Final 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 Masayuki Takahashi (Tohoku University, Japan)
Hitoshi Kuninaka (JAXA, Japan)
2017-o-1-01 ( 9:20 – 9:40 )
Nuclear Electric Propulsion to EUROPA and MARS
Frank Jansen1, Tim Brandt1, Volker Maiwaldt1, Frédéric Masson2, Stephane Oriol2, Jean-Claude Worm3, Emmanouil Detsis3, Francois Lassoudierre4, Richard Granjon5, Maria Cristina Tosi6, Simona Ferraris6, Anatoly S. Koroteev7, Alexander V. Semenkin7, Alexander Solodukhin7, Tim Tinsley8, James Ap. Findlay8, Zara Hodgson8, Lamartine Nogueira Frutuoso Guimarães9
1DLR Institute of Space Systems, Bremen, 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, Tokyo, Japan, 2Department of Applied Mechanics and Aerospace Engineering, Waseda University, Tokyo, Japan, 3Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
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 Frank Jansen (DLR, Germany)
Hiroyuki Koizumi (The University of Tokyo, Japan)
2017-o-1-06 ( 11:00 – 11:20 )
Investigation of Scaling Laws for Electrical Thrusters by Use of Particle-in-Cell Simulations
Tim Brandt1,3,4, Ralf Schneider2, Julia Duras2,6, Daniel Kahnfeld2, Franz Georg Hey5, Holger Kersten4, Frank Jansen1, Nils Haverland7, Jonas Pawlik7, Claus Braxmaier1,3
1DLR, Institute of Space Systems, Bremen, Germany, 2Institute of Physics, Ernst-Moritz-Arndt University Greifswald, Greifswald, Germany, 3Center of Applied Space Technology an Microgravity, University of Bremen, Bremen, Germany, 4Institute of Experimental and Applied Physics, University of Kiel, Kiel, Germany, 5Airbus Defence and Space, Claude-Dornierstraße 1, Immenstaad, Germany, 6Department of Applied Mathematics, Physics and Humanities, Nuremberg Institute of Technology, Nuremberg, Germany, 7University of Bremen, 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
1School of Engineering, Chukyo University, Nagoya, , Japan, 2Advanced Technology R&D Center, MELCO, Amagasaki, Japan
2017-o-1-08 ( 11:40 – 12:00 )
Two-Head Operations of Hall Thruster
Tomohiro Kita, Takeshi Miyasaka, Masahiro Sakoda, Yoshimi Miyake, Kazuya Oishi, Ryo Kawamura, Yuki Mamiya, Kohei Kurita, Hiroki Kanie, Makoto Asahara
Gifu University, Japan
[o-2-1] Launch Vehicle for Small Spacecrafts (1)
Session Date June 6 (Tue) 9:00 – 10:20
Room Meeting Room 7
Chairpersons Kenji Fujii (JAXA, Japan)
Shigeru Aso (Kyushu University, Japan)
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
Japan Aerospace Exploration Agency (JAXA), Sagamihara/Tsukuba, Japan
2017-o-2-02 ( 9:20 – 9:40 )
Epsilon Launch Vehicle – Second Flight and its Evolutions
Tatsuya Kanechika1, Yasunobu Segawa1, Kazuhiro Yagi1, Takayuki Imoto2
1IHI AEROSPACE Co.Ltd.(IA), Japan, 2Institute of Space and Astronautical Science, JAXA, Japan
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
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2Solid Propulsion Office, Rocket Systems Department., IHI Aerospace, Tomioka, Japan
2017-o-2-04 ( 10:00 – 10:20 )
Development and Flight Results of Structure Subsystem for Enhanced Epsilon Launch Vehicle
Hiroshi Ikaida1, Kyoichi Ui1, Ryoma Yamashiro1, Takayuki Imoto1, Yasuhiro Morita2
1Tsukuba Space Center, JAXA, Tsukuba, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
[o-2-2] Launch Vehicle for Small Spacecrafts (2)
Session Date June 6 (Tue) 11:00 – 12:00
Room Meeting Room 7
Chairpersons Atsushi Murakami (IHI AEROSPACE Co., Ltd., Japan)
Kazuhide Mizobata (Muroran Institute of Technology, Japan)
2017-o-2-05 ( 11:00 – 11:20 )
Conceptual Study of Japan’s Future Solid Rocket System
Ryoma Yamashiro1, Shinichiro Tokudome2, Yasuhiro Saitoh1, Takayuki Yamamoto2, Yoshitaka Mochihara1, Hiroki Ikaida1
1Tsukuba Space Center, JAXA, Tsukuba, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
2017-o-2-06 ( 11:20 – 11:40 )
Initial Guess Generation Strategies for Spaceplane Trajectory Optimisation
Federico Toso, Christie Maddock
Aerospace Centre of Excellence, University of Strathclyde, Glasgow, United Kingdom
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., Akabira, Japan, 2Katazen Corporation, Aichi, Japan, 3The Institute of Space and Astronautical Science, Sagamihara, Japan, 4Hokkaido Aerospace Science and Technology Incubation Center, Sapporo, Japan
[o-3-1] Future Space Transportation System (1)
Session Date June 6 (Tue) 14:00 – 15:40
Room Meeting Room 7
Chairpersons Wataru Sarae (JAXA, Japan)
Takahiro Fujikawa (Kyushu Institute of Technology, Japan)
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, JAXA, Sagamihara, 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, Sagamihara, Japan, 2Department of Space Flight Systems, Institute of Space and Astronautical Science (ISAS), JAXA, Sagamihara, Japan
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
1Yokohama National University, Yokohama, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
2017-o-3-04 ( 15:00 – 15:20 )
Computational Study on Finned Reusable Rocket during Turnover
Takuya Aogaki1, Keiichi Kitamura1, Satoshi Nonaka2
1Graduate School of Engineering, Yokohama National University, Kanagawa, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
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, JAXA, Sagamihara, Japan, 2IHI Corporation, Tokyo, Japan
[o-3-2] Future Space Transportation System (2)
Session Date June 6 (Tue) 16:00 – 17:20
Room Meeting Room 7
Chairpersons Koki Kitagawa (JAXA, Japan)
Hiroshi Ikaida (Japan Aerospace Exploration Agency, Japan)
2017-o-3-06 ( 16:00 – 16:20 )
Low Cost Reusable 1st Stage Launch Services From International Spaceports
Charles J. Lauer
Rocketplane Global, Inc. USA
2017-o-3-07 ( 16:20 – 16:40 )
Preliminary Mission Analysis of a Commercial Lunar Transportation System
Chit Hong Yam, Takeshi Hakamada, Mohamed Ragab
ispace Inc., Tokyo, 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
Co-founder of ‘Astronautical Society of Taiwan’ and ‘The Consortium of Extreme and Space Settlements’, Member of ‘宇宙建築の会 (Uchu Kenchiku no Kai)’, Space Architecture Activist, MEng.
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, Shoji Sato1, Kiyotoshi Otsuka2, Yoji Ishikawa2
1Shizuoka University, Hamamatsu, Japan, 2Obayashi Co., Tokyo, Japan
[o-3-3] Future Space Transportation System (3)
Session Date June 7 (Wed) 9:00 – 10:40
Room Meeting Room 7
Chairpersons Huai-Chien Chang (Consortium of Extreme and Space Settlements, Astronautical Society of Taiwan, Taiwan)
Yusuke Maru (Japan Aerospace Exploration Agency, Japan)
2017-o-3-10 ( 9:00 – 9:20 )
Conceptual Design Investigation and Aerodynamic Study for Hypersonic Vehicle Baseline Configuration both for TSTO and HST
Takaaki Hirayama, Yasuhiro Tani, Shigeru Aso
Department of Aeronautics and Astronautics, Kyushu University, Fukuoka, Japan
2017-o-3-11 ( 9:20 – 9:40 )
Multi-Objective Design Optimization of RBCC-Based Orbital TSTO Space Transportation Systems for Multi-Asset Deployment
George Coulloupas1,2, Hideaki Ogawa1
1School of Engineering, Royal Melbourne Institute of Technology, Melbourne, Victoria, Australia, 2Aerospace Systems Pty. Ltd., Prahran, Victoria, Australia
2017-o-3-12 ( 9:40 – 10:00 )
Detailed Design of 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
1Kyushu Institute of Technology, Japan, 2Japan Aerospace Exploration Agency (JAXA), Japan
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), Japan
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, Kitakyushu, Japan
[o-4-1] Oxygen/Methane Rocket Combustion and Heat Transfer (1)
Session Date June 6 (Tue) 9:00 – 10:00
Room Meeting Room 8
Chairpersons Simona Silvestri (Technical University of Munich, Germany)
Michael Boerner (DLR, Germany)
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 Roth, Simona Silvestri, Nikolaos Perakis, Oskar Haidn
Technical University of Munich, Institute for Turbomachinery and Flight Propulsion, 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 Combustors
Yu Daimon1, Hideyo Negishi1, Takenori Nakajima2, Roman Keller3, Peter M. Gerlinger3
1Research and Development Directorate, JAXA, Tsukuba, Japan, 2Ryoyu Systems Co., Ltd., Nagoya, Japan, 3Institute of Combustion Technology for Aerospace Engineering, University of Stuttgart, Stuttgart, Germany
2017-o-4-04 ( 9:40 – 10:00 )
Numerical Investigation of Eigenmode Damping Rates in a Single Element Rocket Combustion Chamber
Alexander Chemnitz, Nancy Kings, Moritz Schulze, Thomas Sattelmayer
Institute of Thermodynamics, Technische Universität München, Munich, Germany
[o-4-2] Oxygen/Methane Rocket Combustion and Heat Transfer (2)
Session Date June 6 (Tue) 11:00 – 12:40
Room Meeting Room 8
Chairpersons Christof Martin Roth (Technical University of Munich, Germany)
Oskar Haidn (Technical University of Munich, Germany)
2017-o-4-06 ( 11:00 – 11:20 )
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
1Japan Aerospace Exploring Agency,Tukuba Japan, 2IHI Corporation,Tokyo Japan, 3IHI Aerospace,Gumma Japan
2017-o-4-07 ( 11:20 – 11:40 )
Laser Ignition of a Multi-injector LOX/methane Combustor
Michael Börner1, 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, Austria
2017-o-4-08 ( 11:40 – 12:00 )
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
1Research and Development Directorate, JAXA, Japan, 2Space Systems Department, IHI Aerospace Co., Ltd., Tomioka, Japan, 3Research Division of Machining and Molding, Osaka Research Institute of Industrial Science and Technology, Izumi, Japan, 4Department of Materials Processing, Tohoku University, Sendai, Japan
2017-o-4-09 ( 12:00 – 12:20 )
Experimental and Numerical Investigation of a Multi-Injector GOX-GCH4 Combustion Chamber
Simona Silvestri1, Christoph Kirchberger2, Gregor Schlieben1, Maria Palma Celano1, Oskar Haidn1
1Technical University of Munich, Munich, Germany, 2German Aerospace Center, Lampoldshausen, Germany
2017-o-4-11 ( 12:20 – 12:40 )
Numerical Investigation on Effects of Recess Variation upon a GCH4/GOX Shear Coaxial Combustion Chamber
Yu Daimon1, Hiroshi Terashima2, Hiroumi Tani1
1Research and Development Directorate, JAXA, Tsukuba, Japan, 2Faculty of Engineering, Hokkaido University, Sapporo, Japan
[o-5-1] Hybrid Rocket for Space Transportation
Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 6
Chairpersons Changjin Lee (Konkuk University, Korea)
Daisuke Nakata (Muroran Institute of Technology, Japan)
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, Sagamihara, 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, Lampoldshausen, D-74239 Hardthausen, Germany, 2Bayern-Chemie GmbH, D-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 Schmierer1,2, Mario Kobald1, Johan Steelant3, Stefan Schlechtriem1,2
1Institute of Space Propulsion, German Aerospace Center (DLR), Lampoldshausen, Germany, 2Institute of Space Systems (IRS), University of Stuttgart, Germany, 3European Space Research and Technology Centre (ESTEC), European Space Agency (ESA), Netherlands
2017-o-5-04 ( 10:20 – 10:40 )
Error Analysis for CAMUI Type Hybrid Rocket Regression Simulation
Tor Viscor, Harunori Nagata
Hokkaido University, Japan
[o-5-2] Development and Testing of Hybrid Rocket
Session Date June 6 (Tue) 11:00 – 12:40
Room Meeting Room 6
Chairpersons Helmut K. Ciezki (DLR – German Aerospace Center, Germany)
Toru Shimada (JAXA, Japan)
2017-o-5-05 ( 11:00 – 11:30 )
Development of an Airbreathing Hybrid Rocket Booster
Yen-Sen Chen, J.W. Lin, S.S. Wei
TiSPACE Incorporated, Chunan, Taiwan
2017-o-5-06 ( 11:30 – 12:00 )
A Record Flight of the Hybrid Sounding Rocket HEROS 3
Mario Kobald1,2, Christian Schmierer1,2, Ulrich Fischer1,2, Konstantin Tomilin1,2, Anna Petrarolo1
1Institute of Space Propulsion, DLR, Hardthausen, Germany, 2Institute of Space Systems, Stuttgart University, Stuttgart, Germany
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 Obata, Toru Shimada
Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
[o-5-3] Internal Flow Dynamics of Hybrid Rocket
Session Date June 6 (Tue) 14:00 – 15:40
Room Meeting Room 6
Chairpersons Yen-Sen Chen (TiSPACE Incorporated, Taiwan)
Toru Shimada (JAXA, Japan)
2017-o-5-09 ( 14:00 – 14:30 )
Internal Flow Dynamics and Stability in Hybrid Rocket Combustor with Swirl
Sulha Lee, Jung Eun Kim, Changjin Lee
Department of Aerospace Information Eegineering, 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 Aso1, Yasuhiro Tani1, Masato Yamashita1, Kazuya Komori1, Tomohiro Yamasaki1, Toru Shimada2
1Department of Aeronautics and Astronautics, Kyushu University, Fukuoka, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, 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
Institute of Space and Astronautical Science, JAXA, Sagamihara, 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
1Department of Aeronautics and Astronautics, Tokai University, Hiratsuka, Japan, 2Aerospace Engineering, University of Brasília, Brasília, Brazil
[o-5-4] Elemental Technologies for Hybrid Rocket
Session Date June 6 (Tue) 16:00 – 17:40
Room Meeting Room 6
Chairpersons Shigeru Aso (Kyushu University, Japan)
Christian Schmierer (German Aerospace Center, Germany)
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 )
N2O Flow History Prediction in an Oxidizer Feed Line of Hybrid Rockets
Daisuke Nakata1, Kazuki Yasuda1, Kugo Okada1, Kazuyuki Higashino1, Rikio Watanabe2
1Muroran Institute of Technology, Hokkaido, Japan, 2Tokyo City University, Tokyo, Japan
2017-o-5-15 ( 16:40 – 17:00 )
Thermo-fluid Analysis of Hybrid Rocket with LOX Regenerative Cooling System
Tomoki Matsuno, Toru Shimada
Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
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 Response Characteristics of Axial-Injection End-Burning Hybrid Rockets
Yuji Saito1, Masaya Kimino1, Ayumu Tsuji1, Kazunobu Omura1, Hiroyuki Yasukochi2, Kentaro Soeda2, Tsuyoshi Totani3, Masashi Wakita3, Harunori Nagata3
1Department of Space Engineering, Hokkaido University, Sapporo, Japan, 2Institute for Photon Science and Technology, The University of Tokyo, Tokyo, Japan, 3Faculty of Engineering, Hokkaido University, Sapporo, Japan
[o-5-5] Fuels for Hybrid Rocket
Session Date June 7 (Wed) 9:00 – 10:40
Room Meeting Room 6
Chairpersons Toru Shimada (JAXA, Japan)
Mario Kobald (DLR, Germany)
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, Chiba, Japan, 2Katazen Corporation, Aichi, Japan, 3Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
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 Kumasaki2
1Department of Aerospace Engineering, College of Science and Technology, Nihon University, Chiba, Japan, 2Department of Chemistry, Chemical Engineering and Bioscience, School of Engineering Science, Graduate School, Yokohama National University,Kanagawa, Japan
2017-o-5-20 ( 9:40 – 10:00 )
Regression Rate Improvement of Hybrid Rocket Fuel by Addition of The Magnesium Powder
Akira Takatashi, Raimu Kobayashi, Takamori Yamaguchi, Yuki Komori, Kenichi Takahashi
Department of Aerospace Engineering, College of Science and Technology, Nihon University, Chiba, Japan
2017-o-5-21 ( 10:00 – 10:20 )
Study on Wax Fuel for Hybrid Rockets
Taira Ishigaki1, Ichiro Nakagawa2
1Graduate School of Engineering, Tokai University, Japan, 2Department of Aeronautics and Engineering, Tokai University, Japan
2017-o-5-22 ( 10:20 – 10:40 )
Experimental Investigate of Fuel Regression Rate in Low Melting Point Temperature Thermoplastic Fuels Hybrid Rocket Using the Altering Swirling Oxidizer Flow
Yo Kawabata1, Ayana Banno1, Yutaka Wada1, Kohei Ozawa2, Toru Shimada3, Nobuji Kato4, Keiichi Hori3, Ryo Nagase1
1Chiba Institute of Technology, Narashino, Japan, 2Kyushu Institute of Technology, Kitakyushu, Japan, 3Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 4Katazen Corporation, Oobu, Japan
Technical Session Oral
[a-1] Liquid Propellant 1
Session Date June 7 (Wed) 11:00 – 11:40
Room Meeting Room 6
Chairpersons Shinji Nakaya (The University of Tokyo, Japan)
Oskar J. Haidn (Technical University of Munich, Germany)
2017-a-03 ( 11:00 – 11:20 )
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
1IHI Corporation, Tomioka-shi, Japan, 2Japan Aerospace Exploration Agency, Tsukuba-shi, Japan
2017-a-04 ( 11:20 – 11:40 )
Experiment Result of Turbopump for Small Thrust LOX/Methane Rocket Engine
Taiichi Motomura1, Hiroyuki Sakaguchi1, Toru Tsukano1, Toshiki Kato2, Hideaki Nanri2, Toshiki Morito2, Ideo Masuda2
1IHI Corporation, Tokyo, Japan, 2Japan Aerospace Exploring Agency, Tsukuba, Japan
[a-2] Liquid Propellant 2
Session Date June 7 (Wed) 16:00 – 17:00
Room Meeting Room 6
Chairpersons Mitsuaki Tanabe (Nihon University, Japan)
Takeo Tomita (Japan Aerospace Exploration Agency, Japan)
2017-a-05 ( 16:00 – 16:20 )
Boreas Demonstrator for Next Generation Engines
Ariane Deneuve1, Stephanie Dreyer1, Erwan Humbert1, Louise Lesaunier1, Didier Guichard1, Alban DU Tertre1, Vincent Leudiere2, Marie Theron2, Julien Herpe2
1Airbus Safran Launchers, France, 2CNES Launcher Directorate, France
2017-a-06 ( 16:20 – 16:40 )
Uncertainty Analysis as Applicable to a Miniature Cryogenic Test Stand for Rocket Research
Brunno Vasques, Oskar 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 H. S. Hahn, Jan Deeken, Stefan Schlechtriem
German Aerospace Center DLR, Institute of Space Propulsion, Germany
[a-3] Flow Dynamics
Session Date June 8 (Thu) 9:00 – 10:40
Room Meeting Room 6
Chairpersons Takehiro Himeno (The University of Tokyo, Japan)
Hideyo Negishi (JAXA, Japan)
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 Aerospace Center (DLR), Lampoldhausen, Germany
2017-a-11 ( 9:20 – 9:40 )
Validation of a Lattice Boltzmann Model for Transient Cryogenic Two-Phase Flow
Tobias Traudt, Stefan Schlechtriem
Institute of Space Propulsion, German Aerospace Center, DLR, Hardthausen, 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 Uchiumi3
1Japan Aerospace Exploration Agency, Kakuda, Japan, 2East Japan Star Works Co., Ltd., Kakuda, Japan, 3Muroran Institute of Technology, Muroran, Japan
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, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
2017-a-14 ( 10:20 – 10:40 )
Tubular Equivalent Regression Rate in Hybrid Rockets with Complex Geometries
Landon Kamps1, Tor Viscor1, Ryo Yamaguchi1, Yurika Kiyotani1, Kazuhito Sakurai1, Tsuyoshi Totani2, Masashi Wakita2, Harunori Nagata2
1Department of Mechanical and Space Engineering, Hokkaido University, Sapporo, Japan, 2Faculty of Engineering, Hokkaido University, Sapporo, Japan
[a-4] Combustion Instability
Session Date June 8 (Thu) 11:00 – 12:40
Room Meeting Room 6
Chairpersons Justin Steven Hardi (Institute of Space Propulsion, Germany)
Daisuke Nakata (Muroran Institute of Technology, Japan)
2017-a-15 ( 11:00 – 11:20 )
Interpretation of the Response of Cryogenic Rocket Flames to Forced Acoustics using Large Eddy Simulation
Justin Hardi1, Youhi Morii2, Scott Beinke1,3, Taro Shimizu2, Hideto Kawashima4, Michael Oschwald1,5
1Institute of Space Propulsion, DLR, Lampoldshausen, Germany, 2JEDI Center, JAXA, Kanagawa, Japan, 3School of Mechanical Engineering, The University of Adelaide, Adelaide, Australia, 4Space Technology Directorate I, JAXA, Tsukuba, Japan, 5Institute of Jet Propulsion and Turbomachinery, RWTH, Aachen, Germany
2017-a-16 ( 11:20 – 11:40 )
Dynamics and Mixing Characteristics of a Coaxial Jet-Swirl Injector
Jinhyun Bae1, Taesung Kim1, Seokgyu Jeong1, Chanyeong Jeong2, Jaye Koo3, Youngbin Yoon1,4
1Department of Mechanical and Aerospace Engineering, Seoul National University, Seoul, Korea, 2Mechatronics R&D Center, Samsung Electronics Co., Ltd., Gyeonggi-do, Korea, 3School of Mechanical and Aerospace Engineering, Korean Aerospace University, Gyeonggi-do, Korea, 4The Institute of Advanced Aerospace Technology, Seoul National University, Seoul, 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, The University of Tokyo, Tokyo, Japan, 2Interstellar Technologies Inc., Hokkaido, Japan, 3Kakuda Space Center, Japan Aerospace Exploration Agency, Japan
2017-a-18 ( 12:00 – 12:20 )
Flame Visualization within a Rocket Combustion Chamber without Film Cooling System
Shougo Ozaki1, Youhei Kino2, Yoshio Nunome1, Sadatake Tomioka1, Takeo Tomita1
1Kakuda Space Center, Japan 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
Mitsuaki Tanabe
College of Science and Technology, Nihon University, Funabashi, Japan
[a-5] Air-breathing Engine
Session Date June 8 (Thu) 14:00 – 15:40
Room Meeting Room 6
Chairpersons Kazuhiro Ishii (Yokohama National University, Japan)
Kazuki Sakaki (The University of Tokyo, Japan)
2017-a-20 ( 14:00 – 14:20 )
Squeeze Damper Improvement for Reducing Vibration in Gas Turbine Engine Testing
Ming-Chung Lo1, Chien-Chun Hung2
1Department of Mechanical and Aerospace Engineering Chung Cheng Institute of Technology, National Defense University, Taoyuan, Taiwan, R.O.C., 2Department of Aeronautical and Opto-Mechatronic Engineering, Vanung University, Taoyuan, Taiwan, R.O.C.
2017-a-21 ( 14:20 – 14:40 )
Research on Fuel Mixing in a Non-reacting Situation Simulating a Dual-mode Combustor
Takuya Arakawa1, Sadatake Tomioka2
1Department of Aerospace Engineering, Tohoku University, Miyagi, Japan, 2Advanced Propulsion Research Group, JAXA, Miyagi, Japan
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
1Kakuda Space Center, 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
Shingo Shichiri, Yamato Tsukazaki, Kazuma Hashimoto, Shoji Sakaue, Takakage Arai
Department of Aerospace Engineering, Osaka Prefecture University, Sakai, Osaka, 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
1Waseda University, Tokyo, Japan, 2Japan Aerospace Exploration Agency, Chofu, Japan, 3The University of Tokyo, Tokyo, Japan
[a-6] Solid Propellant
Session Date June 8 (Thu) 16:00 – 17:40
Room Meeting Room 6
Chairpersons Masafumi Tanaka (National Defense Academy, Japan)
Akira Kakami (University of Miyazaki, Japan)
2017-a-25 ( 16:00 – 16:20 )
High Density Composite Propellants for the Upper Stage Rocket Motor
Kotaro Matsumoto1, Akihiro Iwasaki2, Hiroto Habu1
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2Development of Space and Astronautical Science, SOKENDAI (The Graduate University for Advanced Studies), Sagaminahra, Japan
2017-a-26 ( 16:20 – 16:40 )
Continuous Kneading of AP Composite Propellant Slurry by an Peristaltic Artificial Muscle Mixer
Akihiro Iwasaki1, Shun Yoshihama2, Naomasa Hosomi3, Kyota Ashigaki2, Kana Otake3, Kotaro Matsumoto4, Yasuyuki Yamada2, Soichiro Yamaguchi3, Taro Nakamura2, Hiroto Habu4
1Department of Space and Astronautical Science, SOKENDAI, Sagamihara, Japan, 2Department of Precision Engineering, Chuo University, Bunkyo-ku, Japan, 3Department of Engineering Science, Kansai University, Suita, Japan, 4Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
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 Yoshihama1, Akihiro Iwasaki2, Kengo Tagami3, Yasuyuki Yamada4, Hiroto Habu5, Taro Nakamura4
1Graduate School of Science and Engineering, Chuo University, Japan, 2The Graduate University for Advanced Studies, Japan, 3PROGRESS TECHNOLOGIES Inc., Japan, 4Faculty of Science and Engineering, Chuo University, Japan, 5JAXA, Japan
2017-a-28 ( 17:00 – 17:20 )
Active Interruption of Motor Combustion for Ammonium-Perchlorate Composite Propellant
Yosuke Meichin, Masafumi Tanaka
National Defense Academy, Yokosuka, Japan
2017-a-29 ( 17:20 – 17:40 )
Analyzing Dispersion of Particles and Void in AP/HTPB Composite Propellant by X-ray Computed Tomography
Naomasa Hosomi1, Kana Otake1, Natsuyo Uegaki2, Akihiro Iwasaki3, Kotaro Matsumoto4, Hiroto Habu4, Soichiro Yamaguchi2
1Department of Engineering Science, Kansai University, Osaka, Japan, 2Department of Applied Physics, Kansai University, Osaka, Japan, 3Department of Space and Astronautical Science, The Graduate University for Advance Studies, Kanagawa, Japan, 4Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
[a-7] ADN
Session Date June 9 (Fri) 9:00 – 10:40
Room Meeting Room 6
Chairpersons Helmut K. Ciezki (DLR, Germany)
Yu-ichiro Izato (Yokohama National University, Japan)
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, Beijing, China
2017-a-31 ( 9:20 – 9:40 )
Preparation and Thermal Decomposition behavior of High Energy Ionic Liquids based on Ammonium Dinitramide and Amine Nitrates
Hiroki Matsunaga1, Katsumi Katoh1, Hiroto Habu2,3, Masaru Noda1, Atsumi Miyake3
1Department of Chemical Engineering, Fukuoka University, Fukuoka, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 3Institute of Advanced Sciences, Yokohama National University, Japan
2017-a-32 ( 9:40 – 10:00 )
Thermal Properties of ADN based Ionic Liquid Gel Propellants
Kento Shiota1, Yu-Ichiro Izato2, Hiroki Matsunaga3, Hiroto Habu4,5, Atsumi Miyake5
1Graduate School of Environmental and Information Sciences, Yokohama National University and Japan Society for the Promotion of Science, Yokohama, Japan, 2Graduate School of Environmental and Information Sciences, Yokohama National University, Yokohama, Japan, 3Department of Chemical Engineering, Fukuoka University, Fukuoka, Japan, 4Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 5Institute of Advanced Sciences, Yokohama National University, Yokohama, Japan
2017-a-33 ( 10:00 – 10:20 )
Laser Igniton and Thermal Property of Ammonium Dinitramide based Energetic Ionic Liquid Propellants by Including Chemical Dyes
Mamoru Hayata1, Kento Shiota1,2, Yu-Ichiro Izato1, Hiroki Matsunaga3, Hiroto Habu4, Atsumi Miyake5
1Graduate school of Environment and Information Science, Yokohama National University, Yokohama, Japan, 2Research Fellow of Japan Society for the Promotion of Science, Tokyo, Japan, 3Department of chemical engineering, Fukuoka University,Fukuoka Japan, 4Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 5Institute of Advanced Sciences, Yokohama National University, Yokohama, 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, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
[a-8] Low Toxicity
Session Date June 9 (Fri) 11:00 – 12:40
Room Meeting Room 6
Chairpersons Yutaka Wada (Chiba Institute of Technology, Japan)
Kotaro Matsumoto (Japan Aerospace Exploration Agency, Japan)
2017-a-35 ( 11:00 – 11:20 )
Investigation into Prototype of a Hydroxyalmmonium Nitrate (HAN)-based Micropropulsion System
Wai Siong Chai1, Kean How Cheah2,1, Kai Seng Koh2, Jitkai Chin1
1Department of Chemical and Environmental Engineering, University of Nottingham Malaysia Campus, Malaysia, 2School of Engineering and Physical Science, Heriot-Watt University Malaysia, Malaysia
2017-a-36 ( 11:20 – 11:40 )
A Kinetic Model for Combustion of Hydroxylammonium Nitrate (HAN)-Based Propellants
Yu-Ichiro Izato1, Mitsuo Koshi1,2, Atsumi Miyake2
1Graduate school of Environmental and Information Sciences, Yokohama National University, Yokohama, Japan, 2Institute of Advanced Science, Yokohama National University, Yokohama, Japan
2017-a-37 ( 11:40 – 12:00 )
Influence of Injector for Performance of N2O/DME Bipropellant Thruster
Takamasa Asakura1, Shouta Hayashi1, Yasuyuki Yano2, Akira Kakami2
1Department of Mechanical Design Systems Engineering, University of Miyazaki, Japan, 2Technical Center, University of Miyazaki, Japan
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, Osaka, Japan, 2Department of Medical Engineering, Tokyo City University, Tokyo, Japan, 3Splije, Ibaraki, Japan, 4Department of Aerospace Engineering, Muroran Institute of Technology, Hokkaido, Japan
2017-a-39 ( 12:20 – 12:40 )
Evaluation of Laser Ignition for HAN-based Monopropellant of RCS Thruster
Masaya Furusawa, Toshiyuki Katsumi, Satoshi Kadowaki
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 Mario Kobald (DLR, Germany)
Masashi Wakita (Hokkaido University, Japan)
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, Kakuda, Miyagi, Japan, 2Department of Mechanical Engineering, Chubu University, Aichi, Japan
2017-a-41 ( 14:20 – 14:40 )
Coupled Aerodynamic Characteristics of Airframe and Engine of Space Plane
Kanenori Kato1, Kohichi Tatkasaki1, Kouichiro Tani1, Susumu Hasegawa1, Kazuhide Mizobata2, Takeshi Kanda3
1The Research and Development Directorate, JAXA, Miyagi, Japan, 2Muroran Institute of Technology, Hokkaido, Japan, 3Chubu University, Aichi, Japan
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, Yokohama, Japan
2017-a-43 ( 15:00 – 15:20 )
Effect of Carbon Black Diameter on Performance for a Throttleable Solid Propellant Microthruster Using Laser Heating
Daich 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, Japan, 3Technical Center, University of Miyazaki, Japan
2017-a-44 ( 15:20 – 15:40 )
Design and Perfomance 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, Miyazaki, Japan, 2Department of Mechanical Systems Engineering, University of Miyazaki, Miyazaki, Japan, 3Technical Center, University of Miyazaki,, Miyazaki, Japan
[b-1] EP Activities & Missions
Session Date June 6 (Tue) 14:00 – 15:20
Room Pearl Room B
Chairpersons Juan Yang (Northwestern Polytechnical University, China)
Kimiya Komurasaki (The University of Tokyo, Japan)
2017-b-02 ( 14:20 – 14:40 )
Field Emission Cathodes for an Electrodynamic Tether Experiment on the H-II Transfer Vehicle
Yasushi Ohkawa1, Teppei Okumura1, Yuuta Horikawa2, Yoshiyuki Miura3, Satomi Kawamoto1, Koichi Inoue3
1Research and Development Directorate, JAXA, Chofu, Japan, 2Research and Development Directorate, JAXA, Tsukuba, Japan, 3Space Technology Directorate I, JAXA, Tsukuba, 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, Osaka, Japan, 2Department of Aeronautics and Astronautics, Tokai University, Kanagawa, Japan
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, Osaka, Japan, 2High Serve Inc., Tokyo, Japan
[b-2] Cathode
Session Date June 6 (Tue) 16:00 – 17:20
Room Pearl Room B
Chairpersons Hiroki Watanabe (Tokyo Metropolitan University, Japan)
Shigeru Yokota (University of Tsukuba, Japan)
2017-b-06 ( 16:00 – 16:20 )
Numerical Simulation of High Current Hollow Cathode
Kohei Kojima1, Shigeru Yokota2, Akira Osada2, Junko Yamasaki2, Moyuru Yonaha2, Tatsuya Kimura1, Yoshihiro Kawamata1, Masaaki Yasui1
1Mitsubishi Heavy Industries, Ltd, Nagoya, Japan, 2University of Tsukuba, Japan
2017-b-07 ( 16:20 – 16:40 )
Plasma Diagnosis by Langmuir Probing on High Current Hollow Cathode
Kohei Kojima1, Shigeru Yokota2, Junko Yamasaki2, Moyuru Yonaha2, Tatsuya Kimura1, Yoshihiro Kawamata1, Masaaki Yasui1
1Mitsubishi Heavy Industries, Ltd, Nagoya, Japan, 2University of Tsukuba, Japan
2017-b-08 ( 16:40 – 17:00 )
Hybrid-PIC Simulation on Thermal Characteristics of Hollow Cathode
Kenichi Kubota1, Yuya Oshio2, Hiroki Watanabe3, Shinatora Cho1, Yasushi Ohkawa4, Ikkoh Funaki5
1Aeronautical Technology Directorate, JAXA, Chofu, Tokyo, Japan, 2Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology, Koganei, Tokyo, Japan, 3Faculty of System Design, Tokyo Metropolitan University, Hino, Tokyo, Japan, 4Research and Development Directorate, JAXA, Chofu, Tokyo, Japan, 5Institute of Space and Astronautical Science, JAXA, Sagamihara, Kanagawa, Japan
2017-b-09 ( 17:00 – 17:20 )
Experimental Investigation of LaB6 Hollow Cathode with Radiative Heater
Yuya Oshio1, Kenichi Kubota2, Hiroki Watanabe3, Shinatora Cho2, Yasushi Ohkawa2, Ikkoh Funaki2
1Dpartment of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 3Department of System Design, Tokyo Metropolitan University, Tokyo, Japan
[b-3] Hall Thruster 1
Session Date June 7 (Wed) 9:00 – 10:00
Room Pearl Room B
Chairpersons Holak Kim (KAIST, Korea)
Masakatsu Nakano (Tokyo Metropolitan College of Industrial Technology, Japan)
2017-b-11 ( 9:00 – 9:20 )
Study on Suppression Method and Reliability of Pulse Current of Hall Thruster Ignition Process
Wenbo Li, Yingyong Yang, Tao Huang, Liqiu Wei, Daren Yu
Institute of Advanced Power, Harbin Institute of Technology, Harbin, People’s Republic of China
2017-b-12 ( 9:20 – 9:40 )
Performance of a 2 kW-Class Anode-Layer Thruster RAIJIN 66
Yushi Hamada1, Rei Kawashima2, Kimiya Komurasaki2, Hiroyuki Koizumi1
1Department of Advanced Energy, GSFS, The University of Tokyo, Tokyo, Japan, 2Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan
