Mengu CHO
Laboratory of Spacecraft Environment INteraction Engineering (LaSEINE), Kyushu Insttute of Technology,Japan, Japan
2017-r-71p
Measuring 5.8GHz-band microwave emission from hypervelocity impacts of different combinations of projectile and target materials
Yuki Mando1, Ryohei Sakamoto2, Koji Tanaka3, Masatake Kawada1, Eriko Soma3, Ichiro Shiota4, Hiroki Kurita5, Takayuki Hirai6
1Department of Electrical and Electronic Engineering, Tokushima University, Japan, 2Hosei University, 3JAXA/ISAS, 4Kogakuin University, 5Shizuoka University, 6JAXA
2017-w-20p
Key points of lean satellite safety design and verification
Takashi Yamauchi, Daiki Yamaguchi, Sangkyun Kim, Hirokazu Masui, Mengu Cho
Department of Laboratory of Spacecraft Environment Interaction Engineering, Kyushu Institute of Technology, Japan
2017-w-21p
Maintenance Strategy Analysis of a Multi-State Redundant System for Satellite
chao-hui huang1, Chun-Ho Wang2, Yo-Yang Lin3
1Department of Applied Science, Naval Academy, Taiwan, 2Department of Power Vehicle and Systems Engineering, CCIT, National Defense University, 3Systems Development Center, National Chung-Shan Institute of Science and Technology