2017-b-13 ( 9:40 – 10:00 )
Operating Characteristics of Anode-layer-type Hall Thruster Using Alternative Propellant
Junko Yamasaki, Shigeru Yokota, Kohei Shimamura
University of Tsukuba, Tsukuba, Japan
[b-4] Hall Thruster 2
Session Date June 7 (Wed) 11:00 – 12:40
Room Pearl Room B
Chairpersons Yoshiyuki Takao (Nishinippon Institute of Technology, Japan)
Naoji Yamamoto (Kyushu University, Japan)
2017-b-14 ( 11:00 – 11:20 )
Effect of Indent Channel on Discharge Characteristics of a No-Wall-Loss Hall Thruster
Yongjie Ding1,2, Hezhi Sun1, Wuji Peng1, Liqiu Wei1,2
1Plasma Propulsion Lab, Institute of Advanced Power, Harbin Institute of Technology, Harbin, China, 2Electric Drive & Propulsion Technology Lab, Harbin Institute of Technology, Harbin, 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 )
Development of a Low Power Magnetic-field-tailored Hall Thruster
Holak Kim1, Seunghun Lee1,2, Keuntae Doh1, Wonho Choe1
1Korea Advanced Institute of Science and Technology (KAIST), Republic of Korea, 2Korea Institute of Materials Science (KIMS), Republic of Korea
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, Japan
2017-b-18 ( 12:20 – 12:40 )
Propellant Flow Analysis within Electric Propulsion Test Facility
Yoshinori Nakayama
Department of Aerospace Engineering, National Defense Academy, Yokosuka, Japan
[b-5] Ion Thruster
Session Date June 7 (Wed) 16:00 – 17:20
Room Pearl Room B
Chairpersons Michael Tsay (Busek Co. Inc., USA)
Yasushi Ohkawa (JAXA, Japan)
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
School of Astronautic, Northwestern Polytechnical University Xi’an, China
2017-b-20 ( 16:20 – 16:40 )
Transient Behavior of Ion Extraction and Acceleration of Variable Thrust Ion Thruster
Masakatsu Nakano1, Naoji Yamamoto2, Ikkoh Funaki3, Yasushi Ohkawa4
1Tokyo Metropolitan College of Industrial Technology, Tokyo, Japan, 2Kyushu University, Fukuoka, Japan, 3Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 4Research and Development Directorate, JAXA, Chofu, Japan
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, Yutaro Kawahara1, Kensuke Iijima1, Kouichi Ushio1, Naoji Yamamoto1, Taichi Morita1, Masakatsu Nakano2, Yasushi Ohkawa3, Ikkoh Funaki3
1Kyushu University, Japan, 2Tokyo Metropolitan College of Industrial Technology, Japan, 3JAXA, Japan
2017-b-23 ( 17:00 – 17:20 )
Numerical Analysis of a Miniature Microwave Discharge Ion Thruster Using Water as Propellant
Kengo Nakamura1, Hiroyuki Koizumi2, Yoshinori Takao3
1Department of Systems Integration, Yokohama National University, Yokohama, Japan, 2Department of Advanced Energy, The University of Tokyo, Tokyo, Japan, 3Division of Systems Research, Yokohama National University, Yokohama, Japan
[b-6] MPD Thruster
Session Date June 8 (Thu) 9:00 – 10:20
Room Pearl Room B
Chairpersons Daisuke Nakata (Muroran Institute of Technology, Japan)
Akira Iwakawa (Nagoya University, Japan)
2017-b-24 ( 9:00 – 9:20 )
Performance of 100 kW Steady State Applied-Field MPD Thruster
Adam Boxberger, Peter Jüstel, Georg Herdrich
Institute of Space Systems, University of Stuttgart, Stuttgart, 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
Shota Saito, Kengo Chino, Yoshikazu Sugiyama, Hirokazu Tahara, Kyoko Takada
Department of Mechanical Engineering, Osaka Institute Technology, Japan
2017-b-26 ( 9:40 – 10:00 )
The Effect of Anode Configuration on Hydrogen MPD Thruster Performance: A Numerical Study
Shitan Tauchi1, Akira Kawasaki2, Masakatsu Nakane3, Kenichi Kubota4, Ikkoh Funaki5
1Department of Space and Astronautical Science, SOKENDAI (The Graduate University for Advanced Studies), Sagamihara, Japan, 2Department of Aerospace Engineering, Nagoya University, Nagoya, Japan, 3Department of Aerospace Engineering, Nihon University, Funabashi, Japan, 4Aeronautical Technology Directorate, JAXA, Chofu, Japan, 5Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
2017-b-27 ( 10:00 – 10:20 )
Operation Characteristic of Applied-Field Magnetoplasmadynamics Thruster Using Hollow Cathode
Hayato Kasuga
Department of Aerospace Engineering, Nagoya University, Japan
[b-7] Simulation & Modeling
Session Date June 8 (Thu) 11:00 – 12:20
Room Pearl Room B
Chairpersons Jinyue Geng (Beijing Institute of Control Engineering, China)
Takanobu Muranaka (Chukyo University, Japan)
2017-b-28 ( 11:00 – 11:20 )
Numerical Simulation of Helicon Plasma Thruster Discharge by Fluid Model
Guangqing Xia, Qiuyun Wu, Niandong Zhou, Yajie Han, Liuwei Chen
State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, 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, Yuki Harada1, Alseny Diallo2, Kimiya Komurasaki1, Hiroyuki Koizumi1, Rei Kawashima2
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2ESI Group Japan, Tokyo, 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, Hideo Nagatomo2, Atsushi Sunahara3, Masafumi Edamoto1, Taichi Morita1, Naoji Yamamoto1, Naoya Saito1, Satoshi Miura1, Yutaro Itadani1, Shinsuke Fujioka2, Akifumi Yogo2, Hiroaki Nishimura2, Yoshitaka Mori4, Tomoyuki Johzaki5, Hideki Nakashima1
1Department of Advanced Energy Engineering Science, Kyushu University, Japan, 2Institute of Laser Engineering, Osaka University, Japan, 3Center for Materials under eXtreme Enviroment (CMUXE), School of Nucelar Engineering, Purdue Uniersity,West Lafayette, Indiana USA, 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, Yamaguchi, Japan
[b-8] Advanced Thruster 1
Session Date June 8 (Thu) 14:00 – 15:40
Room Pearl Room B
Chairpersons Guangqing Xia (Dalian University of Technology, China)
Yoshihiro Kajimura (National Institute of Technology, Akashi College, Japan)
2017-b-32 ( 14:00 – 14:20 )
Multi-objective Design Optimisation of a Small Scale Cusped Field Thruster for Micro-satellite Platforms
Angus Muffatti1, Hideaki Ogawa2
1Aerospace Systems Pty Ltd, Melbourne, Australia, 2School of Engineering, Royal Melbourne Institute of Technology, Melbourne, 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,Toshihiro Matsuguma1, Hokuto Sekine2, Shintarou Komatsu3, Hiroyasu Kurashige2, Hiroyuki Koizumi2, Kimiya Komurasaki1
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Department of Advanced Energy, The University of Tokyo, Tokyo, Japan, 3Department of Creative Informatics, The University of Tokyo, Tokyo, Japan
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, Yokohama, Japan, 2Department of Electrical Engineering, Tohoku University, Sendai, Japan, 3Division of Systems Research, Yokohama National University, Yokohama, Japan
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, School of Science, Tokai University, Hiratsuka, Japan, 2Chubu Electric Power Co., Inc., Aichi, Japan
2017-b-36 ( 15:20 – 15:40 )
Effect of Cathode Electrode Shape on Performance of Vacuum Arc Thruster
Yayoi Murakami, Kateryna Aheieva, Kazuhiro Toyoda, 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 Liqiu Wei (Harbin Institute of Technology, China)
Yuya Oshio (Tokyo University of Agriculture and Technology, Japan)
2017-b-39 ( 16:40 – 17:00 )
Multi-Coil Magnetic Sail Experiment in Laboratory
Kazuma Ueno1, Yuya Oshio2, Ikkoh Funaki3, Hiroshi Yamakawa4
1Department of Electrical and Electronic Engineering, Chukyo University, Nagoya, Japan, 2Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology, Koganei, Japan, 3Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 4Research Institute for Sustainable Humanosphere, Kyoto University, Uji, Japan
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, Hideo Nagatomo3, Atsushi Sunahara4, Tomohiko Kojima2, Naoya Saito2, Yutaro Itadani2, Yoshitaka Mori5, Tomoyuki Johzaki6, Akifumi Yogo3, Hiroaki Nishimura3, Shinsuke Fujioka3, Hideki Nakashima1, Naoji Yamamoto1
1Faculty of Engineering Sciences, Kyushu University, Kasuga, Japan, 2Interdisciplinary Graduate School of Engineering Sciences, Kyushu University, Kasuga, Japan, 3Institute of Laser Engineering, Osaka University, Japan, 4Center for Materials under eXtreme Enviroment (CMUXE), School of Nucelar Engineering, Purdue Uniersity, Indiana, USA, 5The Graduate School for the Creation of New Photonics Industries, Hamamatsu, Shizuoka, Japan, 6Graduate School of Engineering, Hiroshima University, Higashi-Hiroshima, Hiroshima, Japan
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 Kajimura1, Tatsumasa Hagiwara1, Yuya Oshio2, Ikkoh Funaki3
1Department of Electrical and Computer Engineering, Akashi National College of Technology, Akashi, Japan, 2Department of Mechanical System Engineering, Tokyo University of Agriculture and Technology, Koganei, Japan, 3Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
[b-10] Electrothermal Thruster
Session Date June 9 (Fri) 9:00 – 10:20
Room Pearl Room B
Chairpersons Koichi Mori (Nagoya University, Japan)
Hiroyuki Nishida (Tokyo University of Agriculture and Technology, Japan)
2017-b-42 ( 9:20 – 9:40 )
Research and Development of Low-power Anode-Radiation-Cooled DC Arcjet Thruster Using Water Propellants
Kazuyoshi Okuda1, Yuki Fukutome1, Suguru Shiraki1, Katsuya Shimogaito1, Takefumi Mimura1, Hirokazu Tahara1, Kyoko Takada1, Ai Momozawa2, Daisuke Nakata3, Yuichiro Nogawa4
1Department of Mechanical Engineering, Osaka Institute of Technology, Osaka, Japan, 2Department of Medical Engineering, Tokyo City University, Tokyo, Japan, 3Department of Aerospace Engineering, Muroran Institute of Technology, Hokkaido, Japan, 4Splije, Ibaraki, Japan
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, Miyazaki, Japan, 2Department of Mechanical Systems Engineering, University of Miyazaki, Miyazaki, Japan, 3Technical Center, University of Miyazaki, Japan
2017-b-44 ( 10:00 – 10:20 )
Development of Chemically Augmented Electrothermal Thrusters
Shoko Shibagaki1, Kai Wada1, Mitsutoshi Tsuchiya2, Yuka Arai2, Tomoyuki Ikeda3, Hideyuki Horisawa4
1Department of Mechanical Engineering, Graduate student, Tokai University, Kanagawa, Japan, 2Department of Aeronautics and Astronautics, Undergraduate student, Tokai University, Kanagawa, Japan, 3Department of Aeronautics and Astronautics, Associate Professor, Tokai University, Kanagawa, Japan, 4Department of Aeronautics and Astronautics, Professor, Tokai University, Kanagawa, Japan
[b-11] Pulsed Plasma Thruster
Session Date June 9 (Fri) 11:00 – 12:20
Room Pearl Room B
Chairpersons Akira Kakami (University of Miyazaki, Japan)
Hideyuki Horisawa (Tokai University, Japan)
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, Beijing, China
2017-b-47 ( 11:40 – 12:00 )
Plasma Characterization of a Short-pulse Laser-assisted Pulsed Plasma Thruster
Kentaro Kato1, Toshiyuki Oi1, Hideyuki Horisawa2
1Department of Mechanical Engineering Graduate school of Engineering, Tokai University, Japan, 2Department of Aeronautics and Astronautics, Professor Tokai University, Japan
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 Takada3, Takashi Wakizono4
1Department of Mechanical Engineering, Osaka Institute of Technology, Osaka, Japan, 2Faculty of Electrical Engineering and Information Technology, University of the Federal Armed Forces Munich, Germany, 3Faculty of Intellectual Property, Osaka Institute of Technology, Osaka, Japan, 4Electric Propulsion R&D Section, High-Serve Inc., Tokyo, Japan
[b-12] Low Power Thruster 1
Session Date June 9 (Fri) 14:00 – 15:40
Room Pearl Room B
Chairpersons Yong Cao (Harbin Institute of Technology, China)
Yoshinori Takao (Yokohama National University, Japan)
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, Beijing, China, 2Beijing University of Aeronautics and Astronautics, Beiing, China
2017-b-50 ( 14:20 – 14:40 )
Effect of Anode Magnetic Shield on Performance and Life in Low Power Cylindrical Hall Thruster
Yongjie Ding1,2, Peng Li1, Yu Xu1, Liqiu Wei1,2
1Plasma Propulsion Lab, Institute of Advanced Power, Harbin Institute of Technology, Harbin, China, 2Electric Drive & Propulsion Technology Lab, Harbin Institute of Technology, Harbin, China
2017-b-51 ( 14:40 – 15:00 )
10 W Class Micro Hall Thruster with Anode Layer
Seunghun Lee1,2, Holak Kim1, Keuntae Doh1, Wonho Choe1
1Korea Advanced Institute of Science and Technology (KAIST), Republic of Korea, 2Korea Institute of Materials Science (KIMS), Republic of Korea
2017-b-52 ( 15:00 – 15:20 )
Research and Development of Low-Power Cylindrical Hall Thrusters and Magnetic-Field-Expansion Cathodes 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, Osaka, Japan, 2Department of Aeronautics and Astronautics, Tokai university, Kanagawa, Japan
[b-13] Laser & Microwave Thruster
Session Date June 9 (Fri) 14:00 – 15:40
Room Meeting Room 5
Chairpersons Makoto Matsui (Shizuoka University, Japan)
Hiroshi Katsurayama (Yamaguchi University, Japan)
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 Shimamura1, Naoto Ozaki1, Inoru Kiyono1, Kohei Matsui2, Shigeru Yokota1, Kimiya Komurasaki2
1Department of Engineering Mechanics and Energy, The University of Tsukuba, Tsukuba, Japan, 2Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan
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, Kanagawa, 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, Joseph A. Ofosu2, Kimiya Komurasaki1, Hiroyuki Koizumi2
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Department of Advanced Energy, The University of Tokyo, Tokyo, Japan
2017-b-57 ( 15:00 – 15:20 )
Laser-ablation Plasma Diagnostics by Single- and Triple-probes
Kaede Yano1, Haruhito Kato1, Yuki Nakamura2, Akihiro Osamura2, Ryo Edamura2, Hideyuki Horisawa3
1Dept. Graduate school of engineering, Tokai University, Japan, 2Graduate student, Dept. Aeronautics & Astronautics, Tokai University, Japan, 3Professor, Dept. Aeronautics & Astronautics, Tokai University, Japan
2017-b-58 ( 15:20 – 15:40 )
Feasibility of Laser Ablation Propulsion using Magnetic Fluid as a Propellant
Takuyuki Sakai, Shigeru Yokota, Kohei Shimamura
University of Tsukuba
[b-14] Low Power Thruster 2
Session Date June 9 (Fri) 16:00 – 17:20
Room Pearl Room B
Chairpersons Kazuhiro Toyoda (Kyushu Institute of Technology, Japan)
Hirokazu Tahara (Osaka Institute of Technology, Japan)
2017-b-62 ( 16:00 – 16:20 )
Numerical Investigation of Steady and Transient Ion Beam Extraction Mechanisms for Electrospray Thrusters
Kazuma Emoto1, Toshiyuki Tsuchiya2, Yoshinori Takao3
1Department of Systems Integration, Yokohama National University, Yokohama, Japan, 2Department of Micro Engineering, Kyoto University, Kyoto, Japan, 3Division of Systems Research, Yokohama National University, Yokohama, Japan
2017-b-63 ( 16:20 – 16:40 )
Evaluation of Ion Beam Characteristics for Ionic Liquid Electrospray Thrusters
Naoki Inoue1, Kaito Nakagawa1, Toshiyuki Tsuchiya2, Yoshinori Takao3
1Department of Systems Integration, Yokohama National University, Yokohama, Japan, 2Department of Micro Engineering, Graduate School of Engineering, Kyoto University, Kyoto, Japan, 3Department of Systems Research, Yokohama National University, Yokohama, Japan
2017-b-60 ( 16:40 – 17:00 )
Proposal of Unified Micro-Propulsion System using Water Propellant for CubeSats
Hiroyuki Koizumi1, Yoshinori Takao2, Masakatsu Nakano3, Ryu Funase4, Jun Asakawa4, Yuichi Nakagawa4, Daiki Tomita4, Kimiya Komurasaki4
1Department of Advanced Energy, The University of Tokyo, Tokyo, Japan, 2Tokyo Metropolitan College of Industrial Technology, Yokohama National University, Yokohama, Japan, 3Tokyo Metropolitan College of Industrial Technology, Tokyo, Japan, 4Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan
2017-b-61 ( 17:00 – 17:20 )
Design and Test of a 100 μN-class Thrust Stand for a Miniature Water Ion Thruster with CubeSat
Yuichi Nakagawa1, Daiki Tomita1, Hiroyuki Koizumi2, Kimiya Komurasaki1
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Department of Advanced Energy, The University of Tokyo, Tokyo, Japan
[c-1] Reentry TPS 1
Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 5
Chairpersons Shin-ichi Takeda (JAXA, Japan)
Saori Nagi (IHI Aerospace Co., Ltd., Japan)
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, Stuttgart, Germany, 2Fluid Gravity Engineering Ltd., Emsworth, United Kingdom, 3Belstead Research Ltd., Ashford, United Kingdom, 4Aerospace and Advanced Composites GmbH, Wiener Neustadt, Austria, 5European Space Agency, European Space Research and Technology Centre (ESA-ESTEC), Noordwijk, The Netherlands
2017-c-02 ( 9:20 – 9:40 )
In-Situ Measurement of Thermal Deformation of CFRP Ablator at Arc-Heated Wind Tunnel Using Digital Image Correlation
Kan Sawai1, Yasuhiro Fukuda2, Jun Koyanagi2, Yuelin Zhang1, Satoru Yoneyama1, Kenichi Hirai3
1Department of Mechanical Engineering, Aoyama Gakuin University, Sagamihara, Japan, 2Department of Aeronautics and Astronautics, Tokyo University of Science, Tokyo, Japan, 3IHI AEROSPACE Co., Ltd., Tomioka, Japan
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
1Tokyo University of Science, Japan, 2JAXA, Japan, 3IHI Aerospace, Japan
2017-c-04 ( 10:00 – 10:20 )
Spall Fracture Mechanisms and Strength Evaluation of CFRP against High-speed Impact
Daisuke Yoshimizu
Nagoya University, Japan
2017-c-05 ( 10:20 – 10:40 )
Dust Erosion of the Thermal Protection System for Martian Atmospheric Entry
Takahiro Yamanaka, Jun Koyanagi
Tokyo University of Science, Japan
[c-2] Reentry TPS 2
Session Date June 6 (Tue) 11:00 – 12:00
Room Meeting Room 5
Chairpersons Jun Koyanagi (Tokyo University of Science, Japan)
Ken-ichi Hirai (IHI Aerospace Co., Ltd., Japan)
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, Stuttgart, Germany, 2Institute of Structures and Design, German Aerospace Centre (DLR), Stuttgart, Germany
2017-c-07 ( 11:20 – 11:40 )
Development of Mid Density Carbon Phenolic Ablators for Future Re-entry Capsules
Kenichi Hirai1, Akiko Nakazato1, Jun Koyanagi2, Kazuhiko Yamada3
1IHI Aerospace Co., Ltd., Tomioka, Gunma, Japan, 2Tokyo University of Science, Tokyo, Japan, 3Institute of Space and Astronautical Science, JAXA, Sagamihara, Kanagawa, Japan
2017-c-09 ( 11:40 – 12:00 )
Ablative Performance of High Density Carbon Phenolic after Cold Soak Exposure
Kenichi Hirai1, Akiko Nakazato1, Hayato Yano1, Kenichi Kawazoe1, Jun Koyanagi2, Kazuhiko Yamada3
1IHI Aerospace Co., Ltd., Tomioka, Gunma, Japan, 2Tokyo University of Science, Tokyo, Japan, 3Institute of Space and Astronautical Science, JAXA, Sagamihara, Kanagawa, Japan
[c-3] Measurement and Simulation
Session Date June 6 (Tue) 14:00 – 15:20
Room Meeting Room 5
Chairpersons Yong Chan Cho (Korea Research Institute of Standards and Science, Korea)
Jun Koyanagi (Tokyo University of Science, Japan)
2017-c-10 ( 14:00 – 14:20 )
Structural Health Monitoring using Tilted FBG type Optical Fiber Sensors
Naoto Nakamura1, Shin-Ich Takada2, Toshio Ogasawara1
1Department of Mechanical Systems engineering, Tokyo University of Agriculture and Technology, Tokyo, Japan, 2Aeronautical Technology Directorate, JAXA, Tokyo, Japan
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, Tokyo, Japan, 2Department of Mechanical, systems engineering, Tokyo University of Agriculture and Technology, Tokyo, Japan
2017-c-13 ( 14:40 – 15:00 )
Molding and Evaluation of a Polymer Monolith with a Bicontinuous Structure via the Self-Consistent Field Method
Mayuko Takahashi, Ryosuke Matsuzaki, Jun Koyanagi
Tokyo University of Science , Chiba, Japan
2017-c-14 ( 15:00 – 15:20 )
Dispersion Simulation of Multifunctional PANI/carbon Nanomaterials
Michihiro Yamamoto1, Tomohiro Yokozeki2, Xiuyan Cheng2, Jun Koyanagi3
1Department of Materials Science and Technology, Graduate School of Industrial Science and Technology, Japan, 2Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 3Department of Materials Science and Technology, Tokyo University of Science, Tokyo, Japan
[c-4] Material Characterizations
Session Date June 6 (Tue) 16:00 – 17:20
Room Meeting Room 5
Chairpersons Adam S. Pagan (University of Stuttgart, Germany)
Takashi Iwasa (Tottori University, Japan)
2017-c-15 ( 16:00 – 16:20 )
Structural Study of Extremely Supersaturated KDP and ADP Solution Droplets using Electrostatic Levitation
Yong Chan Cho1, Wonhyuk Jo1,2, Sooheyong Lee1,2, Geun Woo Lee1,2
1Frontier in Extreme Physics, Korea Research Institute of Standards and Science, Republic of Korea, 2Department of Nano Science University of Science and Technology, Republic of Korea
2017-c-16 ( 16:20 – 16:40 )
Analysis of Material Characteristics of Magnetic Elastomer for Fluid Force Control
Ryohei Aoki1, Nobuyoshi Fujimatsu2
1Graduate School of Engineering, Toyo University, Kawagoe, Japan, 2Depertment of Mechanical of Engineering, Toyo University, Kawagoe, 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
Gordan Thiede1, Jörg Riccius1, Stefanie Reese2
1Institute of Space Propulsion, DLR, Lampoldshausen, Germany, 2Institute of Applied Mechanics, RWTH Aachen University, Aachen, Germany
2017-c-18 ( 17:00 – 17:20 )
Charging Characteristics of Spacecraft Dielectric Material at Cryogenic Temperature
Yuki Shibuya, Rikio Watanabe, Akihiro Miyasaka
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 Kosei Ishimura (Japan Aerospace Exploration Agency, Japan)
Yasutaka Satou (JAXA, Japan)
2017-c-19 ( 9:00 – 9:20 )
An Electromagnetically Actuated, Self-Reconfigurable Space Structure
Martin Nisser, Dario Izzo, Andreas Borggraefe
Advanced Concepts Team, European Space Agency, Noordwijk, The Netherlands
2017-c-20 ( 9:20 – 9:40 )
Weightless Construction of High Tower to the Stratosphere
Ryojiro Akiba1, Ken Higuchi2, Ryuichi Mitsuhashi3, Riho Hiramoto3, Jun’Ya Sasaki1
1Hokkaido Aerospace Science and Technology Incubation Center, Sapporo, Japan, 2Muroran Institute of Technology, Muroran, Japan, 3Hokkaido University of Science, Sapporo, Japan
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
1Mechanical Systems Engineering, Tokyo City University, Tokyo, Japan, 2Institute of Industrial Science, The University of Tokyo, Tokyo, Japan
2017-c-23 ( 10:20 – 10:40 )
Structural Characteristics of BCON Truss
Momoko Fukunaga, Yasuyuki Miyazaki
Department of Aerospace Engineering, Nihon University, Chiba, Japan
[c-6] Satellite Structures and Subsystems
Session Date June 7 (Wed) 11:00 – 12:20
Room Meeting Room 5
Chairpersons Nobukatsu Okuizumi (Japan Aerospace Exploration Agency, Japan)
Yohsuke Nambu (Osaka Prefecture University, Japan)
2017-c-26 ( 11:20 – 11:40 )
Study on Competitive Structure Design of Nano Satellite
Bui Nam Duong1, Truong Xuan Hung1, Nguyen Duc Manh1, Kei-Ichi Okuyama2
1Vietnam National Satellite Center, Vietnam Academy of Science and Technology, Hanoi, Vietnam, 2Graduate School of Engineering, Department of Applied Science for Integrated System Engineering, Kyushu Institute of Technology, Kitakyushu, Japan
2017-c-27 ( 11:40 – 12:00 )
Development of CALET CALorimeter/Sensor Structure
Takahito Amanuma1, Daisuke Nakayama1, Akira Kito1, Osamu Maeda1, Yukihiro Ueda2, Kazuhiro Fujimoto2, Koki Oikawa3, Tetsuya Honda3, Norio Sugi3, Shoji Torii4, Shunsuke Ozawa4, Tadahisa Tamura5, Yuki Shimizu5
1Nippi Corporation, Japan, 2IHI AeroSpace, Japan, 3JAXA, Japan, 4Waseda University, Japan, 5Kanagawa University, Japan
2017-c-28 ( 12:00 – 12:20 )
Actuator Development Projects in the Space Exploration Innovation Hub Center
Tomoaki Yano, Masatsugu Otsuki
Space Exploration Innovation Hub Center, JAXA, Sagamihara, Japan
[c-7] High Precise Deployable Space Structures
Session Date June 7 (Wed) 16:00 – 17:40
Room Meeting Room 5
Chairpersons Hiroaki Tanaka (National Defense Academy of Japan, Japan)
Rikio Watanabe (Tokyo City University, Japan)
2017-c-29 ( 16:00 – 16:20 )
An Imporovement of NIPPI HIMAT
Kazuhiro Abe, Manato Makita, Takahiro Yumoto, Osamu Maeda
NIPPI Corporation , Yokohama, 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
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2NIPPI, Kanagawa, Japan
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, JAXA, Sagamihara, Japan, 2NEC Corporation, Fuchu, Tokyo, Japan, 3Nippi Corporation, Yokohama, Kanagawa, Japan
2017-c-33 ( 17:20 – 17:40 )
A Numerical Study on Shape Repeatability of Pin Jointed Beam with Frictional Contact Conditions
Takeshi Akita1, Keisuke Nakajima1, Hiroaki Tanaka2
1Chiba Institute of Technology, Narashino, Japan, 2National Defense Academy, Yokosuka, Japan
[c-8] High Precise Space Antenna and Subsystems
Session Date June 8 (Thu) 9:00 – 10:40
Room Meeting Room 5
Chairpersons Atsuhiko Senba (Meijo University, Japan)
Takashi Iwasa (Tottori University, Japan)
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, Yokosuka, 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
1The University of Tokyo, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 3JAXA, Sagamihara, Japan
2017-c-36 ( 9:40 – 10:00 )
Suppression of Out-of-plane Thermal Deformation of CFRP Reflectors by Linear Actuators
Shun Tanaka1, Tadashige Ikeda2
1Department of Aerospace Engineering, Nagoya University, Nagoya, Japan, 2Department of Mechanical Engineering, Chubu University, Kasugai, Japan
2017-c-37 ( 10:00 – 10:20 )
Preliminary Design Study on Tension Truss Antenna Surface for Shape Stability
Noriyasu Yasui, Yuichiro Takano, 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, Noriyasu Yasui, Rikio Watanabe, Akihiro Miyasaka
Tokyo City University, Japan
[c-9] Membrane Structures I
Session Date June 8 (Thu) 11:00 – 12:20
Room Meeting Room 5
Chairpersons Takeshi Akita (Chiba Institute of Technology, Japan)
Kanjuro Makihara (Tohoku University, Japan)
2017-c-40 ( 11:00 – 11:20 )
Winkling of a Membrane with a Curved Small Thin Film
Masanori Matsushita1, Osamu Mori2, Nobukatsu Okuizumi2, Yasutaka Satou2, Takashi Iwasa3, Saburo Matunaga4
1Department of Mechanical and Aerospace Engineering, Tokyo Institute of Technology, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 3Department of Mechanical and Aerospace Engineering, Tottori University, Tottori, Japan, 4Department of Mechanical Engineering, School of Engineering, Tokyo Institute of Technology, Tokyo, Japan
2017-c-42 ( 11:40 – 12:00 )
Data Driven Model Reduction for Spin-type Membrane Space Structure
Masahiko Yamazaki
Department of Aerospace Engineering, Nihon University, Chiba, Japan
2017-c-43 ( 12:00 – 12:20 )
Estimation Method of Missing Components for Spin Deployable Membrane Dynamics
Shoji Kawazoe, Masahiko Yamazaki, Yasuyuki Miyazaki
Department of Aerospace Engineering , Nihon University, Chiba, Japan
[c-10] Membrane Structures II
Session Date June 8 (Thu) 14:00 – 15:00
Room Meeting Room 5
Chairpersons Kyoichi Nakashino (Tokai University, Japan)
Masahiko Yamazaki (Nihon University, Japan)
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, JAXA, Sagamihara, Japan
2017-c-46 ( 14:20 – 14:40 )
Deployment Properties of Boom-Membrane Integrated Space Structures
Hiroshi Furuya1, Hiraku Sakamoto2, Akihito Watanabe3
1Tokyo Institute of Technology, Yokohama, Japan, 2Tokyo Institute of Technology, Tokyo, Japan, 3Sakase Adtech Co. Ltd, Fukui, Japan
2017-c-47 ( 14:40 – 15:00 )
Similarity Rule of Deployment Behavior for Spin Deployment Membrane
Tomohiro Suzuki, Yasuyuki Miyazaki, Masahiko Yamazaki
Department of Aerospace Engineering, Nihon University, Chiba Japan
[c-11] Vibration and Control
Session Date June 8 (Thu) 16:00 – 17:40
Room Meeting Room 5
Chairpersons Yasuyuki Miyazaki (Nihon University, Japan)
Naoko Kishimoto (Setsunan University, Japan)
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, Chosun University, Gwangju, 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 Takayuki Shimoda (Japan Aerospace Exploration Agency, Japan)
Takashi Iwasa (Tottori University, Japan)
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, JAXA, Sagamihara, Japan
2017-c-55 ( 9:20 – 9:40 )
Analytical Study of Landing Shock Absorber in the High-Speed Impact Test
Keisuke Nakamura1, Tetsuya Yamada2, Hideyuki Tanno3, Koichi Kitazono4
1Waseda University Dept.Applied mechanics , Shinjuku, Japan, 2Division for Space Flight Engineering, ISAS/JAXA, Sagamihara, Japan, 3JAXA Kakuda Space Center, Kakuda, Japan, 4Tokyo Metropolitan University, Hachioji, 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
1Department of Mechanical Engineering, Chubu University, Kasugai, Japan, 2Department of Aerospace Engineering, National Defense Academy of Japan, Yokosuka, Japan, 3Department of Mechanical System Engineering, Kumamoto University, Kumamoto, Japan, 4Department of Aerospace Engineering, Osaka Prefecture University, Sakai, Japan, 5Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 6Department of Mechanical and Aerospace Engineering, Tottori University, Tottori, Japan
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
1School of Defense Science, Chung Cheng Institute of Technology, National Defense University, Taoyuan, Taiwan, 2Dept. of Power Vehicle and Systems Engineering, Chung Cheng Institute of Technology, National Defense University, Taoyuan, Taiwan
[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 Hiraku Sakamoto (Tokyo Institute of Technology, Japan)
Tadashige Ikeda (Chubu University, Japan)
2017-c-58 ( 11:00 – 11:20 )
High-Fidelity Verification of Vision-Based Sensors for Inertial and Far-Range Spaceborne Navigation
Connor Beierle, Joshua Sullivan, Simone D’Amico
Department of Aeronautics and Astronautics, Stanford University, Stanford, California, 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, Neyagawa, Japan, 2Tottori University, Tottori, Japan, 3Muroran Institute of Technology, Muroran, Japan
2017-c-60 ( 11:40 – 12:00 )
Preliminary Investigations of Pneumatic Gravity Compensation System for Deployable Space Structures
Masato Taki, Rikio Watanabe, Akihiro Miyasaka
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 Astronautical Science, JAXA, Sagamihara, Japan, 2Department of Applied Science for Integrated System Engineering, Kyushu Institute of Technology, Kitakyushu, Japan
2017-c-62 ( 12:20 – 12:40 )
Three-dimensional Surface Shape Measurement of Parabola Antenna Model with 1.5m diameter using Grating Projection Method
Kento Ota1, Taku Harada2, Takashi Iwasa3
1Graduate Student, Tottori University, Tottori, Japan, 2Former Graduate student, Tottori University, Tottori, Japan, 3Department of Mechanical and Aerospace Engineering, Tottori University, Tottori, Japan
[d-1] Flight Dynamics Operations 1
Session Date June 6 (Tue) 9:00 – 10:20
Room Meeting Room 1
Chairpersons Lutz Massonne (Telespazio VEGA Deutschland GmbH at ESOC Flight Dynamics, Germany)
Petr Kuchynka (GMV/ESOC, Germany)
ISTS-2017-d-001/ISSFD-2017-001 ( 9:00 – 9:20 )
Feasibility of Metop-A Mission Extension on Drifting Local Time
Pier Luigi Righetti, Richard Dyer
EUMETSAT, Darmstadt, Germany
ISTS-2017-d-003/ISSFD-2017-003 ( 9:20 – 9:40 )
Flight Dynamics Support to extend Metop Instruments Useful Lifetime
Antimo Damiano1, Pier Luigi Righetti2, RüDiger Lang2, Francisco Sancho3
1RHEA Group at EUMETSAT, 2EUMETSAT, 3WGS at EUMETSAT
ISTS-2017-d-004/ISSFD-2017-004 ( 9:40 – 10:00 )
Non-nominal Attitude Manoeuvres during Metop-A Extended Lifetime
Francisco Sancho1, Jörg Fischer2, Stefania Tarquini3
1WGS Workgroup Solutions at EUMETSAT, Darmstadt, Germany, 2Jade Aerospace at EUMETSAT, Darmstadt, Germany, 3EUMETSAT, Darmstadt, Germany
ISTS-2017-d-002/ISSFD-2017-002 ( 10:00 – 10:20 )
Metop Long Term Free-dynamics Attitude Analysis, for Improved Re-entry Prediction
Stefano Pessina1, Pierluigi Righetti1, João Branco2, Victor Manuel Moreno Villa3, Thomas Vincent Peters3
1EUMETSAT, Darmstadt, Germany, 2GMV, Lisbon, Portugal, 3GMV, Madrid, Spain
[d-2] Orbit Dynamics (Martian Moon)
Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 2
Chairpersons Osamu Mori (Japan Aerospace Exploration Agency, Japan)
Laurence Lorda (CNES, France)
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
1German Space Operations Center, DLR, Oberpfaffenhofen, Germany, 2Institute of Planetary Research, DLR, Berlin, Germany
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, Julien Laurent-Varin1,2, Jean Charles Marty1,2, Yuya Mimasu3
1CNES, French Space Agency, Toulouse, France., 2GRGS Spatial Geodesy Research Group, Toulouse, France., 3Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan.
ISTS-2017-d-007/ISSFD-2017-007 ( 9:40 – 10:00 )
The Dynamical Environment for The Exploration of Phobos
Daniel Scheeres, Stefaan VAN Wal, Zubin Olikara, Nicola Baresi
Smead Department of Aerospace Engineering Sciences, The University of Colorado, Boulder, Colorado, USA
ISTS-2017-d-008/ISSFD-2017-008 ( 10:00 – 10:20 )
Orbital Operations Strategy in the Vicinity of Phobos
Hitoshi Ikeda1, Shinji Mitani1, Yuya Mimasu2, Go Ono1, Kenichiro Nigo1, Yasuhiro Kawakatsu2
1Research and Development Directorate, JAXA, Tsukuba, Ibaraki, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Kanagawa, Japan
ISTS-2017-d-009/ISSFD-2017-009 ( 10:20 – 10:40 )
Quasi-Satellite Orbits around Phobos for the Sample Return Mission
Javier Martín, Simone Centuori
Deimos Space SLU, Spain
[d-3] Trajectory Design & Optimization 1
Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 3
Chairpersons Satoshi Ueda (JAXA, Japan)
Lorenzo Casalino (Politecnico di Torino, Italy)
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
Jet Propulsion Laboratory / California Institute of Technology, Pasadena, CA
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, Changsha, 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, Japan
ISTS-2017-d-013/ISSFD-2017-013 ( 10:00 – 10:20 )
Descent Isochrones in Martian Atmosphere
Miljan Kolcic, Dusan Marceta
Department of Astronomy, Faculty of Mathematics, University of Belgrade, Serbia
ISTS-2017-d-014/ISSFD-2017-014 ( 10:20 – 10:40 )
General Characteristics of Robust Orbit Insertion and Trajectory Design with MOI Robustness in MMX Mission
Shota Takahashi1, Naoko Ogawa2, Yasuhiro Kawakatsu2
1Department of Mechanical Engineering, Keio University, Japan, 2Institute of Space and Astronautical Science, JAXA, Japan
[d-5] Orbit Dynamics (Small Body) 1
Session Date June 6 (Tue) 11:00 – 12:40
Room Meeting Room 2
Chairpersons Hitoshi Ikeda (Japan Aerospace Exploration Agency, Japan)
Daniel J. Scheeres (University of Colorado, USA)
ISTS-2017-d-017/ISSFD-2017-017 ( 11:00 – 11:20 )
Assessing the Hazard Posed by Ryugu Ejecta Dynamics on Hayabusa2 Spacecraft
Stefania Soldini, Yuichi Tsuda
Institute of Space and Astronautical Science/JAXA, Sagamihara, Japan
ISTS-2017-d-018/ISSFD-2017-018 ( 11:20 – 11:40 )
Investigation of 1:1 Resonance in a Rotating 4th Degree and Order Gravitational Field
Jinglang Feng1, Ron Noomen2, Xiyun Hou1, Pieter Visser2, Jianping Yuan3, Jingshi Tang1, Lin Liu1
1Nanjing University, China, 2Delft University of Technology, the Netherlands, 3Northwestern Polytechnic University, China.
ISTS-2017-d-019/ISSFD-2017-019 ( 11:40 – 12:00 )
Orbital Stability Regions for Hypothetical Natural Satellites
Samantha Rieger, Daniel Scheeres
Ann and H.J. Smead Department of Aerospace Engineering Sciences, University of Colorado Boulder, Boulder, Colorado, 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 J. Scheeres2, Xiaosheng Xin1, Jinglang Feng1, Jingshi Tang1, Lin Liu1
1School of Astronomy and Space Science, Nanjing University, Nanjing, China, 2Department of Aerospace Engineering Sciences, The University of Colorado at Boulder, Boulder, USA
ISTS-2017-d-021/ISSFD-2017-021 ( 12:20 – 12:40 )
On the Equilibrium Points of Doubly Synchronous Binary Asteroid Systems
Xiaosheng Xin1,2, Xiyun Hou2,3, Lin Liu2,3, Guangliang Dong1
1Beijing Institute of Tracking and Telecommunication Technology, Beijing, China, 2School of Astronomy and Space Science, Nanjing University, Nanjing, China, 3Institute of Space Environment and Astrodynamics, Nanjing University, Nanjing, China
[d-6] Trajectory Design & Optimization 2
Session Date June 6 (Tue) 11:00 – 12:40
Room Meeting Room 3
Chairpersons Naoko Ogawa (Japan Aerospace Exploration Agency, Japan)
Mar Vaquero (NASA Jet Propulsion Laboratory, USA)
ISTS-2017-d-023/ISSFD-2017-023 ( 11:20 – 11:40 )
Design of High-Energy Escape Trajectories with Lunar Gravity Assist
Lorenzo Casalino, Lucio Filizola
Politecnico di Torino, Torino, Italy
ISTS-2017-d-024/ISSFD-2017-024 ( 11:40 – 12:00 )
Matching of Patched-Hyperbolasfor Gravity-Assist Trajectory Design
Yuki Kayama1, Chit Hong Yam2, Kenta Oshima3, Shuntaro Suda4, Yasuhiro Kawakatsu5
1TheUniversity of Tokyo, Japan, 2ispace, Japan, 3Waseda University, Japan, 4Hokkaido University, Japan, 5JAXA, Japan
ISTS-2017-d-179/ISSFD-2017-179 ( 12:00 – 12:20 )
Patented Orbits Transfers and Manoeuvres Review
Christophe R Koppel
KopooS Consulting Ind., Paris, France
[d-7] Flight Dynamics Operations 2
Session Date June 6 (Tue) 14:00 – 15:20
Room Meeting Room 1
Chairpersons Takanori Iwata (JAXA, Japan)
Stefano Pessina (EUMETSAT, Germany)
ISTS-2017-d-026/ISSFD-2017-026 ( 14:00 – 14:20 )
Lessons Learned from Initial Sentinel-3A Maneuver Operations
Daniel Aguilar Taboada1, Pier Luigi Righetti2, Rami Houdroge3
1CLC Space at EUMETSAT, Germany, 2EUMETSAT, Germany, 3Serco at 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
1LSE at European Space Operations Center, ESA, Darmstadt, Germany, 2CS at European Space Operations Center, ESA, Darmstadt, Germany, 3CGI at European Space Operations Center, ESA, Darmstadt, 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,a, Miguel Angel Martin Serrano1,b, Mikel Catania1,c, Xavier Marc1,d, Dirk Kuijper1,e, Vitali Braun2,a, Holger Krag2,b
1Flight Dynamics Division, European Space Operations Center, ESA (GMV INSYEN a), SCISYS b), LSE c), ESA d), CGI e)), Darmstadt, Germany, 2Space Debris Office, European Space Operations Center, ESA (ESA a), IMS b)), Darmstadt, Germany
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
André Vasconcelos1, Miguel A. Martín Serrano1, Javier Sánchez2, Xavier Marc3, Dirk Kuijper4
1Scisys GmbH at ESA/ESOC, Darmstadt, Germany, 2GMV at ESA/ESOC, Darmstadt, Germany, 3European Satellite Operations Centre (ESOC), ESA, Darmstadt, Germany, 4CGI at ESA/ESOC, Darmstadt, Germany
[d-8] Orbit Dynamics (Small Body) 2
Session Date June 6 (Tue) 14:00 – 15:40
Room Meeting Room 2
Chairpersons Yasuhiro Kawakatsu (JAXA, Japan)
Elisabet Canalias (CNES, France)
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, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
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 Sánchez3
1Department of Space and Astronautical Science, The Graduate University for Advanced Studies (SOKENDAI), Sagamihara, Japan, 2Reference Systems and Planetology, the Royal Observatory of Belgium (ROB), Brussels, Belgium, 3Space Research Centre, School of Aerospace, Transport & Manufacturing, Cranfield University, Cranfield, United Kingdom
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, Romain Garmier2, Jens Biele3
1CNES, Toulouse, France, 2CS Système d’Informations, Toulouse, France, 3DLR, Cologne, Germany
ISTS-2017-d-033/ISSFD-2017-033 ( 15:00 – 15:20 )
Small-Body Lander Simulations Using the GPU
Stefaan Van Wal1, Robert Reid2, Daniel Scheeres1
1Colorado Center for Astrodynamics Research, University of Colorado Boulder, Boulder, Colorado, USA, 2Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California, USA
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, Jun’Ichiro Kawaguchi2
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
[d-9] Flight Dynamics Operations 3
Session Date June 6 (Tue) 16:00 – 17:40
Room Meeting Room 1
Chairpersons Takaya Inamori (Nagoya University, Japan)
Pierluigi Righetti (EUMETSAT, Germany)
ISTS-2017-d-035/ISSFD-2017-035 ( 16:00 – 16:20 )
Recent Developments and Future Directions in CCSDS Flight Dynamics Standards
David S. Berry
California Institute of Technology, Jet Propulsion Laboratory, Pasadena, California, 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-Bosch2, Xavier Pena3
1SCISYS Deutschland GmbH @ESA/ESOC, Darmstadt, Germany, 2ESA/ESOC, Darmstadt, Germany, 3CNES, Toulouse, France
ISTS-2017-d-037/ISSFD-2017-037 ( 16:40 – 17:00 )
Manoeuvre Optimization in the Galileo L7 Orbit Acquisition
André Vasconcelos1, Pere Ramos Bosch2, Dave Hocken1, Javier Sánchez3, Gerald Ziegler1
1Scisys GmbH at ESA/ESOC, Darmstadt, Germany, 2European Satellite Operations Centre (ESOC), ESA, Darmstadt, Germany, 3GMV at ESA/ESOC, Darmstadt, Germany
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 Prieur1,2, Thomas Lienart1,3, Manuel Rodrigues4, Pierre Touboul5, Troelz Denver6, John L. Jørgensen6, Anastassia M. Bang6, Gilles Metris7
1Centre National d’Etudes Spatiales, 18 av Edouard Belin F31400 Toulouse, France, 2Department of Flight Dynamics, 3Department of Propulsion, 4ONERA, Département ‘Physique, Instrumentation, Environnement, Espace’, Chatillon, France, 5ONERA, Microscope space mission Prime Investigator, Palaiseau, France, 6Technical University of Denmark, Lyngby, Denmark, 7Université de la Cote d’Azur, Observatoire de la Côte d’Azur, CNRS, Géoazur, Valbonne, France
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
Telespazio VEGA Deutschland GmbH at ESA/ESOC, Darmstadt, Germany
[d-10] Guidance, Navigation and Control (Small Body)
Session Date June 6 (Tue) 16:00 – 17:20
Room Meeting Room 2
Chairpersons Jay McMahon (University of Colorado Boulder, USA)
Sofya Spiridonova (German Space Operations Center, Germany)
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
Francesco Torre, Massimiliano Vasile, Romain Serra, Stuart Grey
Department of Mechanical and Aerospace Engineering, University of Strathclyde, Glasgow, United Kingdom
ISTS-2017-d-042/ISSFD-2017-042 ( 16:20 – 16:40 )
Improved Shape Determination for Autonomous State Estimation
Benjamin Bercovici, Jay Mcmahon
Department of Aerospace Engineering Sciences, University of Colorado at Boulder
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 L. Cano, Simone Centuori
Deimos Space S.L.U., Madrid, 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 Ishida1, Yuichi Tsuda2
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
[d-11] Attitude Dynamics
Session Date June 7 (Wed) 9:00 – 10:20
Room Meeting Room 1
Chairpersons Yu Nakajima (Japan Aerospace Exploration Agency, Japan)
Hirohisa Kojima (Tokyo Metropolitan University, Japan)
ISTS-2017-d-046/ISSFD-2017-046 ( 9:00 – 9:20 )
Dynamical Modeling for Flat-Spin Recovery Applications
Frank Janssens1, Jozef Van Der Ha2
1Consultant, Noordwijk, the Netherlands, 2Satellite Mission Design & Operations, Deming, WA, 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, Melbourne, Australia, 2Department of Aerospace Engineering, Tokyo Metropolitan University, Hino, 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, Beijing, 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, Hino, Japan
[d-12] Guidance, Navigation and Control (Landing) 1
Session Date June 7 (Wed) 9:00 – 10:20
Room Meeting Room 2
Chairpersons Satoshi Ikari (The University of Tokyo, Japan)
Alexey Yu Kutomanov (TSNIImash, Russia)
ISTS-2017-d-050/ISSFD-2017-050 ( 9:00 – 9:20 )
OMOTENASHI Trajectory Analysis and Design: Landing Phase
Javier Hernando-Ayuso1, Stefano Campagnola2, Toshinori Ikenaga3, Tomohiro Yamaguchi3, Yusuke Ozawa1, Bruno V. Sarli4, Shota Takahashi5, Chit Hong Yam6
1The University of Tokyo, Japan, 2JPL, USA, 3JAXA, Japan, 4Catholic University of America, USA, 5Keio University, Japan, 6ispace technologies, Japan
ISTS-2017-d-052/ISSFD-2017-052 ( 9:20 – 9:40 )
Fight Control of Flying Test Bed for Future Planetary Landing
Takehiro Higuchi1, Toshiki Tamura1, Seiya Ueno1, Kazuhisa Fujita2, Takashi Ozawa2, Hiroki Takayanagi2
1Yokohama National University, Yokohama, Japan, 2Chofu Aerospace Center, JAXA, Tokyo, Japan
ISTS-2017-d-053/ISSFD-2017-053 ( 9:40 – 10:00 )
A Study on Guidance Technique for Precise Lunar Landing
Satoshi Ueda, Takahiro Ito, Shin-ichiro Sakai
Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
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 Guo1, Linli Guo2, 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 Stefania Soldini (JAXA, Japan)
Hodei Urrutxua (University of Southampton, UK)
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
1University of Colorado at Boulder, Boulder, CO, USA, 2Advanced Space, Boulder, CO, USA
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 J. Masdemont2, Gerard Gómez3, Stéphanie Lizy-Destrez1
1ISAE-Supaéro, Toulouse, France, 2IEEC & Departament de Matemàtiques, Universitat Politècnica de Catalunya, Barcelona, Spain, 3IEEC & Departament de Matemàtiques i Informàtica, Universitat de Barcelona, Barcelona, Spain
ISTS-2017-d-057/ISSFD-2017-057 ( 9:40 – 10:00 )
Assessment of the Gaussian Covariance Approximation Over an Earth-Asteroid Encounter Period
Daniel Mattern
Omitron, Inc., Beltsville, MD | NASA Goddard Space Flight Center, Flight Dynamics Facility, Greenbelt, MD
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 (DLR/GSOC), Wessling, 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 Models
Changyong He1,2, Yang Yang1,2, Brett Carter2, Han Cai1,2, Suqin Wu2, Kefei Zhang2
1Space Environment Research Centre (SERC) Limited, Australia, 2Satellite Positioning for Atmosphere, Climate and Environment (SPACE) Research Centre, School of Sciences, RMIT University, Australia
[d-14] Attitude / Orbit Dynamics & Control
Session Date June 7 (Wed) 11:00 – 12:40
Room Meeting Room 1
Chairpersons Yasuhiro Yoshimura (Tokyo Metropolitan University, Japan)
Jozef C. van der Ha (Mission Design & Operations, USA)
ISTS-2017-d-060/ISSFD-2017-060 ( 11:00 – 11:20 )
An Efficient Algorithm to Compute the SRP Force and Torque on Spacecraft
Juan Manuel García1,2
1European Space Operations Center, ESA, Darmstadt, Germany, 2Flight Dynamics and Operations, GMV-Insyen AG, Darmstadt, 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, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
ISTS-2017-d-062/ISSFD-2017-062 ( 11:40 – 12:00 )
Optical Property Estimation 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, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 3Department of Micro-Nano System Engineering , Nagoya University, Nagoya, Japan
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
Aerospace Science and Technology Department, Politecnico di Milano, Milan, 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, Kenshiro Oguri, Satoshi Ikari, Ryu Funase, Shinichi Nakasuka
Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan
[d-15] Guidance, Navigation and Control (Landing) 2
Session Date June 7 (Wed) 11:00 – 12:40
Room Meeting Room 2
Chairperson Takehiro Higuchi (Yokohama National University, Japan)
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 Sawai2,1, Seisuke Fukuda2,1
1Department of Space and Astronautical Science, SOKENDAI, Sagamihara, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
ISTS-2017-d-066/ISSFD-2017-066 ( 11:20 – 11:40 )
A Study of Terrain Feature Matching for Lunar Landing Navigation
Yasuhiro Katayama1, Shigehito Shimizu2, Misuzu Haruki2, Shuhei Shigeto2, Isao Kawano2, Kazuhisa Fujita1
1Research and Development Directorate, JAXA, Chofu, Tokyo, Japan, 2Research and Development Directorate, JAXA, Tsukuba, Ibaraki, Japan
ISTS-2017-d-067/ISSFD-2017-067 ( 11:40 – 12:00 )
The Robust Spacecraft Locaiton Estimation Algorithm toward the Misdetection Crater and the Undetected Crater in SLIM
Haruyuki Ishii1, Keiki Takadama1, Akinori Murata1, Fumito Uwano1, Takato Tatsumi1, Yuta Umenai1, Kazuma Matsumoto1, Hiroyuki Kamata2, Takayuki Ishida3, Seisuke Fukuda4, Shujiro Sakai4, Shinichiro Sawai4
1Department of Information, The University of Electro-Communication, Tokyo, Japan, 2Department of Electrical engineering, Meiji University, Tokyo, Japan, 3Institute of Space and Astronautical Science, JAXA & ISAS, Sagamihara, Japan, 4Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
ISTS-2017-d-068/ISSFD-2017-068 ( 12:00 – 12:20 )
Autonomous Navigation for Pinpoint Lunar Soft Landing
Chengchao Bai1, Jifeng Guo1, Linli Guo2, 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 Morikawa1, Hikaru Eguchi2, Yusuke Maru2,3, Taro Kawano3, Masahiro Nohmi1, Shujro Sawai2,3
1Department of Engineering, Shizuoka University, Shizuoka, Japan, 2Department of Space and Astronautical Science, The Graduate University for Advanced Studies(SOKENDAI), Sagamihara, Japan, 3Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
[d-16] Orbit Dynamics & Control 2
Session Date June 7 (Wed) 11:00 – 12:00
Room Meeting Room 3
Chairpersons Toshinori Ikenaga (Japan Aerospace Exploration Agency, Japan)
Yue Wang (Beihang University, China)
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, Tokyo, Japan, 2Space Dynamics Groups, Technical University of Madrid, Spain
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 Örger1, 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, Singapore
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, United Kingdom, 2Space Dynamics Group, Technical University of Madrid, Spain
[d-17] Attitude Determination
Session Date June 7 (Wed) 16:00 – 17:40
Room Meeting Room 1
Chairpersons Takanori Iwata (JAXA, Japan)
Juan Manuel Garcia (GMV GmbH, ESOC, Germany)
ISTS-2017-d-075/ISSFD-2017-075 ( 16:00 – 16:20 )
Study on an Advanced Attitude Determination Algorithm for the ERG Spacecraft
Halil Ersin Söken, Shin-Ichiro Sakai, Kazushi Asamura, Yosuke Nakamura, Takeshi Takashima
Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
ISTS-2017-d-076/ISSFD-2017-076 ( 16:20 – 16:40 )
Labelling Technique for the Fast Star Identification
Sangkyun Kim, Mengu Cho
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
1Department of Aeronautics and Astronautics, Istanbul Technical University, Istanbul, Turkey, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
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 Söken1, Jozef C. Van Der Ha2, Shin-Ichiro Sakai2
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2Satellite Mission Design and Operations, Deming, WA, USA
ISTS-2017-d-079/ISSFD-2017-079 ( 17:20 – 17:40 )
Regularized Particle Filter with Roughening for Gyros Bias and Attitude Estimation using Simulated Measurements
William Silva1, Roberta Garcia2, Hélio Kuga1, Maria Zanardi3
1Technological Institute of Aeronautics, ITA, São José dos Campos, Brazil, 2São Paulo University, USP, Lorena, Brazil, 3Federal University of ABC, UFABC, Santo André, Brazil
[d-18] Guidance, Navigation and Control (Ascent/Descent/Deorbit)
Session Date June 7 (Wed) 16:00 – 17:40
Room Meeting Room 2
Chairpersons Shinji Hokamoto (Kyushu University, Japan)
Massimiliano L Vasile (University of Strathclyde, UK)
ISTS-2017-d-080/ISSFD-2017-080 ( 16:00 – 16:20 )
Method of Safe Descent in Case of Off-nominal Onboard Situation on Russian Perspective manned Spacecraft “Federation”
Alexey Yu. Kutomanov, Maxim M. Matushin, Vladimir N. Pochukaev
TSNIImash, Mission Control Centre
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, Kent Shirakata, Hayato Tobiyama
Department of Mechanical and Control Engineering, Kyushu Institute of Technology, Fukuoka, Japan
ISTS-2017-d-082/ISSFD-2017-082 ( 16:40 – 17:00 )
Deorbit Maneuver Strategy for the Three Themis Probes
S. Frey1, V. Angelopoulos2, M. Bester1
1Space Sciences Laboratory, University of California, 7 Gauss Way, Berkeley, CA, 2ESS/IGPP, University of California, Los Angeles, 405 Hilgard Avenue, Los Angeles, CA
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, Yuzo Iwai2, Ryohei Uchino2
1Japan Aerospace Exploration Agency, Tsukuba, Japan, 2Sumitomo Precision Products Co., Ltd., Amagasaki, Japan
[d-19] Orbit Dynamics & Control 3
Session Date June 7 (Wed) 16:00 – 17:20
Room Meeting Room 3
Chairpersons Takanao Saiki (Japan Aerospace Exploration Agency, Japan)
Pavel M. Trivailo (RMIT University, Australia)
ISTS-2017-d-085/ISSFD-2017-085 ( 16:00 – 16:20 )
Study on Low-Thrust Stationkeeping on Geostationary Orbit
Toshinori Ikenaga1, Masayoshi Utashima1, Yu Nakajima1, Toru Yamamoto1, Tadahiko Sano2, Noriyasu Inaba1
1Research and Development Directorate, JAXA, Ibaraki, Japan, 2Space Technology Directorate I, JAXA, Ibaraki, Japan
ISTS-2017-d-086/ISSFD-2017-086 ( 16:20 – 16:40 )
Predictive Autonomous Orbit Control Method for Low Earth Orbit Satellites
Jérôme Thomassin1, Maxime Ecochard2, Guillaume Azema2
1Department of Flight Dynamics, CNES, Toulouse, France, 2Spaceflight Dynamics Department, Thales Services, Toulouse, France
ISTS-2017-d-087/ISSFD-2017-087 ( 16:40 – 17:00 )
De-orbiting Timing for Spacecraft in Geostationary Transfer Orbits Exploiting Luni-solar Perturbations
Yue Wang1, Pini Gurfil2
1School of Astronautics, Beihang University, Beijing, China, 2Faculty of Aerospace Engineering, Technion–Israel Institute of Technology, Haifa, Israel
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
GMV at ESA/ESOC, Darmstadt, Germany
[d-20] Formation Flying & Satellite Constellations 1
Session Date June 8 (Thu) 9:00 – 10:20
Room Meeting Room 1
Chairpersons Masayuki Ikeuchi (JAXA, Japan)
Jean-Sébastien Ardaens (DLR, Germany)
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 Martin Serrano2, Bram de Vogeleer3, Berthyl Duesmann4, Cecilia Mezzera5
1Deimos-Space@ESA, ESTEC, Noordwijk, Netherlands, 2Scisys@ESA, ESOC, Darmstadt, Germany, 3Ims space consultancy@ESA, ESOC, Darmstadt, Germany, 4ESA, ESTEC, Noordwijk, Netherlands, 5ESA, ESTEC, Noordwijk, Netherlands, currently GMV, Trescantos, Spain
ISTS-2017-d-092/ISSFD-2017-092 ( 9:40 – 10:00 )
Operational Flight Dynamics System for PROBA-3 Formation Flying Mission
Pablo García, Catherine Praile, Jesús Robles
GMV, Madrid, 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 Aerospace and Astronautics Science, SOKENDAI, Kanagawa, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
[d-21] Orbit Determination 1
Session Date June 8 (Thu) 9:00 – 10:40
Room Meeting Room 2
Chairpersons Tsutomu Ichikawa (Japan Aerospace Exploration Agency, Japan)
Tomas Jorge Martin-Mur (California Institute of Technology, USA)
ISTS-2017-d-094/ISSFD-2017-094 ( 9:00 – 9:20 )
Monte for Orbit Determination
Jonathon Smith, Theodore Drain, Shyam Bhaskaran, Tomas Martin-Mur
California Institute of Technology / Jet Propulsion Laboratory, Pasadena, California
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, located at ESOC, Germany, 2ESA/ESOC, Germany, 3Deimos Space, located at ESOC, Germany, 4GMV, located at ESOC, Germany
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 Broschart1, Shyam Bhaskaran1, Julie Bellerose1, Ann Dietrich2, Dongsuk Han1, Robert Haw1, Nickolaos Mastrodemos1, William Owen, Jr.1, Brian Rush1, David Surovik3
1Jet Propulsion Laboratory, California Institute of Technology, California, USA, 2University of Colorado – Boulder, Colorado, USA, 3Rutgers University, New Jersey, USA
ISTS-2017-d-097/ISSFD-2017-097 ( 10:00 – 10:20 )
A Quasi-Kinematic Orbit Determination Method for Deep Space Probes
Hiroshi Takeuchi1, Tomohiro Yamaguchi1, Makoto Yoshikawa1, Tsutomu Ichikawa1, Naoko Ogawa1, Kazutaka Nishiyama1, Takanao Saiki1, Yuichi Tsuda1, Sho Taniguchi2, Nobuaki Fujii2, Tomoko Yagami2
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2Technical computing solutions unit, science solutions div, Fujitsu Limited, Tokyo, 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, science solutions div, Fujitsu Limited, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 3Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan
[d-22] Trajectory Design & Optimization 3
Session Date June 8 (Thu) 9:00 – 10:40
Room Meeting Room 3
Chairpersons Takayuki Yamamoto (JAXA, Japan)
Hongru Chen (Chinese Academy of Sciences, China)
ISTS-2017-d-100/ISSFD-2017-100 ( 9:20 – 9:40 )
Optimised GTO-GEO Transfer Using Low-Thrust Propulsion
Marilena DI Carlo1, Massimiliano Vasile1, Stephen Kemble2
1Department of Mechanical and Aerospace Engineering, University of Strathclyde, Glasgow, United Kingdom, 2Airbus Defence and Space, Stevenage, United Kingdom
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, Amagasaki, Japan, 2Graduate School of Engineering, Osaka University, Osaka, Japan
ISTS-2017-d-102/ISSFD-2017-102 ( 10:00 – 10:20 )
Operational Concept for Orbit Raising with Low Thrust
Ferdi DE Bruijn, Francesca Letizia, Juan C. Bastante
OHB System AG, Bremen, 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
1School of Aerospace Engineering – ETSIAE, Technical University of Madrid – UPM, Madrid, Spain, 2Dipartimento di Scienze e Tecnologie Aerospaziali, Politecnico di Milano, Milan, Italy, 3Surrey Space Center, University of Surrey, Guildford, UK
[d-23] Formation Flying & Satellite Constellations 2
Session Date June 8 (Thu) 11:00 – 12:00
Room Meeting Room 1
Chairpersons Tatsuaki Hashimoto (Japan Aerospace Exploration Agency, Japan)
Berthyl Duesmann (European Space Agency, Netherlands)
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 Sciences and Technologies, Politecnico di Milano, Milan, 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
1Department of Mechanical Engineering, Stanford University, USA, 2Department of Aeronautics and Astronautics, Stanford University, USA
ISTS-2017-d-106/ISSFD-2017-106 ( 11:40 – 12:00 )
Optimal Trajectory Design of Formation Flying based on Attractive Sets
Motoki Yamane, Mai Bando, Shinji Hokamoto
Department of Aeronautics and Astronautics, Kyushu University, Fukuoka, Japan
[d-24] Orbit Determination 2
Session Date June 8 (Thu) 11:00 – 12:40
Room Meeting Room 2
Chairpersons Hiroshi Takeuchi (JAXA, Japan)
Shyam Bhaskaran (JPL, USA)
ISTS-2017-d-107/ISSFD-2017-107 ( 11:00 – 11:20 )
Radar Observations of Spacecraft in Lunar Orbit
Marina Brozović1, 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-Valentín3
1Jet Propulsion Laboratory/California Institute of Technology, Pasadena, California, USA, 2Green Bank Observatory, Green Bank, West Virginia, USA, 3Arecibo Observatory/Universities Space Research Association, Arecibo, Puerto Rico, USA
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, Pasadena, 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 Boone, Julie Bellerose, Duane Roth
Cassini Navigation Team, Jet Propulsion Laboratory, California Institute of Technology
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 Menon, Sean Wagner, Stuart Demcak, David Jefferson, Eric Graat, Kyong Lee, William Schulze
Jet Propulsion Laboratory, California Institute of Technology, 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 Massimo Casasco (European Space Agency, Netherlands)
Volker Maiwald (German Aerospace Center, Germany)
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 No Initial Guess
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 Fixed-Time Low-Thrust Rendezvous Solved with the Switching Systems Theory
Clément Gazzino1, Denis Arzelier1, Luca Cerri2, Damiana Losa3, Christophe Louembet1, Christelle Pittet2
1LAAS-CNRS, Université de Toulouse, France, 2CNES, Centre Spatial de Toulouse, France, 3Thales Alenia Space, France
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, Chit Hong Yam2, Wen Han Chiu1
1Department of Physics, The Hong Kong University of Science and Technology, Hong Kong, 2ispace inc., Tokyo, 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
1School of Aerospace Engineering – ETSIAE, Technical University of Madrid – UPM, Madrid, Spain, 2Dipartimento di Scienze e Tecnologie Aerospaziali, Politecnico di Milano, Milan, Italy
[d-26] Formation Flying & Satellite Constellations 3
Session Date June 8 (Thu) 14:00 – 15:20
Room Meeting Room 1
Chairpersons Kenji Kitamura (Mitsubishi Electric Corporation, Japan)
Andres Ayala (GMW for European Space Agency, Netherlands)
ISTS-2017-d-117/ISSFD-2017-117 ( 14:00 – 14:20 )
Rendezvous Control of Spacecrafts via Constrained Optimal Control Using Generating Functions
Dijian Chen1, Kenji Fujimoto2
1Department of Mechanical Science and Engineering, Nagoya University, Nagoya, Japan, 2Department of Aeronautics and Astronautics, Kyoto University, Kyoto, Japan
ISTS-2017-d-118/ISSFD-2017-118 ( 14:20 – 14:40 )
Attitude and Orbit Coupled Tumbling Space Debris Tracking Control
Shuquan Wang1, Lingchao Zhu1,2
1Technology and Engineering Center for Space Utilization, China Academy of Sciences, Beijing, China, 2University of Chinese Academy of Sciences, Beijing, China
ISTS-2017-d-119/ISSFD-2017-119 ( 14:40 – 15:00 )
Angles-Only Relative Orbit Determination during the AVANTI Experiment
Jean-Sébastien Ardaens, Gabriella Gaias
German Space Operations Center (DLR/GSOC), Wessling, 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, Sagamihara, Japan
[d-27] Orbit Determination 3
Session Date June 8 (Thu) 14:00 – 15:20
Room Meeting Room 2
Chairpersons Makoto Yoshikawa (Japan Aerospace Exploration Agency, Japan)
Frank Budnik (ESA, Germany)
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, Marco Agnan4, Jordan Vannitsen4,5
1Laboratory of Excellence for Exploration of Space Environments (LabEx ESEP), Paris Observatory, Paris, France, 2Institut de Mecanique Celeste et de Calcul des Ephemerides (IMCCE), Paris Observatory, Paris, France, 3Paris Sciences Lettres (PSL) Research University, Paris Observatory, Paris, France, 4ODYSSEUS Space Co. Ltd., Tainan, Taiwan, 5Department of Aeronautics and Aerospace (DAA), National Cheng Kung University (NCKU), Tainan, Taiwan
ISTS-2017-d-123/ISSFD-2017-123 ( 14:20 – 14:40 )
A Study of the Navigation for Spacecraft by Using the Modified Estimator
Tsutomu Ichikawa
Institute of Space and Astronautical Science, JAXA, Sagamihara, 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
ISTS-2017-d-015/ISSFD-2017-015 ( 15:00 – 15:20 )
Rosetta Navigation during the End of Mission Phase
Pablo Muñoz1, Vicente Companys2, Frank Budnik2, Bernard Godard3, Dario Pellegrinetti1, Gabriele Bellei4, Rainer Bauske5, Waldemar Martens2
1GMV at ESOC, Darmstadt, Germany, 2ESA/ESOC, Darmstadt, Germany, 3Telespazio Vega at ESOC, Darmstadt, Germany, 4Deimos Space at ESOC, Darmstadt, Germany, 5Terma at ESOC, Darmstadt, Germany
[d-28] Trajectory Design & Optimization 5
Session Date June 8 (Thu) 14:00 – 15:40
Room Meeting Room 3
Chairpersons Jun Matsumoto (Japan Aerospace Exploration Agency, Japan)
Yanping Guo (Johns Hopkins University Applied Physics Laboratory, USA)
ISTS-2017-d-126/ISSFD-2017-126 ( 14:00 – 14:20 )
A Smoothed Eclipse Model for Solar Electric Propulsion Trajectory Optimization
Jonathan D. Aziz1, Daniel J. Scheeres1, Jeffrey S. Parker1, Jacob A. Englander2
1University of Colorado Boulder, USA, 2NASA Goddard Space Flight Center, USA
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, The University of Tokyo, Tokyo, Japan, 2Jet Propulsion Laboratory, NASA, Pasadena, California
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
Institute of Space Systems, German Aerospace Center (DLR), Department of System Analysis Space Segment, 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, Diogene Alessandro Dei Tos1, Mirco Rasotto2, Florian Renk3
1Politecnico di Milano, Department of Aerospace Science and Technology, Milan, Italy, 2Dinamica Srl, Milan, Italy, 3European Space Operation Center (ESOC), Darmstadt, Germany
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, Jun’Ichiro Kawaguchi
Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
[d-29] Formation Flying & Satellite Constellations 4
Session Date June 8 (Thu) 16:00 – 17:00
Room Meeting Room 1
Chairpersons Kenji Fujimoto (Kyoto University, Japan)
Ralph Kahle (DLR, Germany)
ISTS-2017-d-131/ISSFD-2017-131 ( 16:00 – 16:20 )
Robust and Safe N-Spacecraft Swarming in Perturbed Near-Circular Orbits
Adam W. Koenig, Simone D’Amico
Department of Aeronautics and Astronautics, Stanford University, Stanford, California, USA
ISTS-2017-d-132/ISSFD-2017-132 ( 16:20 – 16:40 )
Satellite Constellations for Altimetry
Alain Lamy, Josiane Costeraste
CNES – Centre National d’Etudes Spatiales, Toulouse, France
ISTS-2017-d-134/ISSFD-2017-134 ( 16:40 – 17:00 )
Galileo Extended Slots Characterisation and Relation with the Nominal Constellation
Andrés Ayala1, Rubén Castro2, Nityaporn Sirikan3, Daniel Blonski3, Daniel Navarro3
1ESTEC, European Space Agency, GMV, Noordwijk, The Netherlands, 2ESTEC, European Space Agency, WGS, Noordwijk, The Netherlands, 3ESTEC, European Space Agency, ESA, Noordwijk, The Netherlands
[d-30] Orbit Determination 4
Session Date June 8 (Thu) 16:00 – 17:20
Room Meeting Room 2
Chairpersons Sho Taniguchi (Fijitsu Limited., Japan)
Jonathon J Smith (California Institute of Technology / Jet Propulsion Laboratory, USA)
ISTS-2017-d-135/ISSFD-2017-135 ( 16:00 – 16:20 )
Deep-Space Navigation Using Optical Communications Systems
Tomas Martin-Mur, Sarah Elizabeth Mccandless, Reza Karimi
Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, USA
ISTS-2017-d-136/ISSFD-2017-136 ( 16:20 – 16:40 )
The Effectiveness of Solution Technique on the Autonomous Orbit Determination Accuracy of Lagrangian Navigation Constellation
Youtao Gao1, Bingyu Jin1, Tanran Zhao1, Bo Xu2
1College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing, China, 2College of Astronomy and Space Science, Nanjing University, Nanjing, China
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 Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
ISTS-2017-d-139/ISSFD-2017-139 ( 17:00 – 17:20 )
Autonomous Orbit Determination of Multiple Spacecraft Using Active Sensing with Satellite-to-Satellite Tracking
Kota Kakihara, Naoya Ozaki, Ryu Funase
Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan
[d-31] Orbit Determination 5
Session Date June 9 (Fri) 14:00 – 15:40
Room Meeting Room 2
Chairpersons Takanori Iwata (JAXA, Japan)
Pierluigi Righetti (EUMETSAT, Germany)
ISTS-2017-d-140/ISSFD-2017-140 ( 14:00 – 14:20 )
Generalized Image Navigation & Registration Method Based on Kalman Filter
Ahmed A. Kamel1, Handol Kim2, Dochul Yang2, Chul-Min Park3, Jin Woo4
1Kamel Engineering Services, Los Angeles, California, USA, 2Korea Aerospace Research Institute, Daejeon, ROK, 3Korea Aerospace Industries, ROK, 4Korea Meteorological Administration, Daebang-dong, ROK
ISTS-2017-d-141/ISSFD-2017-141 ( 14:20 – 14:40 )
Satellite Autonomous Navigation with No Ground Links for Korea Regional Navigation Satellite System
Hyungjik Oh1, Young-Rok Kim2, Chandeok Park1, Seung-Mo Seo3
1Department of Astronomy, Yonsei University, Seoul 03722, Republic of Korea, 2Korea Aerospace Research Institute, Daejeon, Republic of Korea, 3Agency for Defense Development, Daejeon, Republic of Korea
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 Lilly-Salkowski
Omitron, Inc., USA
ISTS-2017-d-144/ISSFD-2017-144 ( 15:20 – 15:40 )
Generalised Polynomial Chaos Based Particle Filter for Orbit Determination
Yang Yang1,2, Yanlong Bu3
1SPACE Research Centre, School of Science, RMIT University, Melbourne, Australia, 2Space Environment Research Centre, Canberra, Australia, 3Beijing Aerospace Control Centre, Beijing, China
[d-32] Mission Analysis & Design 1
Session Date June 9 (Fri) 14:00 – 15:40
Room Meeting Room 3
Chairpersons Katsuhiko Yamada (Osaka University, Japan)
Natan Eismont (Space Research Institute of the Russian Academy of Sciences, Russia)
ISTS-2017-d-145/ISSFD-2017-145 ( 14:00 – 14:20 )
Advanced Methods of Low Cost Mission Design for Jovian Moons Exploration
Alexey Grushevskii, Yuri Golubev, Victor Koryanov, Andrey Tuchin, Denis Tuchin
KIAM (Keldysh Institute of Applied Mathematics of RAS), Russian Federation
ISTS-2017-d-146/ISSFD-2017-146 ( 14:20 – 14:40 )
Solar Probe Plus: Primary and Backup Launch Windows
Yanping Guo
The Johns Hopkins University Applied Physics Laboratory, Maryland, USA
ISTS-2017-d-147/ISSFD-2017-147 ( 14:40 – 15:00 )
Solar Orbiter Trajectory Profile and Navigation Challenges
José Manuel Sánchez Pérez, Frank Budnik
European Space Agency, ESA, ESOC, Darmstadt, Germany
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
California Institute of Technology, Jet Propulsion Laboratory, Pasadena, USA
ISTS-2017-d-149/ISSFD-2017-149 ( 15:20 – 15:40 )
Guidance Navigation and Control Challenges for the ESA Asteroid Impact Mission
Massimo Casasco1, Jesus GIL Fernandez1, Guillermo Ortega1, Ian Carnelli2
1European Space Technology Centre, Noordwijk, The Netherlands;, 2European Space Agency Headquarters, Paris, France
[d-33] Attitude Control 1
Session Date June 9 (Fri) 14:00 – 15:20
Room Sub-Hall
Chairperson Hirohisa Kojima (Tokyo Metropolitan University, Japan)
ISTS-2017-d-150/ISSFD-2017-150 ( 14:00 – 14:20 )
LMI-based Mixed H2/H Control with Regional Constraints for Spacecraft Attitude Tracking
Takahiro Sasaki1,2,3, Takashi Shimomura1, Sayaka Kanata1
1Department of Aerospace Engineering, Osaka Prefecture University, Osaka, Japan, 2Department of Aerospace Engineering Science, University of Colorado Boulder, Colorado, USA, 3Research Fellow of Japan Society for the Promotion of Science (DC1)
ISTS-2017-d-151/ISSFD-2017-151 ( 14:20 – 14:40 )
Fast Slew Maneuvers for the High-Torque-Wheels BIROS Satellite
Paul Acquatella B.
DLR, German Aerospace Center, Institute of System Dynamics and Control, Oberpfaffenhofen, Germany
ISTS-2017-d-152/ISSFD-2017-152 ( 14:40 – 15:00 )
Single Axis Pointing for Underactuated Spacecraft with a Residual Angular Momentum
Alessandro Zavoli1, Fabrizio Giulietti2, Giulio Avanzini3, Guido de Matteis1
1Department of Mechanical and Aerospace Engineering, ‘Sapienza’ Università di Roma, Rome, Italy, 2Department of Industrial Engineering, Università di Bologna (ForlÌ Campus), ForlÌ, Italy, 3Department of Engineering for Innovation, Università del Salento, Lecce, Italy
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 Endo, Kazuma Sekiguchi, Kenichiro Nonaka
Department of Mechanical Systems Engineering, Tokyo City University,Tokyo, Japan
[d-34] Orbit Determination 6
Session Date June 9 (Fri) 16:00 – 16:40
Room Meeting Room 2
Chairpersons Frank Budnik (ESA, Germany)
Yang Yang (RMIT University, Australia)
ISTS-2017-d-155/ISSFD-2017-155 ( 16:00 – 16:20 )
Orbit Determination for the MICROSCOPE Mission Specificities and Performance
David Pascal, John Moyard, Flavien Mercier, Pierre-Yves Guidotti, Thomas Junique, Romain Mathieu
CNES, Toulouse, France
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
Milan Klinc1, Stefano Pessina2
1Independent Consultant at EUMETSAT, Flight Operations Division, EUMETSAT, Darmstadt, Germany, 2Flight Operations Division, EUMETSAT, Darmstadt, Germany
[d-35] Mission Analysis & Design 2
Session Date June 9 (Fri) 16:00 – 17:40
Room Meeting Room 3
Chairpersons Ryu Funase (The University of Tokyo, Japan)
Alain Lamy (CNES, France)
ISTS-2017-d-158/ISSFD-2017-158 ( 16:00 – 16:20 )
Mission Design Problems for Spectrum-Roentgen-Gamma Project
Ravil Nazirov1, Natan Eismont1, Vadim Arefiev1, Fedor Korotkov1, Andrei Pogodin2, Andrei Tregubov3, Alexey Ditrikh3
1Space Research Institute of the Russian Academy of Sciences, Russia, 2Lavochkin Association, Russia, 3Russian Space Corporation Energia
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 Yam3, Yuki Kayama4, Yasuhiro Kawakatsu5, Naoya Ozaki6, Quentin Verspieren6, Kota Kakihara6, Kenshiro Oguri6, Ryu Funase6
1Department of Applied Mechanics and Aerospace Engineering, Waseda University, Tokyo, Japan, 2Jet Propulsion Laboratory, California Institute of Technology, CA, USA, 3ispace inc., Tokyo, Japan, 4Department of Advanced Energy, The University of Tokyo, Tokyo, Japan, 5Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 6Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan
ISTS-2017-d-072/ISSFD-2017-072 ( 16:40 – 17:00 )
EQUULEUS Mission Analysis: Design of the Science Orbit Phase
Kenshiro Oguri1, Kota Kakihara1, Stefano Campagnola2, Naoya Ozaki1, Kenta Oshima3, Tomohiro Yamaguchi4, Ryu Funase1
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Jet Propulsion Laboratory, California Institute of Technology, CA, USA, 3Department of Applied Mechanics and Aerospace Engineering, Waseda University, Tokyo, Japan, 4Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
ISTS-2017-d-160/ISSFD-2017-160 ( 17:00 – 17:20 )
Preliminary Mission Design and Analysis of a Lunar Far-side Positioning CubeSat Mission
Hongru Chen1, Lei Liu2,3, Yazhe Meng1,4, Zhenyu Xu1,4, Long Long1,4, Jiangkai Liu1,4
1Key Labrotary of Space Utilization, Technology and Engineering Center for Space Utilization, Chinese Academy of Sciences, Beijing, China, 2College of Science, National University of Defense Technology, Changsha, China, 3Beijing Aerospace Control Center, Beijing, China, 4University of Chinese Academy of Sciences, Beijing, China
ISTS-2017-d-161/ISSFD-2017-161 ( 17:20 – 17:40 )
SIRIUS-DV: The New Flight Dynamics Algorithms for the Future CNES Missions
Iván Llamas1, Yannick Tanguy2, Michel Lacotte2, Jean-Jacques Wasbauer2
1GMV, Madrid, Spain, 2CNES, Toulouse, France
[d-36] Attitude Control 2
Session Date June 9 (Fri) 16:00 – 17:40
Room Sub-Hall
Chairpersons Takashi Shimomura (Osaka Prefecture University, Japan)
Alessandro Zavoli (Rome – Sapienza, Italy)
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, Hino, Japan
ISTS-2017-d-163/ISSFD-2017-163 ( 16:20 – 16:40 )
Attitude Control using Three Control Moment Gyros
Sho Nonomura1, Andrew Meldrum2, Katsuhiko Yamada1, Yasuhiro Shoji1
1Graduate School of Engineering, Osaka University, Osaka, Japan, 2School of Engineering, Osaka University, Osaka, Japan
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, Sakai, Japan, 2Advanced Technology R&D Center, Mitsubishi Electric Corp, Amagasaki, Japan
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, Tokyo, Japan, 2Department of Mechanical Engineering, Tokyo Institute of Technology, Tokyo, Japan
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, Katsuhiko Yamada, Yasuhiro Shoji
Graduate School of Engineering, Osaka University, Osaka, Japan
[e-1] Plasma Flows (1)
Session Date June 7 (Wed) 11:00 – 12:00
Room Meeting Room 15
Chairpersons Hirotaka Otsu (Ryukoku University, Japan)
Hiroshi Katsurayama (Yamaguchi University, Japan)
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, Koganei, 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 Nishida2
1Department of Mechanical and Aerospace Engineering, Tottori University, Tottori, Japan, 2Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology, Japan
[e-2] Plasma Flows (2)
Session Date June 8 (Thu) 9:00 – 10:40
Room Meeting Room 15
Chairpersons Takashi Matsuno (Tottori University, Japan)
Atsushi Matsuda (Meijo University, Japan)
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, Shiga, Japan
2017-e-06 ( 9:20 – 9:40 )
Experimental Investigation of the Role of an Insulating Boundaryin 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, Yamaguchi, Japan, 2Interdisciplinary Graduate School of Engineering Science, Kyushu University, Fukuoka, Japan, 3Graduate School of Integrated Science and Technology, Shizuoka University, Shizuoka, Japan
2017-e-07 ( 9:40 – 10:00 )
Electron Density Measurement by Mach-Zehnder Interferometer Using CO2 Laser for an Atmospheric Pressure Plasma
Takafumi Yamada, Makoto Matsui
Graduate School of integrated Science and Technology, Department of Engineering, Shizuoka University, Hamamatsu, Japan
2017-e-08 ( 10:00 – 10:20 )
Temperature Estimations of SiC Ablations with Several Kinds of Narrow Band-pass Filters
Makoto Hashimoto1, Nurul Malisa2, Masato Funatsu1, Gen Morioka3, Masahiro Ozawa4
1Graduate School of Science and Technology, Gunma University, Kiryu, Japan, 2Tateyama Auto Machine Co., (M) Sdn., Bhd., Shah Alam, Malaysia, 3Mitsubishi Electric Engineering Co., Ltd., Kamakura, Japan, 4Chuo Engineering Co., Ltd., Tokyo, Japan
2017-e-09 ( 10:20 – 10:40 )
Numerical Estimation of Laser-Ablation Propulsion Performance In Spherical Capsule
Chongfa Xie, Thuan Duc Tran, Koichi Mori
Department of Aeronautics and Astronautics, Nagoya University, Nagoya, Japan
[e-3] Atmospheric Entry (1)
Session Date June 8 (Thu) 11:00 – 12:20
Room Meeting Room 15
Chairpersons Hide Tanno (Japan Aerospace Exploration Agency, Japan)
Makoto Matsui (Shizuoka University, Japan)
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, Tokyo, Japan, 2Tottori University, Tottori, Japan, 3Nagoya University, Nagoya, Japan
2017-e-12 ( 11:40 – 12:00 )
One-dimensional Ablation Analysis of Lightweight CFRP Ablators with Coking
Sumio Kato1, Shoichi Matsuda1, Naoyuki Shimada2, Shunsuke Sakai1, Keiichi Okuyama3, Bianca Szasz3, Takayuki Shimoda4
1University of the Ryukyus, Japan, 2Asahi Kinzoku Kogyo Inc. Japan, 3Kyushu Institute of Technology, Japan, 4JAXA/ISAS, Japan
2017-e-13 ( 12:00 – 12:20 )
Thermal Response Analysis Of Porous Carbon-based Non-Ablative Heatshield In An Arcjet Flow Condition
Takumi Horiuchi1, Takeharu Sakai2, Hiroki Fukui1, Yuichi Ishida3, Toshiyuki Suzuki3, Kazuhisa Fujita3
1Department of Aerospace Engineering, Nagoya University, Nagoya, Japan, 2Department of Mechanical and Aerospace Engineering, Tottori University, Tottori, Japan, 3Japan Aerospace Exploration Agency, Chofu, Japan
[e-4] Atmospheric Entry (2)
Session Date June 8 (Thu) 14:00 – 15:40
Room Meeting Room 15
Chairpersons Takeharu Sakai (Tottori University, Japan)
Masato Funatsu (Gunma University, Japan)
2017-e-14 ( 14:00 – 14:20 )
Visualization of Wake Flows of Supersonic Mars Entry Capsule with Light Gus Gun
Satoshi Nomura1, Kao It2, Shingo Matsuyama1, Kazuhisa Fujita1
1Aeronautical Technology Directorate, JAXA, Chofu, Japan, 2Department of Systems Integration, Yokohama National University, Yokohama, Japan
2017-e-15 ( 14:20 – 14:40 )
Numerical Simulation of Flow Conditions Generated by Hyper Velocity Expansion Tube
Tohru Yamada1, Lemal Adrian2, Shingo Matsuyama2, Satoshi Nomura2, Hiroki Takayanagi2, Kazuhisa Fujita2, Makoto Matsui1
1Shizuoka University, Shizuoka, Japan, 2JAXA, Tokyo, Japan
2017-e-16 ( 14:40 – 15:00 )
Electron Temperature and Number Density Measurements Ahead of a Strong Shock Wave
Taito Kawakami1, Satoshi Nomura2, Sayaka Nishimura1, Kazuhisa Fujita2, Makoto Matsui1
1Department of Engineering, Shizuoka University, Hamamatsu, Japan, 2Japan Aerospace Exploration Agency, Chofu, Tokyo, Japan
2017-e-17 ( 15:00 – 15:20 )
Aerodynamic Characteristics of HYFLEX Lifting Body in Shock Tunnel HIEST
Hideyuki Tanno, Katsuhiro Itoh, Tomoyuki Komuro, Kazuo Sato
Kakuda Space Center, JAXA, Kakuda, Miyagi, Japan
2017-e-18 ( 15:20 – 15:40 )
Simulation of Ionization and Electronic Excitation in Hypersonic Shock Tube Flows Using DSMC
T. Ozawa1, S. Nomura1, T. Kawakami2, A. Lemal1, K. Fujita1
1Research and Development Directorate, JAXA, Chofu, Japan, 2Shizuoka Universitye,Hamamatsu, Japan
[e-5] Aerodynamic Decelerator, Balloon (1)
Session Date June 8 (Thu) 16:00 – 17:20
Room Meeting Room 15
Chairpersons Yusuke Maru (Japan Aerospace Exploration Agency, Japan)
Katsuyoshi Fukiba (Shizuoka University, Japan)
2017-e-19 ( 16:00 – 16:20 )
Aerothermodynamic Studies on Low-Ballistic-Coefficient Mars Aerocapture Vehicle with Drag Modulation and Ion Thruster
Kojiro Suzuki
Department of Advanced Energy, The University of Tokyo, Tokyo, Japan
2017-e-20 ( 16:20 – 16:40 )
Thermal-durability Evaluation of Inflatable Structure for a Deployable Aeroshell Using ICP Heater
Kazushige Matsumaru1, Mayuko Tanaka2, Osamu Imamura3, Kazuhiko Yamada4
1Department of Mechanical Engineering, Nihon University, Chiba, Japan, 2Department of Applied Mechanics, Waseda University, Tokyo, Japan, 3Department of Sustainable Engineering, Nihon University, Chiba, Japan, 4The Institute of Space and Astronatical, JAXA, Sagamihara , Japan
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, Tokyo, Japan, 2Department of Advanced Energy, The University of Tokyo, Tokyo, Japan
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, The University of Tokyo, Tokyo, Japan
[e-6] Aerodynamic Decelerator, Balloon (2)
Session Date June 9 (Fri) 9:00 – 10:20
Room Meeting Room 15
Chairpersons Kojiro Suzuki (The University of Tokyo, Japan)
Osamu Imamura (Nihon University, Japan)
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 Minami2, Hirokazu Adachi2, Yoshihisa Aoki2, Toshio Fukui2, Toshiaki Daibo2, Takashi Mugitani2, Taro Tsukamoto2, Shinji Ishimoto2, Takehiro Kumagai3, Hirofumi Shirouzu3, Koji Ohga3
1Research Unit II, Research and Development Directorate, JAXA, Chofu, Japan, 2Research Unit IV, Research and Development Directorate, JAXA, Chofu, Japan, 3Flight Research Unit, Aeronautical Technology Directorate, JAXA, Mitaka, Japan
2017-e-25 ( 9:20 – 9:40 )
Wind Tunnel Tests on Pressure Oscillation in Supersonic Parachutes
Kazuki Mizuta
Shizuoka University, Hamamatsu, 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
1Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology, TAT, Koganei, Japan, 2School of Fundamental science and Engineering, Waseda University, Tokyo, Japan, 3Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
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, JAXA, Sagamihara, Japan, 2Division of Mechanical and Space Engineering, Hokkaido University, Sapporo, Japan, 3Department of Space and Astronautical Science, The Graduate University for Advanced Studies, Sagamihara, Japan
[e-7] Aerodynamics (1)
Session Date June 9 (Fri) 11:00 – 12:00
Room Meeting Room 15
Chairpersons Toshiyuki Suzuki (Japan Aerospace Exploration Agency, Japan)
Hiroyuki Nishida (Tokyo University of Agriculture and Technology, Japan)
2017-e-29 ( 11:00 – 11:20 )
Aerodynamic Analysis on Flight Vehicle with Protuberant Devices
Toshiaki Harada1, Keiichi Kitamura1, Satoshi Nonaka2
1Graduate School of Engineering, Yokohama National University, Kanagawa, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
2017-e-31 ( 11:20 – 11:40 )
Experimental Investigation on the Effectiveness of Micro-jets to Restrain the Base Pressure of Space Vehicles
Musavir Bashir1, Parvathy Rajendran1, S. A. Khan2
1School of Aerospace Engineering, University Sains Malaysia, Penang, Malaysia., 2Department of Mechanical Engineering, IIUM, Kuala Lumpur, Malaysia
2017-e-32 ( 11:40 – 12:00 )
Flow Induced Vibrations of Entry Capsule Models
Koju Hiraki1, Kota Tanaka1, Yuma Yanaga1, Harald Kleine2
1Kyushu Institute of Technology, Kitakyushu, Japan, 2Department of Aeronautics and Astronautics, The University of New South Wales, Canberra, Australia
[e-8] Aerodynamics (2)
Session Date June 9 (Fri) 14:00 – 15:40
Room Meeting Room 15
Chairpersons Nobuyuki Tsuboi (Kyushu Institute of Technology, Japan)
Koju Hiraki (Kyushu Institute of Technology, Japan)
2017-e-33 ( 14:00 – 14:20 )
Aeroelastic Analysis for the High Altitude Propeller by Using Fluid-Structure Interaction Method
Zhengyu Qu, Yanchu Yang, Ying Nie
Academy of Opto-Electronics, Chinese Academy of Science, Beijing, China
2017-e-34 ( 14:20 – 14:40 )
Design of an Efficient Propeller for Low-Reynolds Number Application
Umunna. J. Reuben, Hiraki Koju, Kinjo Satoru
Space Dynamic laboratory, Kyushu Institute of Technology, Kitakyushu, Japan
2017-e-35 ( 14:40 – 15:00 )
Effect of Leading Edge Profile on the Flow Phenomenon of Delta Wing
Ramakrishna Madhira1, Senthil Kumar C2
1Assistant Professor, Dept. of Aeronautical Engg., Tagore Engineering College, Chennai, India, 2Assistant Professor, Dept. of Aeronautical Engg., MIT Campus, Anna University, Chrompet, Chennai, India
2017-e-36 ( 15:00 – 15:20 )
Mach and Reynolds Numbers Effects on Aerodynamics of Delta Wing in Mars Wind Tunnel Experiments
Daichi Ishiwaki, Taku Nonomura, Shintaro Andoh, Keisuke Asai
Departemnt of Aerospace Engineering, Graduate School of Engineering, Tohoku University, Sendai, Miyagi, Japan
2017-e-37 ( 15:20 – 15:40 )
A Study on The Interaction Mechanism of Coaxial Jet Exhausted from a Body in Hypersonic Flow
Mohammad Samara1, Yasumasa Watanabe2, Kojiro Suzuki1
1Department of Advanced Energy, Graduate School of Frontier Sciences, The University of Tokyo, Kashiwa, Japan, 2Department of Aeronautics and Astronautics, Graduate School of Engineering, The University of Tokyo, Tokyo, Japan
[e-9] Computational Fluid Dynamics
Session Date June 9 (Fri) 16:00 – 17:20
Room Meeting Room 15
Chairpersons Taku Nonomura (Tohoku University, Japan)
Katsuyoshi Fukiba (Shizuoka University, Japan)
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, Ehime University, Ehime, Japan, 2Institute of Laser Engineering, Osaka University, Osaka, Japan
2017-e-39 ( 16:20 – 16:40 )
On Causal Structures in Fluid Mechanics
Trevor H. Moulden
The University of Tennessee Space Institute, Tullahoma, USA
2017-e-41 ( 16:40 – 17:00 )
The Interfacial Nanobubbles Studied by Molecular Dynamics Simulations
Tsu-Hsu Yen
Marine Science, R.O.C Naval Academy, Taiwan
2017-e-42 ( 17:00 – 17:20 )
Numerical Investigation of the Radiation Transfer in a Laser Sustained Plasma Wind Tunnel with Carbon-dioxide Gas
Yutaro Ehara1, Hiroshi Katsurayama1, Makoto Matsui2, Takeharu Sakai3, Katoh Yasuo1
1Graduate School of Sciences and Technology for Innovation, Yamaguchi University, Ube, Japan, 2Graduate School of Integrated Science and Technology, Shizuoka University, Shizuoka, Japan, 3Graduate School of Engineering, Tottori University, Tottori, Japan
[f-1] Mission1
Session Date June 6 (Tue) 9:00 – 10:20
Room Pearl Room A
Chairpersons Hironori Sahara (Tokyo Metropolitan University, Japan)
Tsuyoshi Totani (Hokkaido University, Japan)
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 System Design for AMMEQ-1: A Step towards QKD
Eugene Kim1, Xiaofeng Wu1, Trevor Kwan1, Robert Bedington2, Xueliang Bai2, Alexander Ling2
1School of Aerospace, Mechanical and Mechatronics Engineering, The University of Sydney, Australia, 2Centre for Quantum Technologies, National University of Singapore, 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 Ho Holden2
1Kyushu Institute of Technology, Japan, 2Nanyang Technological University, Singapore
[f-2] Mission2
Session Date June 6 (Tue) 11:00 – 12:20
Room Pearl Room A
Chairpersons Sangkyun Kim (Kyushu Institute of Technology, Japan)
Masaaki Kawamura (University of Teikyo, Japan)
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 Iijima6, Shin Takeuchi7, Osamu Konno7, Taizoh Yamamoto8, Naoki Kabaya9, Giichi Sakemi10, Kenji Ishida11, Yu Okumura12, Yuji Nishikawa12, Shouhei Minami12, Kazuhito Miura12, Soopal Hong12, Astrex Kansai Satellite Group , Dream Satellite Project Team
1Kobe University, Japan, 2AstreX, Japan, 3Osaka Institute of Technology, Japan, 4Tokai University, Japan, 5Ao SysTem eneRgy Exploration, Japan, 6KOBE ENGINEERING Co., Ltd., Japan, 7Nissin inc., Japan, 8YAMAMOTO METAL TECHNOS CO., LTD., Japan, 9FUTUREAGRI Co., Ltd., Japan, 10Fantastical AeroSpace Promotion Incorporated Association, Japan, 11JAPAN FUTEC Co., Ltd., Japan, 12Nichiwa System, Japan
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
1Graduate School of Pure and Applied Sciences, University of Tsukuba, Japan, 2Graduate School of Systems and Information Engineering, University of Tsukuba, Japan, 3Faculty of Engineering, Information and Systems, University of Tsukuba, Japan
2017-f-008 ( 11:40 – 12:00 )
Mission Definition and Preliminary Design of NanoDragon, the First Vietnamese Nanosatellite
Nguyen Dinh Chau Minh1, Vu Viet Phương1, Le Xuan Huy1, Pham Anh Tuan1, Truong Xuan Hung1, Nguyen Truong Thanh1, Hoang The Huynh1, Pham Anh Minh1,2
1Vietnam National Satellite Center, 2Graduate School of System Design and Management, Keio University
2017-f-009 ( 12:00 – 12:20 )
Software Demodulation Technique for the Store and Forward System of Vietnam’s first 
Micro-Satellite MicroDragon
James Harpur1, Toshinori Kuwahara1, Ngo Thanh Cong1,2, Ta Phuong Linh1,2, Nguyen Phuong Mai1,2, Tran Van Ninh1,2, Nguyen Minh Thao1,2, Kazuya Yoshida1
1Department of Aerospace Engineering, Tohoku University, Sendai, Japan, 2Vietnam National Satellite Center, Vietnam Academy of Science and Technology, Hanoi, Vietnam
[f-3] Mission3
Session Date June 6 (Tue) 14:00 – 15:40
Room Pearl Room A
Chairpersons Alim Rustem Aslan (Istanbul Technical University, Turkey)
Shinichi Nakasuka (The University of Tokyo, Japan)
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 Fukuda2, Koyo Taniwaki2, Hirokazu Masui2, Horyu-Iv Project Team 2, Koichi Takamiya3, Mengu Cho2
1National Authority for Remote Sensing and Space Sciences (NARSS), Egypt, 2Kyushu Institute of Technology (Kyutech), Japan, 3Kyoto 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 Yamazaki1, Katsuya Shibata2, Masaaki Kawamura1
1Department of Aerospace Engineering, Faculty of Science and Engineering, Teikyo University, Tochigi, Japan, 2Division of Integrated Science and Engineering, Graduate School of Science and Engineering, Teikyo University, Tochigi, 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 GravitationalWave Sources
Kyosuke Tawara1, Shohei Harita2, Yoichi Yatsu2, Saburo Matunaga3
1Department of Mechanical and Aerospace Engineering, Tokyo Institute of Technology, Tokyo, Japan, 2Department of Physics, Tokyo Institute of Technology, Tokyo, Japan, 3Department of Mechanical Engineering, Tokyo Institute of Technology, Tokyo, Japan
2017-f-014 ( 15:20 – 15:40 )
UNISEC-Global Challenge: An approach for Contribution to Debris Mitigation – Deorbit Device Competition
Rei Kawashima1, Alim Rüstem Aslan2, Yasuyuki Miyazaki3, Mohammed Khalil Ibrahim3, Herman Steyn4
1UNISEC-Global, Tokyo, Japan, 2Istanbul Technical University, Istanbul, Turkey, 3Nihon University, Chiba, Japan, 4Stellenbosch University, Stellenbosch, South Africa
[f-4] BIRDS
Session Date June 6 (Tue) 16:00 – 17:40
Room Pearl Room A
Chairpersons Toshinori Kuwahara (Tohoku University, Japan)
Toshihiro Kameda (University of Tsukuba, Japan)
2017-f-015 ( 16:00 – 16:20 )
Overview of Joint Global Multi-Nation Birds Satellite Project
Taiwo Raphael Tejumola1, Birds Project Members 1, Birds Partners 1, George Maeda1, Sangkyum Kim1, Hirokazu Masui1, Mengu Cho1
1Laboratory of Spacecraft Environment Interaction Engineering, 2Kyushu Institute of Technology, Kitakyushu. Japan
2017-f-016 ( 16:20 – 16:40 )
Design, Manufacture and Verification of CubeSat Structure for BIRDS Constellation
Ibukun Adebolu, BIRDS Project Members , BIRDS Partners , George Maeda, Sangkyun Kim, Hirokazu Masui, Mengu Cho
Laboratory of Space Environment Interaction Engineering Kyushu Institute of Technology, Kitakyushu, Japan
2017-f-017 ( 16:40 – 17:00 )
Design and Verification of BIRDS Project Mission Data Downlink System
Maisun Ibn Monowar1, BIRDS Project Members 1, BIRDS Partners 1, George Maeda1, Sangkyun Kim1, Hirokazu Masui1, Mengu Cho1, Kaname Kojima2
1Laboratory of Spacecraft Environment Interaction Engineering, Kyushu Institute of Technology, Kitakyushu, Japan, 2Addnics Corp., Japan
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 Quansah, BIRDS Project Members , BIRDS Partners , George Maeda, Sangkyun Kim, Hirokazu Masui, Mengu Cho
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 Yasuyuki Miyazaki (Nihon University, Japan)
Kazuhiko Yamada (Japan Aerospace Exploration Agency, Japan)
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 Watanabe10, Takashi Abe1, MAAC group 1
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology, Koganei, Japan, 3Collage of Industrial Technology, Nihon University, Narashino, Japan, 4Department of Material Science and Technology, Tokyo University of Science, Tokyo, Japan, 5Graduate School of Frontier Sciences, The University of Tokyo, Kashiwa, Japan, 6Department of International Development Engineering, Tokyo Institute of Technology, Tokyo, Japan, 7Graduate school of Natural Science and technology, Okayama University, Okayama, Japan, 8Graduate School of Engineering, Osaka University, Suita, Japan, 9 Faculty of Engineering, Hokkaido University, Sapporo, Japan, 10Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan
2017-f-022 ( 9:20 – 9:40 )
SIMON, an Electric Propulsion CubeSat Test Bed for CAPE
Valentin Belser1, Jonas Burgdorf2, Manfred Ehresmann1,2, Daniel Galla1, Markus Koller1, Martin Siedorf1, Valentin Starlinger1, Sascha Wizemann1, Georg Herdrich2, Adam S. Pagan2, Christoph Montag2, René Laufer3,4
1Small Satellite Student Society KSat e.V., University of Stuttgart, Germany, 2Institute of Space Systems, University of Stuttgart, Germany, 3CASPER, Baylor University, USA, 4Space Lab, University of Cape Town, South Africa
2017-f-023 ( 9:40 – 10:00 )
Development of CubeSat OrigamiSat-1 for Space Demonstration of Deployable Membrane Structure Technologies
Hiraku Sakamoto1, Hiroki Nakanishi1, Hiroshi Furuya1, Masahiko Yamazaki2, Yasuyuki Miyazaki2, Akihito Watanabe3, Kazuki Watanabe4, Ayako Torisaka-Kayaba5
1Tokyo Institute of Technology, Tokyo, Japan, 2Nihon University, Chiba, Japan, 3Sakase Adtech, Co., Ltd., Fukui, Japan, 4WEL Research Co., Ltd., Chiba, Japan, 5Tokyo Metropolitan University, Tokyo, Japan
2017-f-024 ( 10:00 – 10:20 )
Development of Internal Antenna Deployment Mechanism for a CubeSat
Raihana S. I. Antara, BIRDS Project , BIRDS Partners , George Maeda, Sangkyun Kim, Hirokazu Masui, Mengu Cho
Laboratory of Spacecraft Environment Interaction Engineering Kyushu Institute of Technology, Kitakyushu, Japan
[f-6] Constellations
Session Date June 7 (Wed) 11:00 – 12:40
Room Pearl Room A
Chairpersons Mengu Cho (Kyushu Institute of Technology, Japan)
Shinichi Nakasuka (The University of Tokyo, Japan)
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
Koh-Ichiro Oyama1,2,3, T. Kodama4
1Institute of Space and Plasma Sciences, National Cheng Kung University, Tainan,Taiwan, 2International Center of Space Weather Study and Education, Fukuoka, Japan, 3CoLtd Asia Space Environment Research Consortium, Sagamihara, Japan, 4Japan Space Exploration Agency, Tsukuba, Japan
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 A. Dei Tos, Daniele Filippetto, Aureliano Rivolta, Karthik Venkatesh Mani
Politecnico di Milano, Italy
2017-f-029 ( 12:20 – 12:40 )
The DLR Small-Satellite Constellation FireBird
Halle W., Terzibaschian Th., Bärwald W., Schultz C.
Institute of Optical Sensor Systems, Germany
[f-7] STARS-E
Session Date June 7 (Wed) 16:00 – 17:20
Room Pearl Room A
Chairpersons Hiraku Sakamoto (Tokyo Institute of Technology, Japan)
Takaya Inamori (Nagoya University, Japan)
2017-f-030 ( 16:00 – 16:20 )
Velocity Control Applied to Tether Reel Mounted on STARS-E
Atsushi Bito, Masahiro Nohmi
The University of Shizuoka, 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 Nohomi
Shizuoka University , Shizuoka, Japan
2017-f-032 ( 16:40 – 17:00 )
Design of the Communication Antenna for the STARS-E Climber
Tomohiro Kakuta
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 Coste1, Shun Yokota1, Tomohiro Kakuta1, Yudai Kuramoto1, Yoshio Aoki1, Yoshiki Yamagiwa2, Masahiro Nohmi2, Isao Yoda3
1Nihon University, Japan, 2Shizuoka University, Japan, 3Tokyo Institute of Technology, Japan
[f-8] Infrastructure
Session Date June 8 (Thu) 9:00 – 10:20
Room Pearl Room A
Chairpersons Mohammed Khalil Ibrahim (Nihon University, Japan)
Kenneth Olafsson (KSAT – Kongsberg Satellite Services AS, Norway)
2017-f-034 ( 9:00 – 9:20 )
Integrated Ground Network Technologies – “KSAT Lite” Small Antenna Network
Kenneth Olafsson
Kongsberg Satellite Services (KSAT), Tromsø, Norway
2017-f-035 ( 9:20 – 9:40 )
Advantages of a Cubesat Receiving Station Located in the South of the Indian Ocean
Vincent Dinnat, Julie Hoarau, Lucas Kerdoncuff, Esteban Decline, Brice Lagarigue, Noann Mondon, Evan Piffarelly, Iannis Poquet
Lycée Bois d’Olives, Saint-Pierre, Reunion Island
2017-f-036 ( 9:40 – 10:00 )
Affordable Small Satellites Launch Options Research
Elena Petrakova, Valery Panasenkov
Moscow Aviation Institute (National Research University), Moscow, Russian Federation
2017-f-037 ( 10:00 – 10:20 )
Aggregated Preference Value Analysis on Small Satellite Launch Opportunities
Mengying Zhang1, Qin Xu1, Qiangang Tang2, Qingbin Zhang2
1School of Mechanical, Aerospace and Civil Engineering, The University of Manchester, UK, 2Department of Aerospace Science and Technology, National University of Defense Technology, Changsha, Hunan, China
[f-9] Beyond Earth
Session Date June 8 (Thu) 11:00 – 12:40
Room Pearl Room A
Chairpersons Ryu Funase (The University of Tokyo, Japan)
Yasuhiro Kawakatsu (JAXA, Japan)
2017-f-038 ( 11:00 – 11:20 )
Thinking Outside the “Cube”
Anita Bernie, Alex da Silva Curiel, Nikki Jahn, Luis Gomes, Sir Martin Sweeting
Surrey Satellite Technology Ltd., Guildford, UK
2017-f-039 ( 11:20 – 11:40 )
Making Small Lunar Missions Viable
Alex da Silva Curiel1, Susan Jason1, Jonathan Friend1, Chris Saunders1, Matthew Cosby2, James Carpenter3, Andreas Borregrafe3, Berhard Hufenbach3, Veronica La Regina3, Martin Sweeting1
1Surrey Satellite Technology Ltd., UK, 2Goonhilly Earth Station Ltd., 3European Space Agency
2017-f-040 ( 11:40 – 12:00 )
Spacecraft in the Shot: A Platform for Deep-Space Cinematography
Jessie M Kawata, Jonathon Smith
NASA Jet Propulsion Laboratory, California Institute of Technology, 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 Tan Chiang Eric2, Kazumasa Imai1, Nobuto Hirakoso2, Taku Takada1, Kentarou Kitamura3
1National Institute of Technology, Kochi College, Japan, 2National Institute of Technology, Gunma College, Japan, 3National Institute of Technology, Tokuyama College, Japan
2017-f-042 ( 12:20 – 12:40 )
Development of Binary Black Hole Observation Satellite ‘‘ORBIS’’
Jun Matsushima1, Hironori Sahara1, Shogo Asano1, Masahiro Kaku1, Toshihiro Kanda1, Mayu Banno1, Hirohisa Asano1, Yuya Kobayashi1, Natsumi Kimura1, Norio Yamashita1, Yuichiro Ezoe2, Kumi Ishikawa3, Kasumi Nakakamura2, Masaki Numazawa2, Kazuma Takeuchi2, Masaru Terada2, Daiki Ishii2, Yusuke Noda2, Maiko Fujitani2, Naoki Isobe3, Hiroshi Nakajima4, Norihide Miyamura5
1Department of Aerospace Engineering, Tokyo Metropolitan University, Tokyo, Japan, 2Department of Physics, Tokyo Metropolitan University, Tokyo, Japan, 3Institute of Space and Astronautical Sciensce, JAXA, Sagamihara, Japan, 4Department of Earth and Space Science, Osaka University, Osaka, Japan, 5Department of Interdisciplinary Science and Engineering, Meisei University, Tokyo, Japan
[f-10] EQUULEUS
Session Date June 8 (Thu) 14:00 – 15:40
Room Pearl Room A
Chairpersons Alex da Silva Curiel (Surrey Satellite Technology Ltd., UK)
Tetsuya Yamada (ISAS/JAXA, Japan)
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 Campagnola3, Hiroyuki Koizumi1, Yuta Kobayashi4, Taichi Ito2, Takumi Kudo1, Yuki Koshiro1, Shunichiro Nomura1, Akifumi Wachi1, Masashi Tomooka1, Ichiro Yoshikawa5, Hajime Yano2, Shinsuke Abe6, Tatsuaki Hashimoto2, EQUULEUS Project Team 1
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 3Jet Propulsion Laboratory, NASA, California, USA, 4Research and Development Directorate, JAXA, Tsukuba, Japan, 5Department of Complexity Science and Engineering, The University of Tokyo, Kashiwa, Japan, 6Department of Aerospace Engineering, Nihon University, Funabashi, Japan
2017-f-044 ( 14:20 – 14:40 )
Mission Analysis for EQUULEUS and OMOTENASHI
Stefano Campagnola1, Naoya Ozaki2, Javier Hernando-Ayuso3, Kenta Oshima3, Tomohiro Yamaguchi3, Kenshiro Oguri2, Yusuke Ozawa3, Toshinori Ikenaga3, Kota Kakihara2, Shota Takahashi3, Ryu Funase2, Yasuhiro Kawakatsu3, Tatsuaki Hashimoto3
1Jet Propulsion Laboratory, NASA, Pasadena, California. *Work performed as ITYF at JAXA/ISAS, 2Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 3Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
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 Koizumi1,2 , Naoki Takeda2, Keita Nishii2, Masaya Murohara1, Ryu Funase1, Kimiya Komurasaki1
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Graduate School of Frontier Sciences, The University of Tokyo, Tokyo, Japan
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, The 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, Shuhei Matsushita, Akihiro Ishikawa, Ryu Funase
Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan
[f-11] Components
Session Date June 8 (Thu) 14:00 – 15:40
Room Meeting Room 7
Chairpersons Tsutomu Nagatsuma (National Institute of Information and Communications Technology, Japan)
Norihide Miyamura (Meisei University, Japan)
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
1Japanese Aerospace Exploration Agency (JAXA), Japan, 2Nippon Avionics Co., Ltd., Japan, 3Avionics Fukushima Co., Ltd., Japan
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
1Research Institute for Sustainable Humanosphere, Kyoto University, Kyoto, Japan, 2Graduate School of Natural Science and Technology, Kanazawa University, Kanazawa, Japan
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 Ishisaka9, Ayako Matsuoka5, Reiko Nomura5, Tetsuro Ishida7, Yukihiro Takahashi7
1Space Environment Laboratory, NICT, Koganei, Japan, 2Department of Geophysics, Graduate School of Science, Tohoku University, Sendai, Japan, 3Institute of Science and Engineering, Kanazawa University, Kanazawa, Japan, 4Department of Mechanical & Electrical Engineering, Tokuyama College of Technology, Tokuyama, Japan, 5Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 6Graduate School of Science, Kyoto University, Kyoto, Japan, 7Department of Cosmosciences, Graduate School of Science, Hokkaido University, Sapporo, Japan, 8Research Institute for Sustainable Humanosphere, Kyoto University, Kyoto, Japan, 9Department of Information Systems Engineering, Toyama Prefectural University, Toyama, Japan
2017-f-052 ( 15:20 – 15:40 )
First High Resolution High Speed CubeSat of Turkey
A.R Aslan1, A.Y. Ozyıldırım3, M. Suer2, M.E. Bas2, E. Yakut2, M.Ş. Uludağ1, B. Karabulut1, M.D. Aksulum2, E. Erdogan2, S. Türkoğlu1, M. Karataş1, C. Cenik1, O. Sarı3
1 Istanbul Technical University, Space Systems Design and Test Lab, 2Gumush Uzay Ltd., Istanbul, Turkey, 3ASELSAN Co., Ankara, Turkey
[f-12] Lunar & Deep Space Missions
Session Date June 8 (Thu) 16:00 – 17:20
Room Pearl Room A
Chairpersons Sabro Matunaga (Tokyo Institute of Technology, Japan)
Jessie M Kawata (NASA Jet Propulsion Laboratory / Caltech, USA)
2017-f-053 ( 16:00 – 16:20 )
Nano Moon Lander: OMOTENASHI
Tatsuaki Hashimoto1, Tetsuya Yamada1, Junji Kikuchi1,2, Masatsugu Otsuki1, Toshinori Ikenaga2, OMOTENASHI Project Team 1
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2Research and Development Directorate, JAXA, Sagamihara, Japan
2017-f-054 ( 16:20 – 16:40 )
OMOTENASHI Trajectory Analysis and Design: Earth-Moon Transfer Phase
Yusuke Ozawa1, Shota Takahashi2, Javier Hernando-Ayuso1, Stefano Campagnola3, Toshinori Ikenaga4, Tomohiro Yamaguchi4, Bruno V. Sarli5
1The University of Tokyo, Japan, 2Keio University, Japan, 3Jet Propulsion Laboratory, USA, 4Institute of Space and Astronautical Science, JAXA, Japan, 5Catholic University of America, USA
2017-f-055 ( 16:40 – 17:00 )
Development of Crushable Shock Absorption Structure for OMOTENASHI Semi-hard Impact Probes
Tetsuya Yamada1, Hideyuki Tanno2, Tatsuaki Hashimoto1
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2Kakuda Space Center, JAXA, Kakuda, Japan
2017-f-058 ( 17:00 – 17:20 )
Comparative Analysis of Control Moment Gyros and Reaction Wheels for Micro-Class Low Lunar Orbiters
Tushar Sharma, Amin Ali Mody, Arinut Sharma
SRM University, India
[f-13] Thruster
Session Date June 8 (Thu) 16:00 – 17:40
Room Meeting Room 7
Chairpersons Hirokazu Tahara (Osaka Institute of Technology, Japan)
Hiroyuki Koizumi (The University of Tokyo, Japan)
2017-f-059 ( 16:00 – 16:20 )
Qualification Model Development of CubeSat RF Ion Propulsion System “BIT-3”
Michael Tsay, John Frongillo, Jurg Zwahlen, Joshua Model, Carl Barcroft, Charlie Feng
Busek, Co. Inc., Natick, Massachusetts, U.S.A.
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
1The University of Tokyo, Japan, 2Japan Aerospace Exploration Agency (JAXA), Japan
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, Eugene Kim, Xiaofeng Wu
The School of Aerospace, Mechanical, and Mechatronics Engineering, The University of Sydney, 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, Osaka, Japan, 2Department of Aeronautics and Astronautics, Tokai University, Kanagawa, Japan
[f-14] Attitude Determination
Session Date June 9 (Fri) 9:00 – 10:00
Room Pearl Room A
Chairpersons Wu Xiaofeng (University of Sydney, Australia)
Hiroshi Hirayama (Akita University, Japan)
2017-f-065 ( 9:00 – 9:20 )
Pseudo-Linear Kalman Filter for Attitude Estimation of a Spinning Nanosatellite
Osama Khurshid1, Jorma Selkainaho1, Esa Kallio1, Arto Visala1, Halil Ersin Söken2
1Aalto University, Espoo, Finland, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
2017-f-066 ( 9:20 – 9:40 )
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 Gonzalez, Yuji Sakamoto, John Leur Labrador, Kazuya Yoshida, Toshinori Kuwahara
Department of Aerospace Engineering, Tohoku University, Japan
2017-f-068 ( 9:40 – 10:00 )
A Sun Vector Determination with Use of Insufficient Data from Sensors
Dmytro Faizullin, Koju Hiraki, HORYU-IV team, Mengu Cho
Kyushu Institute of Technology, Kitakyushu, Japan
[f-15] Design
Session Date June 9 (Fri) 9:00 – 10:20
Room Meeting Room 1
Chairpersons Sabro Matunaga (Tokyo Institute of Technology, Japan)
Tran Duy Vu Bui (Nanyang Technological University, Singapore)
2017-f-069 ( 9:00 – 9:20 )
Application of Design Structure Matrix (DSM) to Nano-satellite Systems Design and Management
Mohammed Khalil Ibrahim, Yasuyuki Miyazaki
Aerospace Engineering Department, College of Science and Technology Nihon University, Funabashi, Chiba, Japan.
2017-f-070 ( 9:20 – 9:40 )
Systems Engineering Approach to The Wires Harness Process of Microsatellites
Nguyen Duc Manh, Takashi Hiramatsu, Shusaku Yamaura, Makoto Ioki
The 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
Pham Anh Minh, Shusaku Yamaura, Takashi Hiramatsu, Seiko Shirasaka
Graduate School of System Design and Management, Keio University, Japan
2017-f-073 ( 10:00 – 10:20 )
Thermal Design of Micro-satellites Deployed from Japan Experimental Module Small Satellite Orbital Deployer (J-SSOD)
Delburg Mitchao1, Tsuyoshi Totani2, Masashi Wakita2, Harunori Nagata2
1Graduate School of Engineering, Hokkaido University, Hokkaido, Japan, 2Faculty of Engineering, Hokkaido University, Hokkaido, Japan
[f-16] Disturbance and Utilization
Session Date June 9 (Fri) 11:00 – 12:00
Room Pearl Room A
Chairpersons Tatsuaki Hashimoto (Japan Aerospace Exploration Agency, Japan)
Tsuyoshi Totani (Hokkaido University, Japan)
2017-f-074 ( 11:00 – 11:20 )
Observer-based Disturbance Estimation for a Small Satellite Inertial Pointingusing Magnetic Torquers
Jongbum Kim, Hyochoong Bang, Mikaël Marin
Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon, Korea
2017-f-076 ( 11:20 – 11:40 )
Magnetic Torque Caused by Shape Magnetic Anisotropy in Nano-satellites
Takaya Inamori1, Mana Nagao1, Yutaka Terao2, Nobutada Sako3
1Department of Aerospace Engineering, Nagoya University, Nagoya, Japan, 2Department of Advanced Energy, The University of Tokyo, Chiba, Japan, 3Canon Electronics Inc., Tokyo, Japan
2017-f-077 ( 11:40 – 12:00 )
Detailed Analysis of Aerodynamic Effect on Small Satellites
Kikuko Miyata1, Rei Kawashima2, Takaya Inamori1
1Department of Aeronautics and Astronautics, Nagoya University, Tokyo, Japan, 2Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan
[f-17] Test
Session Date June 9 (Fri) 11:00 – 12:40
Room Meeting Room 1
Chairpersons Yuji Sakamoto (Tohoku University, Japan)
Hiroyuki Sugita (JAXA, Japan)
2017-f-078 ( 11:00 – 11:20 )
The Development of Support System for Radiation Resistance Test
Akihiro Nagata1, Atsushi Yasuda2, Hiromasa Watanabe2, Toshihiro Kameda3
1Graduate School of Systems and Information Engineering, University of Tsukuba, Tsukuba, Japan, 2Graduate School of Pure and Applied Sciences, University of Tsukuba, Tsukuba, Japan, 3Faculty of Engineering, Information and Systems, University of Tsukuba, Tsukuba, Japan
2017-f-079 ( 11:20 – 11:40 )
Evaluation of Structural Thermal Model of a Small Spacecraft Using CFRP
Yutaro Ogata, Takumi Iso, Takashi Hiramoto, Masaaki Kawamura
Department of Aerospace Engineering, Faculty of Science and Engineering, Teikyo University, Tochigi, 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
Laboratory of Space Environment Interaction and Engineering, Kyushu Institute of Technology, Kitakyushu, Japan
2017-f-081 ( 12:00 – 12:20 )
Development of Structural Thermal Model of Multipurpose Space Environment Utilization Satellite “TeikyoSat-4”
Takumi Iso, Katsunori Takahashi, Takashi Hiramoto, Masaaki Kawamura
Department of Aerospace Engineering, Teikyo University, Tochigi, Japan
2017-f-082 ( 12:20 – 12:40 )
Design, Development and Testing of Structure and Thermal Subsystem of AOBA-VELOX III
Hirokazu Masui1, Kyutech Students Satellite Project 1, Mengu Cho1, Tran Quang Vinh2
1Laboratory of Spacecraft Interaction Engineering (LaSEINE), Kyushu Institute of Technology, Kitakyushu, Japan, 2Satellite Research Centre, Nanyang Technological University, Singapore
[f-18] Attitude Control
Session Date June 9 (Fri) 14:00 – 15:40
Room Pearl Room A
Chairpersons Takaya Inamori (Nagoya University, Japan)
Yasuhiro Shoji (Osaka University, Japan)
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
1Aerospace Science and Technology Department, Politecnico di Milano, Milan, Italy, 2GP Advanced Projects Srls, Brescia, Italy
2017-f-084 ( 14:20 – 14:40 )
Attitude Control for a Nanosatellite using Only Magnet Torquers
Takashi Kimoto, Katsuhiko Yamada, Yasuhiro Shoji
Department of Mechanical Engineering, Osaka University, Osaka, 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, The University of Manchester, Manchester, United Kingdom
2017-f-086 ( 15:00 – 15:20 )
FDA-A6 – A Fluid-Dynamic Attitude Control System for TechnoSat
Daniel Noack1, Jonathan Ludwig2, Philipp Werner1, Merlin F. Barschke1, Klaus Brieß1
1Institute of Aeronautics and Astronautics, Technische Universität Berlin, Berlin, Germany, 2Magson GmbH, Berlin, Germany
2017-f-087 ( 15:20 – 15:40 )
Dynamics Analysis of Weather-cock like Passive Sun-oriented Control Using Solar Pressure
Hiroki Nakanishi, Ryuhei Takagi, Mitsushige Oda
Dept. of Mechanical engineering, Tokyo Institute of Technology, Tokyo, Japan
[f-19] Operation & Verification
Session Date June 9 (Fri) 14:00 – 15:40
Room Meeting Room 1
Chairpersons Keiichi Hirako (Keio University, Japan)
Hirokazu Masui (Kyushu Institute of Technology, Japan)
2017-f-088 ( 14:00 – 14:20 )
VELOX-II: Summary of One Year in Operation
S.T. Goh1, L.S. Lim1, T.D.V. Bui2, M.S.C. Tissera1, V.H.P. Pham2, R. Abhishek1, J.J. Soon1, J.M. Lew2, H. Aung1, G.X. Lee1, J.W. Chia3, K.W. Chow1, S. Ankit1, L. Deng2, K.S. Low1
1Department of Electrical and Computer Engineering, National University of Singapore, Singapore, 2School of Electrical and Electronic Engineering, Nanyang Technological University, Singapore, 3Space System Engineering, Delft University of Technology, Netherlands
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 Paler1, Toshinori Kuwahara1, Kazuya Yoshida1, Tetsuo Ishida2, Junichi Kurihara2, Yukihiro Takahashi2
1Department of Aerospace Engineering, Tohoku University, Sendai, Japan, 2Department of Cosmosciences, Hokkaido University, Sapporo, Japan
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
The University of Shizuoka, Japan
2017-f-091 ( 15:00 – 15:20 )
Orbit Verification Result of De-orbit Mechanism Demonstration CubeSat FREEDOM
Hiroki Uto1, Toshiyuki Mogi2, Toshinori Kuwahara2
1Nagoya Technical Center, Nakashimada Engineering Works, Ltd., Kasugai, Japan, 2Department of Aerospace engineering, Tohoku University, Sendai, 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 Masahiro Nohmi (Shizuoka University, Japan)
Kikuko Miyata (Nagoya University, Japan)
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 Yatsu4, Saburo Matunaga1
1Department of Mechanical Engineering, School of Engineering, Tokyo Institude of Technology, Tokyo, Japan, 2Department of Mechanical and Aerospace Engineering, Graduate school of Engineering, Tokyo Institude of Technology, Tokyo, Japan, 3Department of Physics, School of Science, Tokyo Institude of Technology, Tokyo, Japan, 4Department of Physics, Graduate school of Science, Tokyo Institude of Technology, Tokyo, Japan
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. Martínez Valdés
Laboratory of Electronic Instrumentation for Space Systems, National Autonomous University of Mexico, Mexico
2017-f-095 ( 16:40 – 17:00 )
Investigation into Star Tracker Algorithms using Smartphones with Application to High-Precision Pointing CubeSats
Joshua Critchley-Marrows, Xiaofeng Wu
School of Aeronautical, Mechanical and Mechatronic Engineering, University of Sydney, 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 Shinichi Kimura (Tokyo University of Science, Japan)
Hsin-Chia Lin (National Space Organization, Taiwan)
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, Sendai, Japan
2017-f-099 ( 16:20 – 16:40 )
Development of an Improved Micro-Satellite Environment Simulator for Attitude Determination and Control System Verification Through DIWATA-1 Flight Data Analysis
John Leur Labrador, Ariston Gonzalez, Yuji Sakamoto, Toshinori Kuwahara, Kazuya Yoshida
Space Robotics Laboratory, Department of Aerospace Engineering, Tohoku University, Sendai, Japan
2017-f-100 ( 16:40 – 17:00 )
Software Development for Galassia CubeSat – Design, Implementation and In-Orbit Validation
Hassan Ali Askari, Ee Wei Han Eugene, Ajie Nayaka Nikicio, Goh Cher Hiang, Luo Sha, Liaw Hwee Choo
Department of 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
[g-1] Space Transportation (1)
Session Date June 7 (Wed) 11:00 – 12:20
Room Meeting Room 7
Chairpersons George Nicholas Coulloupas (RMIT University, Australia)
Satoshi Nonaka (Japan Aerospace Exploration Agency, Japan)
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 Ishigami2, Masaaki Miura2, Kazuyuki Higashino1, Takakage Arai3
1Aerospace Plane Research Center, Muroran Institute of Technology, Muroran, Japan, 2Graduate student, Muroran Institute of Technology, Muroran, Japan, 3Osaka Prefecture University, Sakai, Japan
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 Yamazaki1, Kazuhide Mizobata2, Kazuyuki Higashino2
1Graduate student, Muroran-IT, Japan, 2Aerospace Plane Research Center, Muroran-IT, 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 Mizobata2, Kazuyuki Higashino2, Takakage Arai3
1Graduate student, Muroran Institute of Technology, Hokkaido, Japan, 2Muroran Institute of Technology, Hokkaido, Japan, 3Osaka Prefecture University, Osaka, Japan
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, Muroran, Japan
[g-2] Space Transportation (2)
Session Date June 7 (Wed) 16:00 – 17:00
Room Meeting Room 7
Chairpersons Chit Hong Yam (ispace Inc., Japan)
Shinichiro Tokudome (JAXA, Japan)
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 Launch Vehicle Flight Using Angle of Attack Estimator
Ario Birmiawan Widyoutomo1, Yasuhiro Morita2
1Department of Space and Astronautical Science, The Graduate University for Advanced Studies (SOKENDAI), Sagamihara, Japan, 2Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan
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
1Co-founder of ‘Astronautical Society of Taiwan’, Space Architecture Activist, MEng., 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 Satoshi Nomura (JAXA, Japan)
Taro Tsukamoto (JAXA, Japan)
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 Toba1, Ikkoh Funaki2, Yoshiki Yamagiwa1
1Shizuoka University, Hamamatsu, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
2017-g-12 ( 9:40 – 10:00 )
Evaluation Study on EDL Analysis in Mars Atmosphere Re-entry with High-lift Flexible Vehicle
Mayuri Sakamoto1, Riho Takumi1, Masaaki Kawamura2
1Graduate School of Science &Engineering, Teikyo University, Tochigi, Japan, 2Department of Aerospace Engineering, Teikyo University, Tochigi, Japan
2017-g-13 ( 10:00 – 10:20 )
Initial Study by the EDL Analysis of the “Target Marker” for Guidance in Mars Exploration
Riho Takumi1, Mayuri Sakamoto1, Masaaki Kawamura2
1Graduate School of Science & Engineering, Teikyo University, 2Department of Aerospace Engineering, Teikyo University
2017-g-14 ( 10:20 – 10:40 )
Coplanar Aerocapture Reachable Domain
Hongwei Han1, Dong Qiao1,2, Hongbo Chen3
1School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China, 2Key Laboratory of Autonomous Navigation and Control for Deep Space Exploration, Ministry of Industry and Information Technology, Beijing, China, 3China Academy of Launch Vehicle Technology, Beijing, China
[g-4] Space Transportation (4)
Session Date June 8 (Thu) 11:00 – 12:20
Room Meeting Room 14
Chairpersons Tetsuhiko Kozasa (Mitsubishi Heavy Industries, Ltd., Japan)
Takashi Ozawa (JAXA, Japan)
2017-g-15 ( 11:00 – 11:20 )
Subsystem Development Status of the H3 Launch Vehicle
Hironori Takeda1, Yorichika Mihara1, Keitaro Ishikawa1, Tomoki Furusawa1, Osamu Kitayama1, Akihiro Satoh1, Wataru Sarae2, Hiroyuki Ueda2, Akito Hattori2, Kiyoshi Kobayashi2, Hiroyuki Nagata2
1Mitsubishi Heavy Inductries, Japan, 2Japan Aerospace Exploration Agency, JAXA, Japan
2017-g-16 ( 11:20 – 11:40 )
Hot-fire Testing Plan of LE-9 Development Engine for H3 Launch Vehicle
Tetsuya Fujiwara1, Daiki Watanabe1, Nobuki Negoro1, Takashi Tamura1, Tadaoki Onga1, Hideto Kawashima2, Teiu Kobayashi2, Koichi Okita2
1Mitsubishi Heavy Industries, LTD. Komaki, Japan, 2Japan Aerospace Exploration Agency, Tsukuba, Japan
2017-g-17 ( 11:40 – 12:00 )
Subscale Combustion Testing of Additive Manufacturing Injector
Akane Nagasaki1, Daiki Watanabe1, Takashi Tamura1, Tadaoki Onga1, Akira Ogawara1, Norio Higuchi2, Hitoshi Sakai2, Yoshio Nunome3, Hideto Kawashima3
1Mitsubishi Heavy Industries, LTD. Komaki, Japan, 2NTT Data Engineering Systems Corporation, Mino, Japan, 3Japan Aerospace Exploration Agency, Tsukuba, Japan
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, Research and Development Directorate, JAXA, Sagamihara, Japan, 2Range Technology Development Unit, Space Technology Directorate I, JAXA, Tsukuba, Japan
[g-5] Space Transportation (5)
Session Date June 8 (Thu) 14:00 – 15:40
Room Meeting Room 14
Chairpersons Seiji Tsutsumi (JAXA, Japan)
Toshiyuki Suzuki (Japan Aerospace Exploration Agency, Japan)
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, Sendai, Japan, 2Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 3Department of Mechanical Engineering, Keio University, Yokohama, Japan, 4Research and Development Directorate, Japan Aerospace Exploration Agency, Kakuda, Japan
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, Tokyo, Japan, 2Department of Advanced Energy, The University of Tokyo, Tokyo, Japan
2017-g-21 ( 14:40 – 15:00 )
A Numerical and Experimental Approaches on Aerodynamic Characteristics of Waverider with Orbiter
Tomoki Uzaki1, Tomoyuki Muta1, Nobuyuki Tsuboi1, Yusuke Maru2, Kazuhisa Fujita3
1Kyushu Institute of Technology, Kitakyushu, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 3Aerospace Research and Development Directorate, JAXA, Tsukuba, Japan
2017-g-22 ( 15:00 – 15:20 )
Numerical Analysis of Aerodynamic Characteristics on Reusable Sounding Rocket
Yoshiki Nishikawa1, Nobuyuki Tsuboi1, Takashi Ito2, Satoshi Nonaka2
1Kyushu Institute of Technology, Kitakyushu, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
2017-g-23 ( 15:20 – 15:40 )
Numerical Simulation Accompanied with Shock Stand-o Prediction for Heat-flux Mitigation by MHD Flow Control on Re-entry Vehicles
P P Upadhyay, R Tietz, G Herdrich
Institute of Space Systems,University of Stuttgart,Baden W¨urttemberg, Germany
[h-1] Combustion
Session Date June 8 (Thu) 16:00 – 17:20
Room Meeting Room 14
Chairpersons Osamu Moriue (Kyushu University, Japan)
Takehiko Ishikawa (Japan Aerospace Exploration Agency, Japan)
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, Gifu, 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
1Graduate School of Sciences and Technology for Innovation, Yamaguchi University, Yamaguchi, Japan, 2Graduate School of Science and Engineering, Yamaguchi University, Yamaguchi, Japan
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, Yoshinari Kobayashi, Hiroaki Iida, Shinji Nakaya, Mitsuhiro Tsue
Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan
[h-2] Fundamental Physics / Short Term Microgravity
Session Date June 9 (Fri) 9:40 – 10:40
Room Meeting Room 14
Chairpersons Yuko Inatomi (JAXA, Japan)
Takehiko Ishikawa (Japan Aerospace Exploration Agency, Japan)
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
1Faculty of Pharmacy, Chiba Institute of Science, Chiba, Japan, 2Faculty of Science and Technology, Tokyo University of Science, Chiba, Japan, 3Institute of Space and Astronautical Science, JAXA, Tsukuba, Japan
2017-h-08 ( 10:00 – 10:20 )
Unmanned Aerial Vehicle Appliance in Microgravity Research
Tomas Pupinis1, Domantas Brucas1,2, Matas Razgunas2,3, Marcello Valdatta4
1Antanas Gustaitis’ Aviation Institute, Vilnius Gediminas Technical University, Vilnius, Lithuania, 2Space Science and Technology Institute, Vilnius, Lithuania, 3Vilnius University, Vilnius, Lithuania, 4University of Bologna, Bologna, Italy
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 Atsumi, Marina Tsutsumi, Ayaka Nakajima, Yuko Watanabe
Tokyo University of Science, Japan
[h-3] Levitation-1
Session Date June 9 (Fri) 11:20 – 12:40
Room Meeting Room 14
Chairpersons Masahito Watanabe (Gakushuin University, Japan)
Paul-Francois Paradis (INO, Canada)
2017-h-11 ( 11:20 – 11:40 )
Thermophysical and Structural Study of Levitated Droplets using Electrostatic Levitation and Scattering Devices
Geun Woo Lee1,2
1Frontier in Extreme Physics, Korea Research Institute of Standards and Science, Korea, 2Department of Nano Science, University of Science and Technology, Korea
2017-h-12 ( 11:40 – 12:00 )
Thermophysical Property of Supercooled-liquid Silicon
Junpei T. Okada1, Takehiko Ishikawa2, Paul-Francois Paradis3, Yuki Watanabe4, Satoshi Uda1
1Institute for Materials Science, Tohoku University, Sendai, Japan, 2Institute of Space and Astronautical Science, JAXA, Tsukuba, Japan, 3INO, Quebec, Canada, 4A.E.S. Co. Ltd., Tsukuba, Japan
2017-h-13 ( 12:00 – 12:20 )
Multiple Pathways of Crystal Nucleation in an Extremely Supersaturated Aqueous Potassium Dihydrogen Phosphate (KDP) Solution Droplet
Sooheyong Lee1,2, Haeng Sub Wi1, Wonhyuk Jo1,3, Yong Chan Cho1, Hyun Hwi Lee4, Se-Young Jeong5, Geun Woo Lee1,2
1Frontier in Extreme Physics, Korea Research Institute of Standards and Science, Daejeon, Republic of Korea, 2Department of Nano Science, University of Science and Technology, Daejeon, Republic of Korea, 3Department of Physics, Soongsil University, Seoul, Republic of Korea, 4Pohang Accelerator Laboratory, Pohang, Republic of Korea, 5Department of Cogno-Mechatronics Engineering, Pusan National University, Miryang, Republic of Korea
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-François Paradis1, Takehiko Ishikawa2, Won-Kyu Rhim3, Junpei T. Okada4
1INO, Quebec City, Quebec, Canada, 2JAXA, Tsukuba, Ibaraki, Japan, 3Caltech, Pasadena, CA, United States, 4Tohoku University, Sendai, Miyagi, Japan
[h-4] Levitation-2
Session Date June 9 (Fri) 14:00 – 15:40
Room Meeting Room 14
Chairpersons Geun Woo Lee (Korea Research Institute of Standards and Science, Korea)
Junpei Okada (Tohoku University, Japan)
2017-h-15 ( 14:00 – 14:20 )
Status and Prospects of Electrostatic Levitation Furnace (ELF) Experiment in ISS-KIBO
Haruka Tamaru1, Chihiro Koyama1, Hideki Saruwatari1, Yasuhiro Nakamura1, Takehiko Ishikawa2, Tetsuya Takada3
1Human Spaceflight Technology Directorate, JAXA, Tsukuba, Japan, 2Institute of Space and Astronautical Science, JAXA, Tsukuba, Japan, 3Space Systems Department, IHI Aerospace Co., Ltd., Tomioka, Japan
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, Haruka Tamaru4, Takehiko Ishikawa4
1Department of Physics, Gakushuin University, Tokyo, Japan, 2Graduate school of Engineering, Osaka University, Suita, Japan, 3Graduate school of Engineering, Tohoku University, Sendai, Japan, 4Japan Aerospace Exploration Agency(JAXA), Tsukuba, Japan
2017-h-17 ( 14:40 – 15:00 )
Thermophysical Properties Measurements of Liquid Alloys under Oxygen Influence in ISS (OXYTHERM Project)
Masahito Watanabe1, Shumpei Ozawa2, Jürgen Brillo3
1Department of Physics, Gakushuin University, Tokyo, Japan, 2Department of Materials Science and Engineering, Chiba Institute of Technology, Narashino, Japan, 3Institute of Materials Physics in Space, German Aerospace Center, Köln, Germany
2017-h-18 ( 15:00 – 15:20 )
Thermophysical Properties of Zr-O liquid Alloys Measured by Electrostatic Levitation
Yuji Ohishi1, Toshiki Kondo1, Takehiko Ishikawa2,3, Junpei T. Okada4, Yuki Watanabe5, Hiroaki Muta1, Ken Kurosaki1, Shinsuke Yamanaka1,6
1Graduate School of Engineering, Osaka University, Suita, Osaka, Japan, 2Japan Aerospace Exploration Agency, Tsukuba, Ibaraki, Japan, 3SOKEN-DAI (Graduate University for Advanced Studies), Sagamihara, Kanagawa, Japan, 4Institute for Materials Research, Tohoku University, Sendai, Miyagi, Japan, 5Advanced Engineering Services Co. Ltd., Tsukuba, Ibaraki, Japan, 6Research Institute of Nuclear Engineering, University of Fukui, Tsuruga, Fukui, Japan
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, JAXA, Tsukuba, Japan, 2INO, Quebec, Canada, 3A.E.S. Co. Ltd., Tsukuba, Japan., 4Tohoku University, Sendai, Japan.
[h-5] Levitation-3 /Researches using the ISS
Session Date June 9 (Fri) 16:00 – 17:20
Room Meeting Room 14
Chairpersons Satoshi Matsumoto (Japan Aerospace Exploration Agency, Japan)
Takehiko Ishikawa (Japan Aerospace Exploration Agency, Japan)
2017-h-20 ( 16:00 – 16:20 )
Contactless Coalescence of Acoustically Levitated Droplets under Reduced Gravity Conditions
Ayumu Watanabe1, Motonori Niwa1, Kenji Kobayashi1, Tomohisa Yuasa1, Koji Hasegawa2, Satoshi Matsumoto3, Akiko Kaneko1, Yutaka Abe1
1University of Tsukuba, Japan, 2Kogakuin University, Japan, 3JAXA, Japan
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 Fluids
Taishi Yano1, Koichi Nishino1, Satoshi Matsumoto2, Ichiro Ueno3, Atsuki Komiya4, Yasuhiro Kamotani5, Nobuyuki Imaishi6
1Department of Mechanical Engineering, Yokohama National University, Yokohama, Japan, 2Human Spaceflight Technology Directorate, JAXA, Tsukuba, Japan, 3Department of Mechanical Engineering, Faculty of Science &Technology, Tokyo University of Science, Noda, Japan, 4Institute of Fluid Science, Tohoku University, Sendai, Japan, 5Department of Mechanical and Aerospace Engineering, Case Western Reserve University, Cleveland, USA, 6Kyushu University, Ichihara, 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
1Human Spaceflight Technology Directorate, JAXA, Tsukuba, Japan, 2Department of Aeronautics and Astronautics, Kyushu University, Fukuoka, Japan, 3Department of Mechanical Engineering, Kobe University, Kobe, Japan, 4Department of Mechanical Engineering, University of Hyogo, Himeji, Japan, 5Course of Aerospace Engineering, Muroran Institute of Technology, Muroran, Japan
2017-h-23 ( 17:00 – 17:20 )
Summary of ALLOY SEMICONDUCTOR Project
Yuko Inatomi1,2,3, Nirmal Kumar Velu3, Mukannan Arivanandhan3, Takuya Yamamoto4, Xin Jin4, Haryo Mirsandi4, Yasunori Okano4,3,1, Yasuhiro Hayakawa3, Takehiko Ishikawa1,2
1Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan, 2School of Physical Sciences, SOKENDAI, Japan, 3Research Institute of Electronics, Shizuoka University, Japan, 4Department of Materials Engineering Science, Osaka University, Osaka, Japan
2017-h-24 ( 17:20 – 17:40 )
The Development of Hardware for the Atomization Experiment in Microgravity on Kibo
Tatsuya Taguchi1, Yasuhiro Nakamura1, Masao Kikuchi1, Satoshi Matsumoto1, Satoshi Yukizono2, Hidetoshi Nakagami3, Wataru Ono3
1JAXA, Japan, 2Jupitor Corporation, Japan, 3Chiyoda Corporation, Japan
[i-1] Advanced Theraml Control Device
Session Date June 9 (Fri) 9:00 – 10:20
Room Meeting Room 7
Chairpersons Hosei Nagano (Nagoya University, Japan)
Hiroki Nagai (Tohoku University, Japan)
2017-i-01 ( 9:00 – 9:20 )
Numerical Investigation of MEMS-based Black Body System using the Thermoelectric Device
Bong-Geon Chae, Tae-Gyu Kim, Hyun-Ung Oh
Department of Aerospace Engineering, Chosun University, Republic of 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, Nagoya, Japan, 2Department of Mechanical Engineering, Nagoya University, Nagoya, Japan, 3Research and Development Directorate, JAXA, Tsukuba, Japan
2017-i-03 ( 9:40 – 10:00 )
Characteristics of Thermophysical Properties Through Metal-insulation for Future Advanced Thermal Control Device
Jihoon Kim1, Daeil Park1, Hosei Nagano1, Sumitaka Tachikawa2
1Nagoya University, Nagoya, Aichi, Japan, 2Institute of Space and Astronautical Science, Kanagawa, Japan
2017-i-08 ( 10:00 – 10:20 )
Multi-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, Glasgow, UK, 2Sophrodyne Ltd Science and Engineering Research Studio, Glasgow, UK
[i-2] Thermal Control System
Session Date June 9 (Fri) 11:00 – 12:00
Room Meeting Room 7
Chairpersons Hosei Nagano (Nagoya University, Japan)
Hiroki Nagai (Tohoku University, Japan)
2017-i-02 ( 11:00 – 11:20 )
Numerical Investigation of TransientBehavior of Loop Heat Pipes
Takuya Adachi, Hiroki Nagai2
1Department of Aerospace Engineering, Tohoku University, Miyagi, Japan, 2Institute of Fluid and Science, Tohoku University, Miyagi Japan
2017-i-07 ( 11:20 – 11:40 )
Design of Two-Phase Mechanically Pumped Fluid Loop with Large Isothermal Evaporator using Porous Wick Structure
Kenichi Sakamoto1, Takuya Adachi1, Takurou Daimaru1, Hiroki Nagai1, Eric Sunada2, Pradeep Bhandari2, Benjamin Furst2, Stefano Cappucci3
1Institute of Fluid Science, Tohoku University, Sendai, Japan, 2Propulsion, Thermal and Materials Engineering Section, Jet Propulsion Laboratory/California Institute of Technology, Pasadena, America, 3Aerospace Engineering, Polytechnic University of Turin, Turin, Italy
2017-i-11 ( 11:40 – 12:00 )
A Multi-nodes Model for the Thermal Performance of Stratospheric Airship
Qiang Liu, Yanchu Yang, Taihua Zhang, Jingjing Cai, Yanxiang Cui
Academy of Opto-Electronics, Chinese Academy of Sciences, Beijing, China
[i-3] Theraml Design for Future Spacecraft
Session Date June 9 (Fri) 14:00 – 15:00
Room Meeting Room 7
Chairpersons Hosei Nagano (Nagoya University, Japan)
Hiroki Nagai (Tohoku University, Japan)
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
1Institute of Fluid Science, Tohoku University, Sendai, Japan, 2JAXA, Tsukuba, Japan 3)Waseda University,Tokyo, Japan
2017-i-10 ( 14:20 – 14:40 )
Thermal based Path Planning using Solar Orientation for a Lunar Micro Rover
Hugo 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 Kato1, Makiko Ando1, Yasuhiro Fukuzoe2
1Research and Development Directorate, JAXA, Tsukuba, Japan, 2Space Technology Directorate I, JAXA, Kumage, Japan
[j-1] Antennas and Stations
Session Date June 6 (Tue) 16:00 – 17:40
Room Meeting Room 15
Chairpersons Tetsushi Ikegami (Meiji University, Japan)
Amane Miura (NICT, Japan)
2017-j-01 ( 16:00 – 16:20 )
New Receiving Ground Antenna for Satellites using Active Phased Array Antenna
Nobuyuki Kaya, Rie Nakayama
Kobe University, Japan; WaveArrays, Inc, Japan
2017-j-02 ( 16:20 – 16:40 )
Precise Beam Formation Control for Mobile Communication Satellite Based on Onboard Measurement of Large Reflector Surface Shape
Maki Akioka1, Amane Miura1, Teruaki Orikasa1, Hiroyuki Tsuji1, Morio Toyoshima1, Masaki Satoh2, Yoshiyuki Fujino1
1Wireless Network Research Center, National Institute of Information and Communications Technology, Koganei, Tokyo, Japan, 2Kashima Space Technology Center, Wireless Network Research Center, National Institute of Information and Communications Technology, Kashima, Ibaraki, 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 Satoh, Amane Miura, Teruaki Orikasa, Maki Akioka
National Institute of Information and Communications Technology, Tokyo, Japan
2017-j-04 ( 17:00 – 17:20 )
Signal Level Fluctuation Caused by Cable Wrapping System of Usuda Deep Space Center
Tomoaki Toda, Koji Yuchi, Takashi Uchimura, Kenji Numata
Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
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
Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
[j-2] Hardware Implimentation and Broadcasting
Session Date June 7 (Wed) 9:00 – 10:40
Room Meeting Room 14
Chairpersons Yoshiyuki Fujino (National Institute of Information and Communications Technology, Japan)
Masanobu Yajima (Japan Aerospace Exploration Agency, Japan)
2017-j-06 ( 9:00 – 9:20 )
High Power High Efficient Compact GaN Amplifier for the Solid-state Radar
Daisuke Hayashi1,2, Ryoko Kishikawa2, Shigeo Kawasaki2,3
1Koden Electronics Co., Ltd., Tokyo, Japan, 2SOKENDAI (The Graduate University for Advanced Studies), Sagamihara, Japan, 3Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan
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, JAXA, Ibaraki, Japan
2017-j-08 ( 9:40 – 10:00 )
100W C-band GaN Solid State Power Amplifier with 50% PAE for Satellite Use
M. Kido, S. Kawasaki, A. Shibuya, K. Yamada, T. Ogasawara, T. Suzuki, S. Tamura, K. Seino, A. Ichikawa, A. Tsuchiko
Space Systems & Electronic Engineering Department, Mitsubishi Electric TOKKI Systems Corporation, Kanagawa, Japan
2017-j-09 ( 10:00 – 10:20 )
Experimental Verification of Prototype Equalizer for Non-linear Compensation over Satellite Channel
Masaaki Kojima, Masafumi Nagasaka, Yoichi Suzuki, Yuki Koizumi, Koichi Saito, Shoji Tanaka
NHK Science & Technology Research Laboratories,Tokyo, Japan
2017-j-10 ( 10:20 – 10:40 )
Hardware Performance of Optical Distribution Equipment for 12-GHz Band Satellite Broadcasting using Dual-polarization
Atsushi Iwasaki1, Masafumi Nagasaka1, Yuki Koizumi1, Masaaki Kojima1, Susumu Nakazawa1, Shoji Tanaka1, Kazuya Ueda2
1Science & Technology Research Laboratories, Japan Broadcasting Corporation, Tokyo, Japan, 2Association of Radio Industries and Businesses, Tokyo, Japan
[j-3] WINDS and Next Systems
Session Date June 7 (Wed) 11:00 – 12:40
Room Meeting Room 14
Chairpersons Masaaki Kojima (NHK Science & Technology Research laboratories, Japan)
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
National Institute of Information and Communications Technology, Koganei, Tokyo, 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, JAXA, Tsukuba, Japan, 2Space Engineering Development Co., Ltd, Tsukuba, Japan
2017-j-13 ( 11:40 – 12:00 )
High-Speed Transmission for Ka-Band Aeronautical Satellite Communications Using WINDS
Tomoshige Kan, Takashi Takahashi, Noihiko Katayama, Toshio Asai, Kazuyoshi Kawsaki, Maki Akioka, Morio Toyoshima
Space Communications Laboratory, National Institute of Information and Communications Technology, Ibaraki, Japan
2017-j-14 ( 12:00 – 12:20 )
Conceptual Design for Next Engineering Test Satellite
Kentaro Nishi1, Kunitoshi Nishijo2, Satoru Ozawa1, Tadahiko Sano2, Yasushi Hatooka2, Tsutomu Fukatsu2
1Research and Development Directorate, JAXA, Tsukuba, Japan, 2Space Technology Directorate I, JAXA, Tsukuba, 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 Yamamoto1, Takashi Takahashi1, Kazuyoshi Kawasaki1, Tomoshige Kan1, Shinichi Kozono1, Toshihiro Kubooka1, Testuharu Fuse1, Hiroo Kunimori1, Yoshisada Koyama1, Yasushi Munemasa1, Hideki Takenaka1, Kolev Dimitar1, Alberto Carrasco-Casado1, Morio Toyoshima1, Kazuma Kaneko2, Hiroki Nishiyama2, Nei Kato2, Eiichi Sakai3, Terumi Sunaga3, Nobuyoshi Horie3, Arimasa Kanasashi3, Toshiyasu Tsunoda3, Yuichi Yamamoto3, Yoshifumi Goto3, Toshihiko Hayashi3, Katsumi Tsukahara3, Hisayuki Mukae3
1NICT, Tokyo, Japan, 2Tohoku University, Miyagi, Japan, 3Mitsubishi Electric Corp., Tokyo, Japan
[j-4] Navigation and Applications
Session Date June 7 (Wed) 16:00 – 17:40
Room Meeting Room 14
Chairpersons Mitsugu Ohkawa (National Institute of Information and Communications Technology, Japan)
Yoshiyuki Fujino (National Institute of Information and Communications Technology, Japan)
2017-j-16 ( 16:00 – 16:20 )
Precision Navigation Achieved by ASTRO-H Space-borne GPS Receiver
Yu Nakajima1, Toru Yamamoto1, Koji Yamanaka1, Yoshinori Kondoh2, Kyohei Akiyama3, Mina Ogawa4, Susumu Kumagai5, Satoko Kawakami5, Masaru Kasahara5
1Research and Development Directorate, JAXA, Tsukuba, Japan, 2Human Spaceflight Technology Directorate, JAXA, Tsukuba, Japan, 3Space Tracking and Communications Center, JAXA, Tsukuba, Japan, 4Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 5Space Engineering Division, NEC Space Technologies, Ltd., Fuchu, Japan
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
Keio University, Yokohama, Japan
2017-j-18 ( 16:40 – 17:00 )
Stochastic Constellation Replenishment Planner
Federico Letterio1, Gonzalo Vicario1, Javier Martin1, Mauro Federici2, Daniel Navarro-Reyes3
1Deimos Space S.L.U., Spain, 2Deimos Space U.K., United Kingdom, 3ESA
2017-j-19 ( 17:00 – 17:20 )
Environmental-data Collection System for Satellite-to-Ground Optical Communications
Kenji Suzuki, Dimitar Kolev, Alberto Carrasco-Casado, Morio Toyoshima
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 Shinichi Kimura (Tokyo University of Science, Japan)
Kenji Suzuki (NICT, Japan)
2017-j-21 ( 9:00 – 9:20 )
Updates on the Design and Implementation of the Philippines’ Diwata-2 Amateur Radio Payload
Mary Ann Constante1, Izrael Zenar Bautista1, Edgar Paolo Violan1, Lorenzo Sabug, Jr.1, Leonard Bryan Paet1,2, Janette Salvatus1, Gladys Bajaro1, Adrian Salces1, Marc Caesar Talampas1, Joel Joseph Marciano, Jr.1,3
1College of Engineering, University of the Philippines, Diliman, Quezon City, Philippines, 2Department of Aerospace Engineering, Tohoku University, Sendai, Japan, 3Advanced Science and Technology Institute, Department of Science and Technology, Quezon City, Philippines
2017-j-22 ( 9:20 – 9:40 )
Self-Powered Beacon Development for Satellite Communication Loss Prevention
Rahmi Rahmatillah, Mengu Cho
Laboratory of Spacecraft Environment Interaction Engineering, Kyushu Institute of Technology, Kitakyushu, 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, Koji Kumura1, Toshiki Nakamura1, Motoharu Taketsu1, Tomonori Ito2, Shin Satori1,2
1Department of Future Industry, Happy Science University, Chiba 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 Kawasaki1, Toshinori Kuwahara1, Masafumi Hiraoka1, Toshiyuki Mogi1, Daichi Morita1, Shota Suzuki1, Kazushi Fukuda1, Shinya Fujita1, Yuji Sato1, Lena Okajima2
1Department of Aerospace Engineering, Tohoku University, Sendai, Japan, 2ALE Co., Ltd., Tokyo, 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 Hiraoka1, Toshinori Kuwahara1, Yuji Sato1, Shinya Fujita1, Shunsuke Kawasaki1, Daichi Morita1, Toshiyuki Mogi1, Shouta Suzuki1, Lena Okajima2
1Department of Aerospace Engineering, Tohoku University, Sendai, Japan, 2ALE Co., Ltd., Tokyo, Japan
[k-1] ISS and Near Earth Missions
Session Date June 6 (Tue) 16:00 – 17:40
Room Meeting Room 8
Chairpersons Igor V. Sorokin (S.P. Korolev Rocket and Space Corporation Energia, Russia)
Hajime Yano (JAXA/ISAS, Japan)
2017-k-01 ( 16:00 – 16:20 )
Technology of Payloads Maintenance aboard the ISS Russian Segment
Igor V. Sorokin
S.P. Korolev Rocket and Space Corporation Energia (RSC Energia), Korolev, Moscow Region, 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 (ISAC) Team 1#
1JAXA/Institute of Space and Astronautical Science, 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
1Department of Physics, Chiba University, Chiba, Japan, 2Institute of Space and Astronautical Science (ISAS), JAXA, Sagamihara, Japan, 3Institute for Advanced Biosciences, Keio University, Tsuruoka, Japan, 4Department of Bioengineering, Nagaoka University of Technology, Nagaoka, Japan, 5Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology, Koganei, Japan, 6Department of Earth and Planetary Sciences, Kyushu University, Fukuoka, Japan, 7Department of Applied Life Sciences, Tokyo University of Pharmacy and Life Sciences, Hachioji, Japan, 8Department of Chemistry, Chemical Engineering and Life Science, Yokohama National University, Yokohama, Japan, 9Department of Life, Environment and Materials Science, Fukuoka Institute of Technology, Fukuoka, Japan, 10Office for Planning and Management, University of Aizu, Aizu-Wakamatsu, Japan, 11School of Health Sciences, Tokyo University of Technology, Tokyo, Japan
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 Imai8
1Tokyo University of Pharmacy and Life Sciences,Tokyo, Japan, 2ISAS/JAXA, Sagamihara, Japan, 3Yokohama National University, Yokohama, Japan, 4Fukuoka Institute of Technology,Fukuoka, Japan, 5Osaka University, Osaka, Japan, 6JAXA, Tokyo, Japan, 7Chiba University,Chiba, Japan, 8Nagaoka University of Technology, Nagaoka, Japan
2017-k-05 ( 17:20 – 17:40 )
Experimental Verification Strategy for Navigation Involving Contact Dynamics under Microgravity
Hiroki Kato, Daichi Hirano, Tatsuhiko Saito, Mari Nishiyama, Ippei Takahashi
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan
[k-2] Small Bodies and Dust Explorations (1)
Session Date June 7 (Wed) 9:00 – 10:40
Room Meeting Room 8
Chairpersons Massimo Casasco (European Space Agency, Netherlands)
Tatsuaki Okada (Japan Aerospace Exploration Agency, Japan)
2017-k-06 ( 9:00 – 9:20 )
In-Flight Performance of Thermal Infrared Imager on Hayabusa2 and Its Implications to the Observations of Asteroid 162173 Ryugu
Tatsuaki Okada1,2, Tetsuya Fukuhara3, Satoshi Tanaka1, Makoto Taguchi3, Takehiko Arai4, Hiroki Senshu5, Hirohide Demura6, Yoshiko Ogawa6, Toru Kouyama7, Ryosuke Nakamura7, Naoya Sakatani8, Jun Takita2, Tomohiko Sekiguchi9, Sunao Hasegawa1, Tsuneo Matsunaga4, Takeshi Imamura2, Takehiko Wada1, Jorn Helbert10, Thomas G. Mueller11, Axel Hagarmann12, Solar Power Sail Science Team 1
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2The University of Tokyo, Hongo, Bunkyo, Tokyo, Japan, 3Graduate School of Science, Rikkyo University, Tokyo, Japan,, 4National Institute for Environmental Studies, Tsukuba, Japan, 5Planetary Exploration Research Center, Chiba Institute of Technology, Narashino, Japan, 6University of Aizu, Aizu-Wakamatsu, Japan, 7National Institute of Advanced Industrial Science and Technology, Tokyo, Japan, 8Graduate School of Science and Technology, Meiji University, Kawasaki, Japan, 9Hokkaido University of Education, Asahikawa, Japan, 10German Aerospace Center, Berlin, Germany, 11Max-Planck Institute for Extraterrestrial Physics, Garching, Germany, 12The Open University, Milton Keynes, UK
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, Tokyo, Japan, 2École Polytechnique, Paris, France
2017-k-08 ( 9:40 – 10:00 )
Estimation of Interior Density Distribution for Small Bodies:The Case of Asteroid Itokawa
Masanori Kanamaru, Sho Sasaki
Department of Earth and Space Science, Osaka University, Osaka, 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, The University of Tokyo, 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 Gil Fernandez3, Paolo Martino2
1European Space Agency Headquarters, Paris, France, 2European Space Astronomy Centre, Madrid, Spain, 3European Space Technology Centre, Noordwijk, The Netherlands
[k-3] Small Bodies and Dust Explorations (2)
Session Date June 7 (Wed) 11:00 – 12:35
Room Meeting Room 8
Chairpersons Shinsuke Abe (Nihon University, Japan)
Kazutaka Nishiyama (Japan Aerospace Exploration Agency, Japan)
2017-k-11 ( 11:00 – 11:15 )
Numerical Estimation of Gamma-ray Spectroscopy for Deep Space Microsatellite
Masayuki Naito1, Junya Ishii1, Daisuke Aoki1, Hiroshi Nagaoka2, Eido Shibamura2, Nobuyuki Hasebe1,2
1School of Advanced Science and Engineering, Waseda University, Tokyo, Japan, 2Research Institute for Science and Engineering, Waseda University, Tokyo, Japan
2017-k-12 ( 11:15 – 11:30 )
Neutron Spectroscopy for Exploration of Near-Earth Asteroids
Junya Ishii1, Masayuki Naito1, Daisuke Aoki1, Hiroshi Nagaoka2, Nobuyuki Hasebe1,2
1School of Advanced Science and Engineering, Waseda University, Tokyo, Japan, 2Research Institute for Science and Engineering, Waseda University, Tokyo, 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, Tokyo, 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, DESTINY Working Group 1
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 3Planetary Exploration Research Center, Chiba Inst. of Technology, Japan
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
1Department of Aerospace Engineering, Nihon University, Funabashi, Japan, 2Swedish Institute of Space Physics, Kiruna, Sweden, 3National Institute of Polar Research, Tachikawa, Japan, 4National Astronomical Observatory of Japan, Mitaka, Japan, 5Research Institute for Sustainable Humanosphere, Kyoto University, Uji, 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 Osamu Mori (Japan Aerospace Exploration Agency, Japan)
Takahiro Iwata (Japan Aerospace Exploration Agency, Japan)
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, Toshihiro Chujo1, 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, Kazuhiro Yamada1, Tatsuaki Okada1, Takahiro Iwata1, Ralf Boden1, Yusuke Oki1, Yuki Takao2
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan
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
1Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Kanagawa, Japan, 2Department of Advanced Sciences, Hosei University, Tokyo, Japan, 3Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 4Graduate School of Science and Engineering, Aoyama Gakuin University, Kanagawa, Japan, 5Department of Physics, Osaka University, Osaka, Japan
2017-k-19 ( 16:40 – 17:00 )
Two Motors Drive Rotary Sample Conveyance Mechanism
Shuya Kashioka1, Masatsugu Otsuki2, Jun Matsumoto2, Jun Aoki3, Osamu Mori2
1The Graduate University for Advanced Studies, Japan, 2The Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 3Osaka University
2017-k-20 ( 17:00 – 17:20 )
Science and Instrumentation for Exploring a Jupiter Trojan Asteroid in the Solar Power Sail Mission
Tatsuaki Okada1,2, Yoko Kebukawa3, Jun Aoki4, Motoo Ito5, Masatsugu Ohtsuki1, Chisato Okamoto6, Yusuke Oki2, Jun Matsumoto1, Hajime Yano1, Ryosuke Nakamura7, Takahiro Iwata1, Osamu Mori1, Jean-Pierre Bibring8, Stephan Ulamec9, Solar Power Sail Science Team 1
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2The University of Tokyo, Hongo, Bunkyo, Tokyo, Japan, 3Faculty of Engineering, Yokohama National University, Japan, 4Graduate School of Science, Osaka University, Toyonaka, Japan, 5Kochi Core Center, Japan Agency for Marine-Earth Science and Technology, Japan, 6Faculty of Science and Engineering, Hosei University, Tokyo, Japan, 7National Institute of Advanced Industrial Science and Technology, Tokyo, Japan, 8Institut dʼAstrophysique Spatiale, Orsay, France, 9German Aerospace Center, Cologne, Germany
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, Tatehiro Mihara6, Tatsuaki Okada1, Jun Matsumoto1, Osamu Mori1
1The Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2Kwansei Gakuin University, Sanda, Japan, 3Tohoku University, Sendai, Japan, 4Japan Aerospace Exploration Agency, Mitaka, Japan, 5Kanazawa University, Kanazawa, Japan, 6Institute of Physical and Chemical Research (RIKEN), Wako, Japan
[k-5] Mercurial and Lunar Explorations
Session Date June 8 (Thu) 9:00 – 10:00
Room Meeting Room 8
Chairpersons Roger Wilson (Airbus DS GmbH, Germany)
Tatsuaki Hashimoto (Japan Aerospace Exploration Agency, Japan)
2017-k-22 ( 9:00 – 9:20 )
The BepiColombo Spacecraft and its Mission to Mercury
Roger J. Wilson, Markus Schelkle
Airbus Defence and Space, Friedrichshafen, Germany
2017-k-23 ( 9:20 – 9:40 )
Japanese Lunar Polar Exploration Lander
Tatsuaki Hashimoto1,2, Takeshi Hoshino2, Hisashi Otake1,2, Satoshi Tanaka1, Sachiko Wakabayashi2, Hitoshi Morimoto2, Koichi Masuda2, Makiko Ohtake1, Masataku Sutoh3, Takanobu Shimada2
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2Space Exploration Innovation Hub Center, JAXA, Sagamihara, Japan, 3Faculty of Textile Science and Technology, Shinshu University, Ueda, Japan
2017-k-24 ( 9:40 – 10:00 )
Skid Traveling System to Travel on Planetary Surface
Hikaru Eguchi1, Yusuke Maru1,2, Masatsugu Otsuki2, Shunpei Morikawa3, Shujiro Sawai1,2
1Department of Space and Astronautical Science, The Graduate University for Advanced Studies, Kanagawa, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 3Department of Engineering, Shizuoka University, Shizuoka, Japan
[k-6] Lunar Science and Utilization
Session Date June 8 (Thu) 11:00 – 12:40
Room Meeting Room 8
Chairpersons Kyeong Ja Kim (Korea Institute of Geoscience and Mineral Resources, Korea)
Hiroshi Nagaoka (Waseda University, Japan)
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 Hasebe1,2, Masayuki Naito2, Eido Shibamura1, Haruyoshi Kuno1, Miho Mizone2, Yoshiki Nabekura2, Kyeong Ja Kim3
1Research Institute for Science and Engineering, Waseda University, Japan, 2Schools of Advanced Science and Engineering, Waseda University, Japan, 3KIGAM, South Korea
2017-k-28 ( 11:20 – 11:40 )
Current Development Status of a Gamma-Ray Spectrometer for the Korea Pathfinder Lunar Orbiter
Kyeong Ja Kim1,2, Yire Choi1,2, Junghun Park1, Eung Seok Yi1,3, Sungsoon Lee1, Yeongwang Yeon1, Chang Wan Sun1,2, K.B. Lee4, Yongkwon 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
1Korea Institute of Geoscience and Mineral Resources, Daejeon, Republic of Korea, 2University of Science and Technology, Daejeon, Republic of Korea, 3Chungnam National University, Daejeon, Republic of Korea, 4Korea Research Institute of Standards and Science, Daejeon, Republic of Korea, 5Nucare, Incheon, Republic of Korea, 6Korea Advanced Institute of Science and Technology, Daejeon, Republic of Korea, 7Inha University, Incheon, Republic of Korea, 8Waseda University, Tokyo, Japan, 9NASA Ames Research Center, Moffett Field, CA, USA, 10Quest University, Squamish, BC, Canada, 11IRAP, Toulouse, France, 12NASA Goddard Space Flight Center, Greenbelt, MD, USA
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 Hoshoda1, Sachiko Wakabayashi1
1Japan Aerospace Exploration Agency, Japan, 2MORUTARU MAGIC Co., Ltd., Japan
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., Japan
[k-7] Technologies for Lunar and Planetary Explorations (1) – Landing
Session Date June 8 (Thu) 14:00 – 15:40
Room Meeting Room 8
Chairpersons Marcus Lobbia (NASA Jet Propulsion Laboratory, USA)
Kazuhisa Fujita (Japan Aerospace Exploration Agency, Japan)
2017-k-32 ( 14:00 – 14:20 )
Planetary Image Recognition using Deep Learning
Hiya Roy1, Tatsuaki Hashimoto1,2
1The University of Tokyo, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
2017-k-33 ( 14:20 – 14:40 )
Supersonic Retro-Propulsion for Future High-Mass Robotic Mars Lander Missions
Marcus Lobbia, Aron Wolf, Charles Whetsel
NASA Jet Propulsion Laboratory, California Institute of Technology, USA
2017-k-34 ( 14:40 – 15:00 )
Hazard Avoidance Control Using Stochastic Optimization for Mars Safe Landing
Ryohei Takahashi, Akifumi Wachi, Ryu Funase, Shinichi Nakasuka
The 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, Naomi Takizawa1, Seiya Ueno2, Takehiro Higuchi2, Toshiki Tamura2, Ryuki Otani2, Hiroaki Kobayashi1, Nobutaka Bando1
1Japan Aerospace Exploration Agency, Tokyo, Japan, 2Yokohama National University, Yokohama, Japan
2017-k-36 ( 15:20 – 15:40 )
Planetary Exploration Spacecraft Landing Gear with Three-Dimensional Linear-Rotary-Energy-Conversion Mechanism
Susumu Hara1, Satoshi Saito1, Keisuke Sugita1, Takao Maeda2
1Department of Aerospace Engineering, Nagoya University, Nagoya, Japan, 2Department of Electrical, Electronic, and Communication Engineering, Chuo University, Tokyo, Japan
[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 Hiya Roy (The University of Tokyo, Japan)
Hiroyuki Kawamoto (Waseda University, Japan)
2017-k-37 ( 16:00 – 16:20 )
Capability of a Time-of-Flight Camera as a Hazard Detection and Avoidance Sensor for a Moon Exploration Microrover
Kentaro Uno1, Louis-Jerome Burtz2, Marc Hulcelle3, Kazuya Yoshida1
1Department of Aerospace Engineering, Tohoku University, Sendai, Japan, 2KK ispace Inc., Tokyo, Japan, 3Ecole des Mines de Saint-Etienne, France
2017-k-38 ( 16:20 – 16:40 )
Dynamic Locomotion of a Multi-Legged Planetary Exploration Rover with Isotropic Leg Arrangement
Tomohito Sekiguchi1, Saki Omi2, Mai Bando1, Shinji Hokamoto1
1Kyushu University, Japan, 2Cranfield University, UK
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, Tokyo, 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 Hiroki Nagai (Tohoku University, Japan)
Akira Oyama (Japan Aerospace Exploration Agency, Japan)
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 Miyazaki1, 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, Sagamihara, Japan, 2Institute of Fluid Science, Tohoku University, Sendai, Japan, 3Kanazawa University, Kanazawa, Japan, 4Kyushu University, Japan, 5Kyushu Institute of Technology, Japan, 6Kanazawa Institute of Technology, Japan, 7Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan, currently Tohoku University, Japan, 8Aeronautical Technology Directorate, Japan Aerospace Exploration Agency, Japan, 9Tohoku University, Japan, 10Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Japan, currently Tokyo University of Science, Japan
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
1Interdisciplinary Graduate School of Engineering Sciences, Kyushu University, Kasuga, Japan, 2Department of Aeronautics, Kanazawa Institute of Technology, Tokyo, Japan, 3Institute of Space Astronautical Science, JAXA, Sagamihara, Japan, 4Institute of Fluid Science, Tohoku University, Sendai, Japan
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
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2Kanazawa University, Kanazawa, Japan, 3Institute of Fluid Science, Tohoku University, Sendai, Japan
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, Japan, 3Institute of Fluid Science, Tohoku University, Japan
2017-k-46 ( 10:20 – 10:40 )
Comparison of Thermal Analysis and Flight Test Results on Mars Airplane Balloon Experiment-1 (MABE-1)
Yasuyuki Oda1, Takurou Daimaru1, Hiroki Nagai1, Koji Fujita2, Akira Oyama2
1Institute of Fluid Science, Tohoku University, Sendai, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
[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 Huai-Chien Chang (Consortium of Extreme and Space Settlements, Astronautical Society of Taiwan, Taiwan)
Kojiro Suzuki (The University of Tokyo, Japan)
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, Kashiwa, Japan
2017-k-48 ( 11:20 – 11:40 )
Space Weathering Simulation with Sulfur
Sho Sasaki1, Hirokazu Tanaka1, Yasunori Kanamaru1, Mizuki Okazaki1,4, Takahiro Hiroi2, Akira Miyake3, Tohru Matsumoto3, Akira Tsuchiyama3
1Department of Earth and Space Science, Osaka University, Toyonaka, Japan, 2Department of Earth, Environmental and Planetary Sciences, Brown University, Providence, USA, 3Department of Earth and Planetary Sciences, Kyoto University, Kyoto, Japan, 4Now at Benesse Corp., Japan
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 Fujita2, Tomohiro Usui10
1Tokyo University of Pharmacy and Life Science, Tokyo, Japan, 2JAXA, Sagamihara, Japan, 3Tamagawa University, Tokyo, Japan, 4Tokyo University of Technology, Tokyo, Japan, 5Yokohama National University, Yokohama, Japan, 6Hiroshima University, Hiroshima, Japan, 7Fukuoka Institute of Technology, Fukuoka, Japan, 8Nagaoka University of Technology, Nagaoka, Japan, 9Hiroshima University, Hiroshima, Japan, 10Tokyo Institute of Technology, Tokyo, 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
1Co-founder of ‘Astronautical Society of Taiwan’, Space Architecture Activist, MEng., Taiwan, 2Research Assistant, Geomatics Laboratory of National Taipei University of Technology, Taiwan
[k-11] Explorations for Mars and its Moons
Session Date June 9 (Fri) 14:00 – 15:35
Room Meeting Room 8
Chairpersons Michael G. Wilson (Jet Propulsion Laboratory / California Institute of Technology, USA)
Yasuhiro Kawakatsu (JAXA, Japan)
2017-k-52 ( 14:00 – 14:20 )
Martian Moons eXploration (MMX) Conceptual Study Results
Yasuhiro Kawakatsu1, Kiyoshi Kuramoto2, Masaki Fujimoto1
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2Department of Earth and Planetary Sciences, School of Science, Hokkaido University, Sapporo, Japan
2017-k-53 ( 14:20 – 14:35 )
Development of Near-infrared Spectrometer MacrOmega for the Martian Moon’s Sample Return Mission MMX
Takeshi Sakanoi1, Takahiro Iwata2, Hiromu Nakagawa1, Jean-Pierre Bibring3, Vincent Hamm3, Cedric Pilorget3, Tomoki Nakamura4, Shohei Aoki5, Takao M. Sato2, Yasumasa Kasaba1
1Department of Geophysics, Tohoku University, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 3Institut d’Astrophysique Spatiale, Université Paris-Sud, France, 4Department of Earth Science, Tohoku University, Japan, 5Institut d’Aéronomie Spatiale de Belgique (IASB), Bruxelles, Belgium
2017-k-54 ( 14:35 – 14:50 )
Nuclear Spectroscopy for Unveiling the Origin of the Martian Moons
Nobuyuki Hasebe1,2, Hiroshi Nagaoka2, Masayuki Naito1, Eido Shibamura2, Haruyoshi Kuno2, Sota Shimizu2,3, Kyeong Ja Kim4, Valery V. Dmitrenko5, Tomoki Nakamura6, Hisashi Otake7
1Department of Physics, School of Advanced Science and Engineering, Waseda University, Japan, 2Research Institute for Science and Engineering, Waseda University, Japan, 3Graduate School of Science and Technology, Keio University, Japan, 4Planetary Geology Department, Geological Research Division, Korean Institute of Geoscience and Mineral Resources, Republic of Korea, 5National Research Nuclear University, Moscow Engineering Physics Institute (MEPhI), Russia, 6Division of Earth and Planetary Materials Scinece, Tohoku University, Japan, 7Japan Aerospace Exploration Agency (JAXA), Japan
2017-k-55 ( 14:50 – 15:05 )
An Ion Mass Spectrometer for Observation of Secondary Ions from Small Bodies
Shoichiro Yokota1, Ayako Matsuoka1, Reiko Nomura2, Yoshifumi Saito1
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2Tsukuba space center, JAXA, Tsukuba, Japan
2017-k-56 ( 15:05 – 15:20 )
NASA Mars 2020 Landed Mission Development
Michael Wilson, Jennifer Trosper, Fernando Abilleira
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 Hauke Hussmann (DLR Institute of Planetary Research, Germany)
Alex da Silva Curiel (Surrey Satellite Technology Ltd., UK)
2017-k-58 ( 16:00 – 16:20 )
Experiment SIGNAL Onboard the Interhelioprobe Spacecraft
Valery V. Dmitrenko1, Sergey E. Ulin1, Nobuyuki Hasebe2,3
1National Research Nuclear University, Moscow Engineering Physics Institute (MEPhI), Moscow, Russia, 2Department of Physics, School of Advanced Science and Engineering, Waseda University, Tokyo, Japan, 3Research Institute for Science and Engineering, Waseda University, Tokyo, Japan
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
1Co-founder of ‘Astronautical Society of Taiwan’, Space Architecture Activist, MEng., Taiwan, 2Research Assistant, Geomatics Laboratory of National Taiwan University of Technology, Taiwan
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, Chiba, Japan, 5IAA-CSIC Granada, Spain, 6National Astronomcal Observatory of Japan (NAOJ), 7Physikalisches Institut, University 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, Cavan Cuddy3
1NASA Jet Propulsion Laboratory, California Institute of Technology, USA, 2NASA Goddard Space Flight Center, USA, 3Lockheed Martin Space Systems, USA
2017-k-62 ( 17:20 – 17:40 )
Twinkle – A New Idea for a Commercial Astrophysics Mission
Alex da Silva Curiel1, Susan Jason1, Marcell Tessenyi2, Giovanna Tinetti2, Giorgio Savini2, Jonathan Tennyson2, Enzo Pascale3, Sean Lindsay4, Neil Bowles4
1Surrey Satellite Technology Ltd., United Kingdom, 2Blue Skies Space Ltd. & University College London, United Kingdom, 3Sapienza Università di Roma, Italy, 4Department of Physics, University of Oxford, United Kingdom
[m-1] Astrophysics using Balloon and Sounding Rocket
Session Date June 9 (Fri) 9:00 – 10:40
Room Meeting Room 12
Chairpersons Yidong Gu (Chinse Academy of Sciences, China)
Shigeto Watanabe (Hokkaido Information University, Japan)
2017-m-01 ( 9:00 – 9:20 )
GRAINE Project : Analysis Status of Balloon Experiment in 2015
Fukashi Mizutani1, Shigeki Aoki1, Kaname Hamada3, Toshio Hara2, Atsushi Iyono5, Hiroaki Kawahara4, Koichi Kodama6, Ryosuke Komatani4, Masahiro Komatsu4, Kenji Kuretsubo1, Toshitugu Marushima1, Haruka Matsumoto1, Motoaki Miyanishi4, Kunihiro Morishima4, Misaki Morishita4, Naotaka Naganawa4, Mitsuhiro Nakamura4, Toshiyuki Nakano4, Akira Nishio4, Kimio Niwa4, Naoto Otsuka4, Keita Ozaki1, Hiroki Rokujo4, Osamu Sato4, Emi Shibayama1, Atsumu Suzuki2, Satoru Takahashi1, Yurie Tateishi1, Misato Yabu1, Kyohei Yamada1, Saya Yamamoto5, Masahiro Yoshimoto4
1Department of Human Development, Kobe University, Kobe, Japan, 2Department of Science, Kobe University, Kobe, Japan, 3Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 4Department of Science, Nagoya University, Nagoya, Japan, 5Department of Science, Okayama University of Science, Okayama, Japan, 6Aichi University of Education, Kariya, Japan
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
1Graduate School of Science, Kyoto University, Kyoto, Japan, 2New Industry Creation Hatchery Center, Tohoku University, Sendai, Japan
2017-m-03 ( 9:40 – 10:00 )
PoGO+ Stratospheric Balloon Mission from Esrange, Sweden, to Victoria Island, Canada
Mattias Abrahamsson1, Christian Lockowandt2
1Science Services Division, SSC, Esrange Space Center, Sweden, 2Science Services Division, SSC, Solna, Sweden
2017-m-04 ( 10:00 – 10:20 )
Cryogenic 32 × 32 CTIA Multiplexer for Far-Infrared Astronomy
Shunsuke Baba1,2, Koichi Nagase2, Takehiko Wada2, Hirokazu Ikeda2, Yasuo Arai3, Morifumi Ohno4, Takahiro Ishimaru2
1Department of Physics, The University of Tokyo, Tokyo, Japan, 2Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan, 3High Energy Accelerator Research Organization (KEK), Tsukuba, Japan, 4National Institute of Advanced Industrial Science and Technology (AIST), Tsukuba, Japan
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, Itsuki Sakon2, Tomoya Yamazaki1, Kyoko K. Tanaka1, Shinsuke Takeuchi3, Yuko Inatomi3,4
1Institute of Low Temperature Science, Hokkaido University, Hokkaido, Sapporo, Japan, 2Department of Astronomy, School of Science, University of Tokyo, Tokyo, Japan, 3Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, Japan, 4School of Physical Sciences, SOKENDAI (The Graduate University for Advanced Studies), Sagamihara, Kanagawa, Japan
[m-2] Engineering of Scientific Balloon and Sounding Rocket System
Session Date June 9 (Fri) 11:00 – 12:20
Room Meeting Room 12
Chairpersons Mattias Abrahamsson (Swedish Space Corporation, Sweden)
Daisuke Akita (Tokyo Institute of Technology, Japan)
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
1National Institute of Technology, Oita College, Oita, Japan, 2College of Science, Rikkyo University, Tokyo, Japan, 3Graduate School of Engineering, Osaka University, Suita, Japan, 4Graduate School of Science, Hokkaido University, Sapporo, Japan, 5Graduate School of Science, Okayama University of Science, Okayama, Japan, 6Graduate School of Engineering, Tohoku University, Sendai, Japan
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, Suita, Japan
2017-m-09 ( 12:00 – 12:20 )
Post Flight Analysis of Sounding Rocket S-310
Takayuki Yamamoto, Satoshi Nonaka, Shunsuke Sato, Nobuaki Ishii
Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
[m-3] Atmospheric Science using Sounding Rocket
Session Date June 9 (Fri) 14:00 – 15:00
Room Meeting Room 12
Chairpersons Yuki Kimura (Hokkaido University, Japan)
Masa-yuki Yamamoto (Kochi University of Technology, Japan)
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 Yamamoto2
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2Hokkaido Information University, Ebetsu, Japan, 3Research Institute for Sustainable Humanosphere, Kyoto University, Uji, Japan, 4Kochi University of Technology, Kochi, Japan
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 Yoshikwa5, Hiroki Matsushita5
1Toyama Prefectural University, Toyama, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 3Tohoku University, Sendai, Japan, 4Tokai University, Kanagawa, Japan, 5Kyushu University, Fukuoka, Japan
2017-m-13 ( 14:40 – 15:00 )
Neutral Wind Measurements by Sounding Rockets
S. Watanabe1, T. Abe2, H. Habu2, Y. Kakinami3, M-Y. Yamamoto4
1Hokkaido Information University / Hokkaido University, Japan, 2JAXA/ISAS, Japan, 3National Institute of Technology, Tomakomai College, Japan, 4Kochi University of Engineering, Japan
[m-4] Next Gerenartion Balloon and Payload System
Session Date June 9 (Fri) 16:00 – 17:40
Room Meeting Room 12
Chairpersons Yasuhiro Shoji (Osaka University, Japan)
Yanchu Yang (Chinese Academy of Science, China)
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
School of Systems Engineering, Kochi University of Technology, Kami, Kochi, 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 Mitsuhashi2, Kazuhisa Chiba3, Tomonori Ito4
1 Happy Science University, 2Hokkaido University of Science, 3The University of Electro-Communications, 4Hokkaido Satellite Co., Ltd.
2017-m-16 ( 16:40 – 17:00 )
Study of Designing for Combined Shape Balloon in Stratosphere
Yanchu Yang, Sheng Wang, Luhua Jiang, Jinggang Miao, Donghui Zhang
Academy of Opto-Electronics, Chinese Academy of Science, Beijing, China
2017-m-17 ( 17:00 – 17:20 )
Design and Ground Test of a 6 Meters Pumpkin Super-pressure Balloon
Zhu Rongchen1,2, Wang Sheng1, Yang Yanchu1, Liu Qiang1
1Academy of Opti-electronics, Chinese Academy of Sciences, Beijing, China, 2University of Chinese Academy of Sciences, Beijing, 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, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 3Department of Aeronautics and Astronautics, Tokai University, Kanagawa, Japan, 4Department of Mechanical Engineering, Meiji University, Kanagawa, Japan, 5Fujikura Parachute Company Ltd, Fukushima, Japan, 6Nakada Industrial Company, Shizuoka, Japan
[n-1] Earth Observation: Advances in Operations and Data Application
Session Date June 7 (Wed) 16:00 – 17:40
Room Meeting Room 15
Chairpersons Akihiko Kuze (Japan Aerospace Exploration Agency, Japan)
Tamotsu Igarashi (Remote Sensing Technology Center of Japan, Japan)
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
1R.O.C. Naval Academy, Kaohsiung, Taiwan (R.O.C.), 2National Defense University, Taoyuan, Taiwan (R.O.C.), 3National Space Organization (NSPO), HsinChu, Taiwan (R.O.C.)
2017-n-02 ( 16:20 – 16:40 )
Heuristic Algorithm for Simultaneous Nadir Overpasses Estimation during Metop-A End of Life Phase
Carlos Vera1, Pier-Luigi Righetti2
1Telespazio VEGA Deutschland at EUMETSAT, Darmstadt, Germany, 2EUMETSAT, Darmstadt, Germany
2017-n-03 ( 16:40 – 17:00 )
A Graph-Theoretic Approach to Optimal Planning of Satellite Downlink Operation
Kazunori Someya1, Takuto Ishimatsu2, Yosuke Nakamura3, Yuya Kakehashi3, Naoki Ishihama1
1Research and Development Directorate, Research Unit III, JAXA, Tsukuba, Japan, 2The University of Tokyo, Tokyo, Japan, 3ERG project Team, JAXA, Sagamihara, Japan
2017-n-04 ( 17:00 – 17:20 )
The Importance of Earth Observations and Data Collaboration within Environmental Intelligence Supporting Arctic Research
Joseph Casas
NASA Marshall Space Flight Center, Huntsville, Alabama, 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, Kuan-Tsung Chang3, Yi Chang4, Takeo Tadono5, Kei Oyoshi5, Hiroki Kai6, Yusuke Kobayashi6, Tamotsu Igarashi6
1Shibaura Institute of Technology, Tokyo, Japan, 2National Taiwan Ocean University, Keelung, Taiwan, 3Minghsin University of Science and Technology, Hsinchu, Taiwan, 4National Cheng- Kung University, Tainan, Taiwan, 5Japan Aerospace Exploration Agency (JAXA), Ibaraki, Japan, 6Remote Sensing Technology Center of Japan (RESTEC), Tokyo, Japan
[n-2] Earth Observation: Advances in Optical Imagers and Radiometers (1)
Session Date June 8 (Thu) 9:20 – 10:40
Room Meeting Room 11
Chairpersons Haruyoshi Katayama (Japan Aerospace Exploration Agency, Japan)
Kei Shiomi (Japan Aerospace Exploration Agency, Japan)
2017-n-06 ( 9:20 – 9:40 )
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, Chiba, Japan, 2Think Earth Science, Tokyo, Japan
2017-n-07 ( 9:40 – 10:00 )
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
Satellite Business Division, PASCO CORPORATION, Tokyo, Japan
2017-n-09 ( 10:00 – 10:20 )
SLATS and Future Prospect -New Viewpoints for Earth Observation-
Hirokazu Hoshino, Yutaka Kaneko, Masanori Sasaki
Space Technology Directorate I, JAXA, Tsukuba, Japan
2017-n-10 ( 10:20 – 10:40 )
On-board Satellite Imagery Classification using Convolutional Neural Network
Kei Ohta1, Takehiko Koike1, Yoichi Yatsu2, Saburo Matunaga3
1Department of Mechanical and Aerospace Engineering, Tokyo Institute of Technology, Tokyo, Japan, 2School of Engineering Department of Mechanical Engineering, Tokyo Institude of Technology , Tokyo, Japan, 3School of Science Department of Physics, Tokyo Institude of Technology, Tokyo, Japan
[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 Tamotsu Igarashi (Remote Sensing Technology Center of Japan, Japan)
Keiji Imaoka (Yamaguchi University, Japan)
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, Tokyo, Japan, 2Canon Electronics Inc., Tokyo, Japan
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
Advanced Optical Satellite Project Team, JAXA, Tsukuba, 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 Keiji Imaoka (Yamaguchi University, Japan)
Takeo Tadono (JAXA, Japan)
2017-n-16 ( 14:00 – 14:20 )
Simulated Image Generation for the Advanced Optical Satellite
Takeo Tadono, Ayano Oka, Hidenori Watarai, Masakazu Sagihara
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 and Environmental Science, College of Humanities and Sciences, Nihon University, Tokyo, Japan, 2Department of Civil Engineering, College of Science and Technology, Nihon University, Tokyo, Japan
2017-n-18 ( 14:40 – 15:00 )
Mission Planning and System Design for HISA: A Hyperspectral Imaging Satellite for Australia
Eugene Kim, Xiaofeng Wu, Warwick Holmes
School of Aerospace, Mechanical and 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
1Earth Observation Research Center (EORC), JAXA, Tsukuba, Japan, 2Center for Environmental Remote Sensing, Chiba University, Chiba, Japan, 3Nagasaki University, Nagasaki, Japan, 4Department of Environmental Geochemical Cycle Research, JAMSTEC, Yokohama, Japan, 5The University of Tsukuba, Tsukuba, Japan
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 Toratani5, Toru Hirawake6, Teruo Aoki7,8
1Earth Observation Research Center, JAXA, Tsukuba, Japan, 2Center for Environmental Remote Sensing, Chiba University, Chiba, Japan, 3Graduate School of Life and Environmental Science, The University of Tsukuba, Tsukuba, Japan, 4Department of Human and Information Science, Tokai University, Hiratsuka, Japan, 5Department of Optical and Imaging Science and Technology, Tokai University, Hiratsuka, Japan, 6Graduate School of Fisheries Sciences, Hokkaido University, Hakodate, Japan, 7Graduate School of Natural Science and Technology, Okayama University, Okayama, Japan, 8Climate Research Department, Meteorological Research Institute, Tsukuba, Japan
[n-5] Earth Observation: Advances in SARs and Compact Cameras
Session Date June 8 (Thu) 16:00 – 17:40
Room Meeting Room 11
Chairpersons Takeo Tadono (JAXA, Japan)
Haruyoshi Katayama (Japan Aerospace Exploration Agency, Japan)
2017-n-21 ( 16:00 – 16:20 )
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, JAXA, Tsukuba, Japan, 2Space Technology Directorate I, JAXA, Tsukuba, Japan
2017-n-22 ( 16:20 – 16:40 )
Application Demonstration through System and Algorithm Development for Wildfire Monitoring Utilizing CIRC (Compact Infrared Camera)
Koji Nakau
Satellite Applications and Operations Center(SAOC), JAXA, Tsukuba, 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 Shimada2,1, Takashi Ogawa3, Keiko Ishii3, Tomohiko Higashiuwatoko3, Mari Miura4, Hiroaki Okonogi4, Kanako Adachi4, Kenichi Shishido4
1Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan, 2Tokyo Denki University, Hatoyama, Japan, 3Remote Sensing Technology Center of Japan (RESTEC), Tokyo, Japan, 4Japan International Cooperation Agency (JICA), Tokyo, Japan
2017-n-24 ( 17:00 – 17:20 )
ALOS/PALSAR Analysis of Surface Deformation in Chiba Prefecture, Japan
Tomohito Asaka1, Takashi Nonaka1, Hideki Hashiba2, Keishi Iwashita1, Toshiro Sugimura1
1 College of Industrial Technology, Nihon University, Japan, 2College of Science and Technology, Nihon University, Japan
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, Tsukuba, Japan
[n-6] Earth Observation: Advances in Meteorological Instruments
Session Date June 9 (Fri) 9:00 – 10:40
Room Meeting Room 11
Chairpersons Masahiro Hori (Japan Aerospace Exploration Agency, Japan)
Takuji Kubota (Japan Aerospace Exploration Agency, Japan)
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 Nio1, Takuji Kubota1, Riko Oki1, Toshio Iguchi2
1Space Technology Directorate I, JAXA, Tsukuba, Ibaraki, Japan, 2National Institute of Information and Communications Technology, Koganei, Tokyo, Japan
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 N. Takayabu2, Riko Oki1
1Earth Observation Research Center, JAXA, Tsukuba, Japan, 2Atmosphere and Ocean Research Institute, The University of Tokyo, Kashiwa, Japan
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, Tsukuba, Ibaraki, Japan, 2Remote Sensing Technology Center of Japan, Tsukuba, Ibaraki, Japan.
2017-n-29 ( 10:00 – 10:20 )
JAXA Himawari Monitor and its Synergies to the Earth Observation Satellites
Misako Kachi1, Maki Kikuchi1, Mayumi Yoshida1, Takashi Nagao1, Yukio Kurihara2, Hiroshi Murakami1, Masahiro Hori1
1Japan Aerospace Exploration Agency, Tsukuba, Japan, 2Japan Meteorological 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, Chiba, Japan
[n-7] Earth Observation: Advances in Microwave Radiometers
Session Date June 9 (Fri) 11:00 – 12:20
Room Meeting Room 11
Chairpersons Takuji Kubota (Japan Aerospace Exploration Agency, Japan)
Masahiro Hori (Japan Aerospace Exploration Agency, Japan)
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, Nodoka Ono1, Taikan Oki1,2
1Japan Aerospace Exploration Agency, Tsukuba, Japan, 2The University of Tokyo, Japan
2017-n-32 ( 11:20 – 11:40 )
Precipitable Water Vapor Retrieval over Land from GCOM-W/AMSR2
Masahiro Kazumori
Numerical Prediction Division, Forecast Department, JMA, Tokyo, Japan
2017-n-33 ( 11:40 – 12:00 )
Current Status of the AMSR2 Standard Product for Soil Moisture Content and Snow Depth
Hiroyuki Tsutsui, Misako Kachi, Takeshi Maeda
Earth Observation Research Center, JAXA, Tsukuba, 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, Ube, Japan, 2Earth Observation Research Center, JAXA, Tsukuba, Japan
[n-8] Earth Observation: Advances in Spectrometers and Lidars (1)
Session Date June 9 (Fri) 14:00 – 15:40
Room Meeting Room 11
Chairpersons Kei Shiomi (Japan Aerospace Exploration Agency, Japan)
Akihiko Kuze (Japan Aerospace Exploration Agency, Japan)
2017-n-36 ( 14:00 – 14:20 )
The Overview and Status of Vegetation Lidar Mission ‘MOLI’
Rei Mitsuhashi1, Jumpei Murooka1, Daisuke Sakaizawa1, Tadashi Imai1, Toshiyoshi Kimura1, Kazuhiro Asai2
1JAXA, Japan, 2Tohoku Institute of Technology, Japan
2017-n-37 ( 14:20 – 14:40 )
Imaging Spectrometer with an Agile Pointing System to Monitor Global and Regional Greenhouse Gas Fluxes and Target Local Emission
Akihiko Kuze, Hiroshi Suto
JAXA, Sagamihara, 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, Tsukuba, Japan, 2AIST Tokyo Waterfront, Tokyo, Japan
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, Laura Iraci4, Emma Yates4, Warren Gore4, Tomoaki Tanaka4
1Japan Aerospace Exploration Agency, Tsukuba, Japan, 2Remote Sensing Technology Center of Japan, Tsukuba, Japan, 3University of Wisconsin, Madison, USA, 4NASA Ames Research Center, Moffett Field, USA
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 Yoshida1, Nobuo Kenmochi1, Hiroshi Sugita1, Yoshifumi Nodomi1, Shingo Obara2, Akira Sasaki2, Akihiko Kuze2
1NEC Corporation, Fuchu, Tokyo, Japan, 2Japan Aerospace Exploration Agency, Tsukuba, Ibaraki, 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 Kei Shiomi (Japan Aerospace Exploration Agency, Japan)
Akihiko Kuze (Japan Aerospace Exploration Agency, Japan)
2017-n-41 ( 16:00 – 16:20 )
Characterizing On-orbit Electrical Performance of TANSO Onboard GOSAT using its Engineering Model in the Laboratory
Hiroshi Suto1, Jun Yoshida2, Takahiro Kawashima2, Kei Siomi1, Akihiko Kuze1
1Japan Aerospace Exploration Agency, Tsukuba, Ibaraki, Japan, 2NEC Corporation, Fuchu, Tokyo, Japan
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
1JAXA, Tsukuba, Ibaraki, Japan, 2RESTEC, Tsukuba, Ibaraki, Japan
[p-1] Space Life Science (1)
Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 12
Chairpersons Kunihiko Tanaka (Gifu University of Medical Science, Japan)
Masayuki Omoto (University of Kurume, Japan)
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, Gifu, Japan, 2Department of Radiological Technology, Gifu University of Medical Science, Gifu, Japan
2017-p-02 ( 9:25 – 9:50 )
Oxygen Uptake and Muscle Strength is Improved by Electrical Stimulation of the Antagonist Muscle Added to Cycling Exercise Interval Training
Masayuki Omoto1, Ryuuki Hashida1, Yoshio Takano2, Hiroo Matsuse1, Masafumi Bekki1, Yoshihiko Tagawa1, Naoto Siba1
1Division of Rehabilitation, Kurume University Hospital, Kurume, Japan, 2Department of Physical Therapy School of Health Sciences at Fukuoka, International University Health and Welfare, Enokizu, Okawa, Japan
2017-p-03 ( 9:50 – 10:15 )
Trial of the Stress-related Index Measurement under the Confinement Environmental Stress
Yuichi Oi1, Yasuhito Hirai1, Shotaro Doki2, Yuh Ohtaki3, Daisuke Hori4, Christina-Sylvia Andrea3, Shin-Ichiro Sasahara1, Tamaki Saito1, Ichiyo Matsuzaki1,5
1Faculty of medicine, University of Tsukuba, Tsukuba, Japan, 2Hospital Bando, Bando, Japan, 3Graduate School of Comprehensive Human Sciences, University of Tsukuba, Tsukuba, Japan, 4Department of Environmental and Preventive Medicine, Kanazawa University Graduate School of Medical Science, Kanazawa, Japan, 5International Institute for Integrative Sleep Medicine, University of Tsukuba, Tsukuba, Japan
2017-p-04 ( 10:15 – 10:40 )
Development of Mouse Habitat Unit for Individual Housing Used in International Space Station
Hiroyasu Mizuno1, Yusuke Hagiwara2, Hirochika Murase2, Hiroaki Kodama2, Makoto Ohira2, Toshimasa Ochiai2
1Human Spaceflight Technology Directorate, JAXA, Tsukuba, Japan, 2Space Systems Department, Mitsubishi Heavy Industries, Ltd., Nagoya, Japan
[p-2] Space Life Science (2)
Session Date June 6 (Tue) 11:00 – 12:15
Room Meeting Room 12
Chairpersons Koichi Makimura (Teikyo University, Japan)
Takashi Sugita (Meji Pharmaceutical University, Japan)
2017-p-06 ( 11:00 – 11:25 )
Medical Mycology in Space
Koichi Makimura1,2,3
1General Medical Education and Research Center, 2Graduate School of Medicine, Teikyo University, Tokyo, Japan, 3Teikyo University Institute of Medical Mycology, Tokyo, 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 Staying the ISS –
Takashi Sugita1, Ayumi Watanabe1, Otomi Cho1, Noriaki Ishioka2
1Meiji Pharmaceutical University, Tokyo, Japan, 2JAXA, Tokyo, Japan
2017-p-08 ( 11:50 – 12:15 )
Bacterial Horizontal Gene Transfer Frequencies under Simulated Microgravity
Tomoaki Ichijo1, Takehiko Kenzaka2, Masao Nasu1,2, Katsuji Tani2
1Graduate School of Pharmaceutical Sciences, Osaka University, Suita, Japan, 2Faculty of Pharmacy, Osaka Ohtani University, Tondabayashi, Japan
[p-3] Space Life Science (3)
Session Date June 6 (Tue) 14:00 – 15:40
Room Meeting Room 12
Chairpersons Akihisa Takahashi (Gunma University Heavy Ion Medical Center, Japan)
Jun Hidema (Tohoku University, Japan)
2017-p-09 ( 14:00 – 14:25 )
Performance Evaluation of New Devices to Synchronize Heavy-Ion or X-ray Irradiation and Simulated Microgravity for Space Radiation Research~ Improvement of a Control Stage ~
Akihisa Takahashi1, Hiroko Ikeda2, Hikaru Souda1, Anggraeini Puspitasari2, Kathryn D. Held2,3, Jun Hidema4, Takeshi Nikawa5, Yukari Yoshida1, Tatsuaki Kanai1
1Gunma University Heavy Ion Medical Center, Maebashi, Japan, 2Gunma University Initiative for Advanced Research, Maebashi, Japan, 3Massachusetts General Hospital/Harvard Medical School, Boston, USA, 4Graduate School of Life Sciences, Tohoku University, Sendai, Japan, 5Institute of Medical Nutrition, Tokushima University Graduate School, Tokushima, Japan
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, Japan
2017-p-11 ( 14:50 – 15:15 )
Stress-Induced Mitochondrial Fragmentation Impaired Movement inC. elegans
Kenta Momma, Surabhi Sudevan, Rui Isaka, Atsushi Higashitani
Graduate School of Life Sciences, Tohoku University, Sendai, Japan
2017-p-12 ( 15:15 – 15:40 )
Gravity-induced Re-localization of CsPIN1 for Gravimorphogenesis in Cucumber Seedlings
Chiaki Yamazaki1,5, Nobuharu Fujii1, Yutaka Miyazawa2, Motoshi Kamada3, Haruo Kasahara4, Ikuko Osada4, Toru Shimazu5,6, Yasuo Fusejima5, Akira Higashibata6, Takashi Yamazaki7, Noriaki Ishioka6, Hideyuki Takahashi1
1Graduate School of Life Sciences, Tohoku University, Sendai, Japan, 2Faculty of Science, Yamagata University, Yamagata, Japan, 3Advanced Engineering Services, Tsukuba, Japan, 4Japan Manned Space Systems Co., Tsuchiura, Japan, 5Japan Space Forum, Tokyo, Japan, 6Japan Aerospace Exploration Agency, Tsukuba, Japan, 7Teikyo University, Tokyo, Japan
[p-4] Space Life Science (4)
Session Date June 6 (Tue) 16:00 – 17:40
Room Meeting Room 12
Chairpersons Yoshiaki Kitaya (Osaka Prefecture University, Japan)
Naomi Katayama (Nagoya Women’s University, Japan)
2017-p-13 ( 16:00 – 16:25 )
Water Status of Plants under Low Gravity Conditions
Yoshiaki Kitaya1, Hiroaki Hirai1, Ayako Tokuda1, Sachiko Yano2
1Graduate School of Life and Environmental Sciences, Osaka Prefecture University, Osaka, Japan, 2Japan Aerospace Exploration Agency, Ibaraki, Japan
2017-p-14 ( 16:25 – 16:50 )
Evaluation of Growth Performance of Super-Dwarf Rice in Space Agriculture
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, Yukimi Okano1
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) 11:00 – 12:20
Room Meeting Room 13
Chairpersons Tadashi Takano (Nihon University, Japan)
Hiroaki Suzuki (Japan Aerospace Exploration Agency, Japan)
2017-q-02 ( 11:00 – 11:20 )
Current Research on Laser Wireless Power Transmission Technology
Hiroaki Suzuki, Kazuhisa Kitakura
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan
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, Toshihiro Naganawa, Kuniaki Shibata, Kenji Saegusa
Department of Electronics Engineering, Nihon University, Funabashi, 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
1The Graduate University for advanced Studies (SOKENDAI), Sagamihara, Japan, 2Institute of Space and Astronautical Science, Sagamihara, Japan, 3Delft University of Technology, Netherlanmd, 4Tokyo University of Science, Suwa, Japan
2017-q-03 ( 12:00 – 12:20 )
Wireless Power Transmission for Space-based Solar Power with Distributed Electric Grid
Frank E. Little
Texas A&M University, USA
[q-2] Space Power System I
Session Date June 9 (Fri) 14:00 – 15:00
Room Meeting Room 13
Chairperson Koji Tanaka (JAXA, Japan)
2017-q-08 ( 14:00 – 14:20 )
Applications of Linear Programming Techniques to Satellite Power Management and Scheduling
Joshua Critchley-Marrows, Martin Isacsson, Agnes Gårdebäck
KTH Royal Technology Institute, Sweden
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, Sendai, 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-3] Space Power System II
Session Date June 9 (Fri) 16:00 – 17:20
Room Meeting Room 13
Chairperson Koji Tanaka (JAXA, Japan)
2017-q-11 ( 16:00 – 16:20 )
Design and Implementation of a High Powered Electrical Power Subsystem for AMMEQ-1, a 3U CubeSat
Trevor Kwan1, Xiaofeng Wu1, Eugene Kim1, Robert Bedington2, Xueliang Bai2, Alex Ling2
1The 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, Isai Fajardo Tapia1, Bianca Szasz1, Sidi Bendoukha1, Masanori Nishio2
1Department of Applied Science for Integrated Systems Engineering, Kyushu Institute of Technology, Kitakyushu, Japan, 2Aichi University of Technology, Sagamihara, Japan
2017-q-13 ( 16:40 – 17:00 )
Power Resource Allocation in Electrically Closed System using Hybrid Control under Multi-agent System
Sho Ohtani1, Osamu Mori2
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
2017-q-14 ( 17:00 – 17:20 )
The Failure Rate Calculation Method for High Power Devices in Low Earth Orbit
Erdenebaatar Dashdondog, Shohei Harada, Yuji Shiba, Masaki Sudo, Ichiro Omura
Kyushu Institute of Technology, Kitakyushu, Japan
[r-1] Space Environment (Radiation)
Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 13
Chairpersons Masao Nakamura (Osaka Prefecture University, Japan)
Kiyokazu Koga (Japan Aerospace Exploration Agency, Japan)
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, Fukuoka, 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, JAXA, Tsukuba, 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
Arerospace Research and Development Directorate, JAXA, Ibakaki, Japan
2017-r-05 ( 10:20 – 10:40 )
A Pulsed Supersonic Valve System Aimed for Martian Atmospheric Simulation
Ryota Okura1, Minoru Iwata2, Sze Keat Chee3, Kumiko Yokota1, Masahito Tagawa1
1Kobe University, Kobe, Japan;, 2Kyushu Institute of Technology, Kita-Kyusyu, Japan, 3Mechano Transformer Corp., Tokyo, Japan
[r-2] Space Environment (Charging 1)
Session Date June 6 (Tue) 11:00 – 12:40
Room Meeting Room 13
Chairpersons Rikio Watanabe (Tokyo City University, Japan)
Haruka Ueno (JAXA, Japan)
2017-r-06 ( 11:00 – 11:20 )
Mission Results of Arc Event Generator and Investigation Satellite “HORYU-IV” and Impact of Harness Self-inductance to the Discharge Current.
Hiroshi Fukuda1, Horyu-Iv Member 2, Kazuhiro Toyoda2, Mengu Cho2
1Laboratory of Spacecraft Environment Interaction Engineering, Kyushu Institute of Technology, Japan, 2Department of engineering (Electrical and Electronics), Kyushu Institute of Technology, Japan
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 Örger, J. Rodrigo Cordova Alarcon, Kazuhiro Toyoda, Mengu Cho
Kyushu Institute of Technology, Kitakyushu, Japan
2017-r-08 ( 11:40 – 12:00 )
Assessment of Spacecraft Surface Charging in Worst GEO Environmental Conditions
Shinya Nakamura1, Ryota Kawachi1, Masao Nakamura1, Kazuhiro Toyoda2
1Department of Aerospace Engineering, Osaka Prefecture University, Sakai, Japan, 2Department of Electrical Engineering, Kitakyushu, Kitakyushu, Japan
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, NICT, Koganei, Japan, 2Research and Department Directorate, JAXA, Tsukuba, Japan
2017-r-10 ( 12:20 – 12:40 )
An Experimental Process to Measure the I-V Characteristics Using Arc Jet Plasma Wind Tunnel of Space Probe Reentry having Thermal Shield made by LATS
Sidi Ahmed Bendoukha1, Kei-Ichi Okuyama1, Szasz Bianca1, Shimoda Takayuki2
1Graduate School of Engineering, Department of Applied Science for Integrated System Engineering, Kyushu Institute of Technology, Japan, 2Institute of Space and Aeronautical Sciences ISAS, Kanagawa, Japan
[r-3] Space Environment (Charging 2)
Session Date June 6 (Tue) 14:00 – 15:20
Room Meeting Room 13
Chairpersons Kazuhiro Toyoda (Kyushu Institute of Technology, Japan)
Kazuyuki Mori (JAXA, Japan)
2017-r-11 ( 14:00 – 14:20 )
The Relationship Between Accumulated Charge in Electron Beam Irradiated Fluorine Insulating Materials
Masahito Miyoshi, Kimio Hijikata, Hiroaki Miyake, Yasuhiro Tanaka
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 Satellite Charging
Kiyokazu Koga, Haruka Ueno
Research and Development Directorate, JAXA, Tsukuba, Japan
2017-r-13 ( 14:40 – 15:00 )
Evaluation of Electron-emitting Film for Spacecraft 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 (Kyutech), Kitakyushu, Japan, 2Office National d’Etudes et de Recherches Aérospatiales (ONERA), Toulouse, France, 3Japan Aerospace Exploration Agency (JAXA), Japan
2017-r-14 ( 15:00 – 15:20 )
Change of Secondary Electron Emission Yield of Insulating Material by Electron Beam Irradiation
Natsumi Sato, Hiroaki Taniguchi, Hiroaki Miyake, Yasuhiro Tanaka
Tokyo City University, Tokyo, Japan
[r-4] Materials
Session Date June 6 (Tue) 16:00 – 17:40
Room Meeting Room 13
Chairpersons Kiyokazu Koga (Japan Aerospace Exploration Agency, Japan)
Aki Goto (Japan Aerospace Exploration Agency, Japan)
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
1Kobe University, Kobe, Japan, 2Kyushu Institute of Technology, Kita-kyushu, Japan
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 Koshiba1, Kenji Ishida1, Minoru Iwata2, Kumiko Yokota1, Masahito Tagawa1
1Kobe University, Kobe, Japan, 2Kyushu Institute of Technology ,Kita-Kyushu, Japan
2017-r-17 ( 16:40 – 17:00 )
Surface Analysis Results of Atomic Oxygen Protective Coating Film
Miyuki Waki, Yugo Kimoto
Research and Development Directorate, JAXA, Tsukuba, 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 Suzuki1, Hiroaki Miyake1, Yasuhiro Tanaka1, Teppei Okumura2, Shiro Kawakita2, Masato Takahashi2, Kiyokazu Koga2
1The Measurement and Electric Machine Control Laboratory, Tokyo City University, Tokyo, Japan, 2Research and Development Directorate, JAXA, Tsukuba, 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, Tsukuba, Japan
[r-5] Space Debris (Observation)
Session Date June 7 (Wed) 9:00 – 10:00
Room Meeting Room 13
Chairpersons Toshiya Hanada (Kyushu University, Japan)
Matthew D Hejduk (Astrorum Consulting, USA)
2017-r-21 ( 9:00 – 9:20 )
Effective Search Strategy Applicable for Narrow Field-of-view Telescope
Yuki Itaya1, Koki Fujita2, Toshiya Hanada1
1Department of Aeronautics and Astronautics, Kyushu University, Fukuoka, Japan, 2Department of Aerospace Engineering, Nippon Bunri University, Oita, Japan
2017-r-22 ( 9:20 – 9:40 )
Detection of LEO Objects Using Large CMOS Sensor
Toshifumi Yanagisawa, Hirohisa Kurosaki
Chofu Aerospace Center, JAXA, Tokyo , Japan
2017-r-24 ( 9:40 – 10:00 )
A New Method for the Identification of Objects Detected in Beam-park Experiments
Hai Jiang1,2, Jing Liu1,2, Yang Li1, Yao Zhang1,2, Haowen Cheng1
1National Astronomical Observatory, Chinese Academy of Sciences, China, 2University of 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 Toshifumi Yanagisawa (Japan Aerospace Exploration Agency, Japan)
Hai Jiang (Chinese Academy of Sciences, China)
2017-r-25 ( 11:00 – 11:20 )
Application of Image Restoration in Optical Space Debris Observations
Rongyu Sun
Purple Mountain Observatory, Chinese Academy of Sciences, Nanjing, China
2017-r-26 ( 11:20 – 11:40 )
The YORP Effect on Defunct Earth Orbiting Satellites
Daniel Scheeres
Smead Department of Aerospace Engineering Sciences, The University of Colorado Boulder, USA
2017-r-28 ( 12:00 – 12:20 )
Measurement of Momentum to Move with Hypervelocity Impacts of Projectile
Masahiro Nishida1, Koichi Hayashi2, Hirohisa Kurosaki3, Toshifumi Yanagisawa3, Masumi Higashide3
1Nagoya Institute of Technology, Nagoya, Japan, 2National Institute of Technology, Toba College, Toba, Japan, 3JAXA/ARD, Chofu, Japan
2017-r-29 ( 12:20 – 12:40 )
Estimation of Orbital Parameters of Broken-up Objects from In-situ Debris Measurements
Yutaka Kodama1, Koki Fujita2, Toshiya Hanada1
1Department of Aeronautics and Astronautics, Kyushu University, Fukuoka, Japan, 2Aerospace Engineering, Nippon Bunri University, Oita, Japan
[r-7] Space Debris (Modelling)
Session Date June 7 (Wed) 16:00 – 17:40
Room Meeting Room 13
Chairpersons J.-C. Liou (National Aeronautics and Space Administration, USA)
Takayuki Hirai (Japan Aerospace Exploration Agency, Japan)
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 Fujita3, Toshiya Hanada1
1Department of Aeronautics and Astronautics, Kyushu University, Fukuoka, Japan, 2Institute of Statistical Mathematics, Research Organization of Information and Systems, Tachikawa, Japan, 3Department of Aerospace Engineering, Nippon Bunri University, Oita, Japan
2017-r-31 ( 16:20 – 16:40 )
Evaluation of Space Debris Mitigation Measures Using a Debris Evolutionary Model
Satomi Kawamoto1, Takayuki Hirai1, Shiki Kitajima2, Shuji Abe2, Toshiya Hanada2
1Research and Development Directorate, JAXA, Chofu, Japan, 2Kyushu University, Fukuoka, Japan
2017-r-32 ( 16:40 – 17:00 )
Spacecraft Break-up Models for the Atmospheric Re-entry from Highly Eccentric and Interplanetary Trajectories
Stijn Lemmens1, Jan Siminski1, Francesca Letizia2, Quirin Funke1, Klaus Merz1
1Space Debris Office, European Space Agency, Darmstadt, Germany, 2Astronautics Research Group, University of Southampton, Southampton, United Kingdom
2017-r-33 ( 17:00 – 17:20 )
Development of an Orbital Model for Small-Sized Space Debris Considering Electromagnetic Fields around the Earth
Keisuke Akari1, Hiroshi Yamakawa1, Toshiya Hanada2, Koki Fujita3
1Research Institute for Sustainable Humanosphere, Kyoto University, Kyoto, Japan, 2Faculty of Engineering, Kyushu University, Fukuoka, Japan, 3Department of Aerospace Engineering, Nippon Bunri University, Oita, Japan
2017-r-34 ( 17:20 – 17:40 )
Crater Shape and Ejecta Size from Pure Aluminum Due to Hypervelocity Impact
Yushiro Mozaki1, Masahiro Nishida1, Hiroyuki Yamada2
1Nagoya Institute of Technology, Japan, 2National Defense Academy of Japan, Japan
[r-8] Space Debris (Protection)
Session Date June 8 (Thu) 9:00 – 10:20
Room Meeting Room 13
Chairpersons Masahiro Nishida (Nagoya Institute of Technology, Japan)
Yukihito Kitazawa (IHI Corporation, Japan)
2017-r-35 ( 9:00 – 9:20 )
Ballistic Experiment of LPSO-type Magnesium Plate Target
Masahiro Nishida1, Fumiya Kodama1, Kaito Ishida1, Koichi Hayashi2, Yasuhiro Akahoshi3, Kazuyuki Hokamoto4, Tsuyoshi Mayama4, Michiaki Yamasaki4, Yoshihito Kawamura4
1Nagoya Institute of Technology, Japan, 2National Institute of Technology, Toba College, Japan, 3Kyushu Institute of Technology, Japan, 4Kumamoto University, Japan
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
1Nagoya Institute of Technology, Nagoya, Japan, 2JAXA/ARD, Chofu, Japan
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, Sunao Hasegawa3, Yuki Mando4, Shota Yamaguchi5, Koji Tanaka3
1Research and Development Directorate, JAXA, Tokyo, Japan, 2Space Technology Directorate I, JAXA, Ibaraki, Japan, 3Institute of Space and Astronautical Science, JAXA, Kanagawa, Japan, 4Department of Space and Astronautical Science, The Graduate University for Advanced Studies (SOKENDAI), Kanagawa, Japan, 5Graduate School of Engineering, Tokai University, Kanagawa, Japan
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 Satomi Kawamoto (Japan Aerospace Exploration Agency, Japan)
Toshiya Hanada (Kyushu University, Japan)
2017-r-39 ( 11:00 – 11:20 )
Research and Development of the Osaka Institute of Technology PROITERES 4th Nano-Satellite for Debris Removing by Electric Propulsion
Kaisei Kajihara, Hiroki Fujita, Hirokazu Tahara, Kyoko Takada
Department of Mechanical Engineering, Osaka Institute of Technology, Japan
2017-r-40 ( 11:20 – 11:40 )
Quick Report on On-Board Demonstration Experiment for Autonomous-Visual-Guidance Camera System for Space Debris Removal
Shinichi Kimura1, Yuta Horikawa2, Yasuhiro Katayama2
1Department of Electrical Engineering, Tokyo University of Science, Chiba, Japan, 2JAXA, Tsukuba, Japan
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 Hanada3
1Department of Aerospace Engineering, Nippon Bunri University, Oita, Japan, 2Department of Aeronautics and Astronautics, Graduate School of Kyushu University, Fukuoka, Japan, 3Department of Aeronautics and Astronautics, Kyushu University, Fukuoka, Japan
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 Shinichi Kimura (Tokyo University of Science, Japan)
Francois Laporte (CNES, France)
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, Kajuro Makihara1
1Department of Aerospace Engineering, Tohoku University, Sendai, Japan, 2Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara, Japan
2017-r-44 ( 14:20 – 14:40 )
Numerical Simulation of Tape Tether Deployment from Storage Container
Hirohisa Kojima1, Pavel Trivailo2, Takeo Watanabe3, Hironori Fujii4
1Department of Aerospace Engineering, Tokyo Metropolitan University, Hino, Japan, 2School of Engineering, RMIT University, Melbourne, Australia, 3Department of Aerospace Engineering, Kanagawa Institute of Technology, Atsugi, Japan, 4TMIT, Tokyo, Japan
[r-11] Space Debris (Active Debris Removal 3)
Session Date June 8 (Thu) 16:00 – 17:20
Room Meeting Room 13
Chairpersons J.-C. Liou (National Aeronautics and Space Administtation, USA)
Masahiro Furumoto (Kyushu University, Japan)
2017-r-46 ( 16:00 – 16:20 )
Deorbiting of Space Debris by Laser Ablation
Toshikazu Ebisuzaki, Yoshiyuki Takizawa, Satoshi Wada
RIKEN, Wako, Japan
2017-r-47 ( 16:20 – 16:40 )
Study on Orbital Remediation Sequence of Space Debris using Laser Ablation
Yuta Kobayashi1, Hiroshi Yamakawa1, Toshikazu Ebisuzaki2
1Graduate School of Engineering, Research Institute for Sustainable Humanosphere, Kyoto University, Kyoto, Japan, 2RIKEN, 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, Fukuoka, Japan, 2IHI Corporation, Tokyo, Japan, 3Research and Development Directorate, JAXA, Chofu, 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 Toshiya Hanada (Kyushu University, Japan)
Toshifumi Yanagisawa (Japan Aerospace Exploration Agency, Japan)
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, Satoshi Ikari, Shinichi Nakasuka, Ryu Funase, Akihiro Ishikawa
Department of Aeronautics and Astronautics, The University of Tokyo, 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 Yamakawa1
1Research Institute for Sustainable Humanosphere, The University of Kyoto, Kyoto, Japan, 2Department of Mechanical and Aerospace Engineering, The University of Strathclyde, Glasgow, UK
2017-r-53 ( 9:40 – 10:00 )
Magnetic Field Effects on Sub-millimeter-size Debris
Makoto Hanada1, Koki Fujita2, Toshiya Hanada1, Hiroshi Yamakawa3
1Department of aeronautics and astronautics, Kyushu University, Fukuoka, Japan, 2Aerospace Engineering, Nippon Bunri University, Oita, Japan, 3Kyoto University, Kyoto, Japan
2017-r-54 ( 10:00 – 10:20 )
Rotational Changes of the NEA (Near-Earth-Asteroid) 99942 Apophis During the 2029 Close Encounter with the Earth
Jean Souchay1, Christoph Lhotka2, Marta Folgueira3, Victor Puente3
1SYRTE, Observatoire de Paris, PSL Research University, CNRS, Sorbonne Universités, UPMC Univ. Paris, France, 2Space Research Institute, Austrian Academy of Sciences, Austria, 3Sección departemental de Astronomia y Geodesia. Facultad de Ciencas Mathematicas, Universidad Complutense Madrid, Spain
[r-13] Space Debris (Legal Issue, Collision Avoindace, Operation)
Session Date June 9 (Fri) 11:00 – 12:00
Room Meeting Room 3
Chairpersons Yukihito Kitazawa (IHI Corporation, Japan)
Toshikazu Ebisuzaki (RIKEN, Japan)
2017-r-55 ( 11:00 – 11:20 )
Political and Legal Challenges for Active Space Debris Removal-Possible International Steps-
Yu Takeuchi
Management and Integration Department, Space Technology Directorate I, JAXA, Tsukuba, Japan
2017-r-56 ( 11:20 – 11:40 )
French Contribution to EU SST CA Service
François Laporte, Monique Moury
Centre National d’Études Spatiales, CNES, Toulouse, France
2017-r-58 ( 11:40 – 12:00 )
Consideration of Collision “Consequence” in Satellite Conjunction Assessment and Risk Analysis
M. Hejduk1, F. Laporte2, M. Moury2, L. Newman3, R. Shepperd4
1Astrorum Consulting LLC, Woodway, TX USA, 2Centre Nationale d’Études Spatiales, Toulouse, France, 3NASA Goddard Space Flight Center, Greenbelt Maryland USA, 4The Boeing Company, contractor to Iridium Communications, Inc.; Leesburg, Virginia USA
[t-1] Microsatellite and Software
Session Date June 6 (Tue) 14:00 – 15:00
Room Meeting Room 3
Chairpersons Naohiko Kohtake (Keio University, Japan)
Yohsuke Nambu (Osaka Prefecture University, Japan)
2017-t-02 ( 14:00 – 14:20 )
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, Manchester, United Kingdom
2017-t-04 ( 14:20 – 14:40 )
An Implementation of Bus-Type Architecture with Common Subsystem to Microsatellite ORBIS
Hirohisa Asano, Hironori Sahara
Department of Aerospace Engineering, Tokyo Metropolitan University, Tokyo, Japan
2017-t-05 ( 14:40 – 15:00 )
Satellite Control System Utilizing Orbit Calculation Package Software ORBITER FORCE
Yoshiyuki Takasugi, Keiko Takahashi, Shinichi Kawazoe, Takafumi Ohnishi, Masaya Kameyama
Fujitsu Limited, Japan
[t-2] Value Creation and Innovation
Session Date June 6 (Tue) 16:00 – 17:40
Room Meeting Room 3
Chairpersons Naohiko Kohtake (Keio University, Japan)
Yohsuke Nambu (Osaka Prefecture University, Japan)
2017-t-06 ( 16:00 – 16:20 )
A Methodology to Create Innovative Space Application Services
Makoto Ioki1, Tsuyoshi Hirose1, Shoji Yoshikawa2, Naoki Imamura2, Kazuhide Kodeki2, Seiichi Shimizu2, Osamu Takahara2, Eiji Yokoyama2
1Graduate School of System Design and Management, Keio University, Kanagawa, Japan, 2Advanced Technology R&D Center, Mitsubishi Electric Corporation., Hyogo, Japan
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, Manchester, United Kingdom
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 )
Systems Evaluation Framework for a Futuristic Aerospace Project
Nobuaki Minato
Graduate School of Technology Management, Ritsumeikan University, Kyoto, Japan
2017-t-10 ( 17:20 – 17:40 )
Value-Centric/Driven Design – A Framework
Lavanan Vengadasalam, Abdullah Desai, Peter Hollingsworth, Katharine Smith
School of Mechanical, Aerospace and Civil Engineering, The University of Manchester, Manchester, United Kingdom
[t-3] Mission Design and Education
Session Date June 7 (Wed) 9:00 – 10:40
Room Meeting Room 12
Chairpersons Yohsuke Nambu (Osaka Prefecture University, Japan)
Masahiko Nagai (Yamaguchi University, Japan)
2017-t-11 ( 9:00 – 9:20 )
Space Mission Architecture Design Philosophies and Methodologies – A Review
Lavanan Vengadasalam, Peter Hollingsworth, Katharine Smith
School of Mechanical, Aerospace and Civil Engineering, The University of Manchester, Manchester, United Kingdom
2017-t-12 ( 9:20 – 9:40 )
Benchmarking the Collocation Stand-Alone Library and Toolkit (CSALT)
Steven Hughes1, Jeremy Knittel1, Wendy Shoan1, Youngkwang Kim2, Claire Conway3, Darrel Conway3
1NASA Goddard Space Flight Center, USA, 2Yonsei University, South Korea, 3Thinking Systems Inc., USA
2017-t-13 ( 9:40 – 10:00 )
Automated Sensitivity Analysis of Interplanetary Trajectories for Optimal Mission Design
Jeremy Knittel1, Kyle Hughes1, Jacob Englander1, Bruno Sarli2
1NASA Goddard Space Flight Center, USA, 2Catholic University of America, USA
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, Masahiro Fukuhara2, Fabien Roudier2, Naohiko Kohtake1
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, Shoichi Kitazawa, Ken Higuchi
Muroran Institute of Technology, Muroran, Japan
[t-4] Systems Approach
Session Date June 7 (Wed) 11:00 – 12:20
Room Meeting Room 12
Chairpersons Hiraku Sakamoto (Tokyo Institute of Technology, Japan)
Masahiko Nagai (Yamaguchi University, Japan)
2017-t-16 ( 11:00 – 11:20 )
Modular Platform for Hardware-in-the-Loop Testing of Autonomous Flight Algorithms
Mar Cols-Margenet1, Hanspeter Schaub1, Scott Piggott2
1Autonomous Vehicle Systems Laboratory, University of Colorado Boulder, Boulder, Colorado, United States, 2Laboratory for Atmospheric and Space Physics, Boulder, Colorado, United States
2017-t-17 ( 11:20 – 11:40 )
Probability Inference Approach for Stochastic Robust Flight Control Design
Taro Tsukamoto
The Japan Aerospace Exploration Agency, Tokyo, Japan
2017-t-18 ( 11:40 – 12:00 )
Updates on the Development of the Support Software System for the Philippines’ Microsatellite Operations
Mark Edwin Tupas1, Romer Kristi Aranas1, Benjamin Joseph Jiao1, Kaye Kristine Vergel2,3, Francisco Miguel Felicio2, Gay Jane Perez2, Marc Caesar Talampas1, Mary Ann Constante1, Orville Labbao1, John Leur Labrador1,4 , Harold Bryan Paler5, Joel Joseph Marciano, Jr. 1,5
1College of Engineering, University of the Philippines Diliman, Quezon City, Philippines, 2College of Science, University of the Philippines Diliman, Quezon City, Philippines, 3Department of Cosmosciences, Hokkaido University, Sapporo, Japan, 4Department of Aerospace Engineering, Tohoku University, Sendai, Japan, 5Advanced Science and Technology Institute, Department of Science and Technology, Quezon City, Philippines
2017-t-19 ( 12:00 – 12:20 )
Fatigue Life Estimation of Spaceborne 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 University, Republic of Korea, 2Korea Aerospace Research Institute (KARI), Republic of Korea, 3ExleetEdge Inc., Republic of Korea
[t-5] Positioning System
Session Date June 7 (Wed) 16:00 – 17:40
Room Meeting Room 12
Chairpersons Yohsuke Nambu (Osaka Prefecture University, Japan)
Masahiko Nagai (Yamaguchi University, Japan)
2017-t-20 ( 16:00 – 16:20 )
Spot-based RTK Positioning for Improvement of Oil Palm Replanting Processes
Akira Kodaka1, Tomoaki Masuma2, Mohd Najib Bin Abd Rasid3, Haryati Abidin3, Mohd Na’Aim Bin Samad3, Ko Hamamoto4, Naohiko Kohtake1
1Graduate School of System Design and Management, Keio University, Yokohama, Japan, 2Advanced Services, Cisco Systems G.K., Tokyo, Japan, 3FGV R&D and Agri Services Cluster, Kuala Lumpur, Malaysia, 4Department of Aeronautics and Astronautics, JAXA, Tokyo, Japan
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 & Logistics Agency, Japan, 3Keio University, Japan
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 Kohtake
Graduate School of System Design and Management, Keio University, Japan
2017-t-23 ( 17:00 – 17:20 )
Process Optimization Method for the Simplification of Developing Indoor-Outdoor Seamless Positioning Environment
Kenichi Tabata1,2, Madoka Nakajima1,2, Naohiko Kohtake1
1Graduate School of System Design and Management, Keio University, Yokohama, Japan, 2Kokusai Kogyo Co., Ltd, Tokyo, Japan
2017-t-24 ( 17:20 – 17:40 )
A Simulation for GNSS Utilization and DEM Construction in Urban
Masahiko Nagai1, Sakpod Tongleamnak2, Zahid Wani2
1Center for Research and Application for Satellite Remote Sensing, Yamaguchi University, Japan, 2Asian Institute of Technology, Thailand
[t-6] Modeling and Simulation
Session Date June 8 (Thu) 11:00 – 11:40
Room Meeting Room 7
Chairperson Masahiko Nagai (Yamaguchi University, Japan)
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
1Osaka Prefecture University, Osaka, Japan, 2Tottori University, Tottori, Japan, 3levii Inc., Tokyo, Japan
2017-t-26 ( 11:20 – 11:40 )
SIRIUS Model-Driven Software Product Line for Flight Dynamics Systems
Pâmini Annat1, Romain Bernard2, Jesús Esteban Dones3
1Centre National d’Etudes Spatiales, CNES, Toulouse, France, 2EXMS, France, 3Thalès Services, Toulouse, France
[u-1] Space Education for Children and General Public
Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 11
Chairpersons Makoto Yoshikawa (Japan Aerospace Exploration Agency, Japan)
Kaori Sasaki (Japan Aerospace Exploration Agency, Japan)
2017-u-01 ( 9:00 – 9:20 )
Space Education Method to Influence School Teachers
Osamu Matsubara
Space Education Center, JAXA, Sagamihara, Japan
2017-u-02 ( 9:20 – 9:40 )
JAXA Space Education Program for Informal Education- The Process of Reorganizing “Aerospace School” –
Keiko Miyata
Japan Aerospace Exploration Agency (JAXA) Space Education Center
2017-u-03 ( 9:40 – 10:00 )
Outreach and Public Relations of Hayabusa2 Project
Makoto Yoshikawa, Eri Koyama, Satoshi Hosoda, Yuto Takei, Satoru Nakazawa, Yuichi Tsuda, Azusa Yabe, Takuya Ohkawa
Institute of Space and Astronautical Science, JAXA, Sagamihara, 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, Japan
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, Japan
[u-2] Space Education for Students of Engineering
Session Date June 6 (Tue) 11:00 – 12:40
Room Meeting Room 11
Chairpersons Hiroshi Hirayama (Akita University, Japan)
Alim Rustem Aslan (Istanbul Technical University, Turkey)
2017-u-06 ( 11:00 – 11:20 )
Implementation Report of KOSEN Space Camp
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, Japan, 3NIT, Akashi College, Japan, 4NIT, Gunma College, Japan, 5NIT, Tokuyama College, Japan, 6NIT, Kagawa College, Japan, 7 NIT, Nara College, Japan, 8 NIT, Yonago College, Japan, 9NIT, Kagoshima College, Japan, 10 Human Network KOSEN, Japan
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
1National Institute of Technology (NIT), Kochi College, Nankoku, Japan, 2NIT, Tokuyama College, Shunan, Japan, 3NIT, Kagawa College, Takamatsu, Japan, 4NIT, Nara College, Yamatokoriyama, Japan, 5NIT, Niihama College, Niihama, Japan, 6NIT, Akashi College, Akashi, Japan, 7 NIT, Gunma College, Maebashi, Japan, 8 NIT, Kagoshima College, Kirishima, Japan, 9 NIT, Gifu College, Motoshu, Japan, 10 NIT, Yonago College, Yonago, Japan, 11Human Network KOSEN, Tokyo, Japan
2017-u-08 ( 11:40 – 12:00 )
An Engineering Design Education Program as an Inheritance of Space Technology Education Project
Kentaro Kitamura1, Itsuo Sakuramoto1, Mitsumasa Ikeda1, Taku Takada2, Kazumasa Imai2, Makoto Wakabayashi3, Kosen Space Collaboration Group 1
1National Institute of Technology, Tokuyama College, Yamaguchi, Japan, 2National Institute of Technology, Kochi College, Yamaguchi, Japan, 3National Institute of Technology, Niihama College, Yamaguchi, Japan
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
1Faculty of Engineering, Information and Systems, University of Tsukuba, Tsukuba, Japan, 2Graduate School of Systems and Information Engineering, University of Tsukuba, Tsukuba, Japan, 3Graduate School of Pure and Applied Sciences, University of Tsukuba, Tsukuba, Japan
2017-u-10 ( 12:20 – 12:40 )
Space Educational 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, Tokyo, Japan
[u-3] Satellites for Space Education
Session Date June 6 (Tue) 14:00 – 15:40
Room Meeting Room 11
Chairpersons Hironori Sahara (Tokyo Metropolitan University, Japan)
Mohammed Khalil Ibrahim (Nihon University, Japan)
2017-u-11 ( 14:00 – 14:20 )
Introducing CanSat for Project Based Learning (PBL) of Space Science and Engineering in Nepal
Rakesh Chandra Prajapati1, Abinish Kumar Dutta1,2, Sanjeeb Humagain1,2, Saurav Paudel2, Jiten Thapa2, Safal Shrestha2
1Pico/Nano-Satellite Research and Development Lab, ORION Space, Kathmandu, Nepal, 2Department of Electrical and Electronics Engineering, Kathmandu University, Dhulikhel, Nepal
2017-u-12 ( 14:20 – 14:40 )
Capacity Building in Space Technology in the Philippines through the PHL-Microsat Program
Mary Ann Constante1, Paula Jean Cansino1, Izrael Zenar Bautista1, Gladys Bajaro1
1College of Engineering, University of the Philippines Diliman, Quezon City, Philippines, 2Advanced Science and Technology Institute, Department of Science and Technology, Quezon City, Philippines
2017-u-13 ( 14:40 – 15:00 )
Developing a MicroSat Kit for Space Systems Engineering Education
Nguyen Huu Diep, Nguyen Dinh Chau Minh, Pham Van Phap, Nguyen Tien Su, Cao Xuan Hiep, Pham Anh Minh, Tran Cong Duong, Nguyen Truong Thanh, Hoang The Huynh, Le Xuan Huy
Vietnam National Satellite Center (VNSC), Vietnam
2017-u-14 ( 15:00 – 15:20 )
Scalable Nano-Satellite Platform for Low-Cost Space Education
Toshinori Kuwahara, James Harpur, Shinya Fujita, Yuji Sato, Ta Phuong Linh, Ngo Thanh Cong, Tran Van Ninh, Nguyen Minh Thao, Pasith Tangdhanakanond
Department of Aerospace Engineering, Tohoku University, Sendai, 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 (AIST), Tokyo, Japan
[u-4] Competitions and Culture
Session Date June 6 (Tue) 16:00 – 17:20
Room Meeting Room 11
Chairpersons Misuzu Onuki (Space Frontier Foundation, Japan)
Guy Pignolet (Reunion Island Space Initiative, Reunion)
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
1Artist, Reunion Island, 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, Reunion, 3HASTIC, Japan
[u-5] Rockets for Space Education
Session Date June 7 (Wed) 9:00 – 10:20
Room Meeting Room 15
Chairpersons Yutaka Wada (Chiba Institute of Technology, Japan)
Toshiyuki Katsumi (Nagaoka University of Technology, Japan)
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
1Department of Mechanical Engineering, Ehime University, Matsuyama, Japan, 2Department of Mechanical Engineering, Saitama Institute of Technology, Fukaya, Japan
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, Saitama, Japan, 2Department of Mechanical Engineering, Ehime University, Matsuyama, Japan
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-François Paradis1, Benoît Debaque1, Simon Lambert Girard1, Margarida Romero1,2
1EspaceLab, Quebec, Canada, 2Laval University, Teaching and Learning Dept., Quebec, Canada
2017-u-23 ( 10:00 – 10:20 )
A Development of Candy Hybrid Rocket Motor for Undergraduate Space Education
Yutaka Wada1, Yo Kawabata1, Kenji Ogimoto2, Hiroaki Akiyama3, Takao Yanagi4, Seiichi Sakamoto5
1Chiba Institute of Technology, Japan, 2SOUKI Systems Co. Ltd., Japan, 3Wakayama University, Japan, 4Hakuhodo DY media partners Inc., Japan, 5NAOJ, Japan
[v-1] Law and Policy for Space Development
Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 15
Chairpersons Yasuaki Hashimoto (The National Institute for Defense Studies, Japan)
Hirotaka Watanabe (Osaka University, Japan)
2017-v-02 ( 9:20 – 9:40 )
The Legal Status of the Hosted Payload
Akiko Watanabe
Independent Researcher, Tokyo, Japan
2017-v-03 ( 9:40 – 10:00 )
The Legality of an International Regime for Space Traffic Management (STM)- Placing the co-existence of military and civil STM systems –
Yu Takeuchi
Management and Integration Department, Space Technology Directorate I, JAXA, Tsukuba, 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
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 Motoko Uchitomi (The University of Tokyo, Japan)
Yasuaki Hashimoto (The National Institute for Defense Studies, Japan)
2017-v-06 ( 11:00 – 11:20 )
Earthquake Prediction Research as a National Space Project
Tetsuya Kodama
Research and Development Directorate, JAXA, Tsukuba, 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, Tokyo, Japan
2017-v-09 ( 11:40 – 12:00 )
Space Development Models and Paths Analysis of Asian and African Countries
Feng-Tai Hwang
National Space Organization, Hsinchu City, 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 Hirotaka Watanabe (Osaka University, Japan)
Hiroshi Yoshida (Excalibur K.K, Japan)
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
Dentsu Space Lab, Tokyo, Japan
[w-1] Safety and Mission Assurance (EEE Parts)
Session Date June 6 (Tue) 9:00 – 10:40
Room Meeting Room 14
Chairpersons Katsuhito Goto (JAMSS, Japan)
Ryoji Kobayashi (Japan Aerospace Exploration Agency, Japan)
2017-w-01 ( 9:00 – 9:20 )
SEE Sensitivity Evaluation Results of Atom Switch ROM/FPGA
Kozo Takeuchi1, Munehiro Tada2, Toshitsugu Sakamoto2, Hiroyuki Shindo1, Satoshi Kuboyama1, Akinori Takeyama3, Takeshi Ohshima3, Koichi Suzuki1
1Research and Development Directorate, JAXA, Tsukuba, Japan, 2System Platform Research Laboratories, NEC Corp., Tsukuba, Japan, 3Quantum Beam Science Research Directorate, QST, Takasaki, Japan
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
1Research and Development Directorate, JAXA, Tsukuba, Japan, 2Fuji Electric Co., Ltd., Matsumoto, Japan
2017-w-03 ( 9:40 – 10:00 )
Approach to High Thermal Conductive Substrate for Electronic Components
Kazunori Shimazaki, Yuji Yamada, Koichi Suzuki
Research and Development Directorate, JAXA, Tsukuba, 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
Keita Sakamoto, Hiroyuki Shindou, Satoshi Kuboyama, Koichi Suzuki
Japan Aerospace Exploration Agency, JAXA, Japan
2017-w-05 ( 10:20 – 10:40 )
A Proposal for Guideline to use the COTS EEE parts for The Scientific Satellites
Kazuhide Noguchi
Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
[w-2] Safety and Mission Assurance (Assuarance Technology)
Session Date June 6 (Tue) 11:00 – 12:20
Room Meeting Room 14
Chairpersons Ryoji Kobayashi (Japan Aerospace Exploration Agency, Japan)
Shuji Araki (Japan Aerospace Exploration Agency, Japan)
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
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 J. Burtz2, Kazuya Yoshida1
1Department of Aerospace Engineering, Tohoku University, Sendai, Japan, 2K.K. i-space inc., Tokyo, Japan
2017-w-08 ( 11:40 – 12:00 )
Improving Activity of Clean Room for Scientific Spacecraft
Matsushi Miura, Fuminari Ito, Ryoji Kobayashi
Institute of Space and Astronautical Science, JAXA, Sagamihara, 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, Masako Kikuchi1, Koji Oga1, Teruhiko Tabuchi2, Toshinori Ikenaga2, Ryu Funase3, Tatsuaki Hashimoto4
1Japan Manned Space Systems Corporation (JAMSS), Tsukuba, Japan;, 2JAXA, Tsukuba, Japan;, 3University of Tokyo, Tokyo, Japan, 4Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan;
[w-3] Safety and Mission Assurance (Principles and Standards)
Session Date June 6 (Tue) 14:00 – 15:40
Room Meeting Room 14
Chairpersons Koichi Suzuki (Japan Aerospace Exploration Agency, Japan)
Katsuhito Goto (JAMSS, Japan)
2017-w-11 ( 14:00 – 14:20 )
Principles to Develop and Operate Resilient Spacecraft
Ryoji Kobayashi
Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan
2017-w-12 ( 14:20 – 14:40 )
The Utilization of the Metrics of Scale of “Severity” and “Probability” in a Qualitative Risk Matrix
Yasushi Mori
Quality Assurance Department, Kamakura Works, Mitsubishi Electric Corporation, Kamakura, Japan
2017-w-13 ( 14:40 – 15:00 )
Quality Leadership Communication: International Cooperation in IAQG/JAQG
Hiroki Yanagawa
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 Kado1, Shuji Araki1, Mieko Matsuda1, Masayuki Ikeuchi2
1Japan Aerospace Exploration Agency, Tsukuba, Japan, 2Japan Aerospace Exploration Agency, Kanagawa, Japan
[w-4] Safety and Mission Assurance (Software Assurance)
Session Date June 6 (Tue) 16:00 – 17:20
Room Meeting Room 14
Chairpersons Shuji Araki (Japan Aerospace Exploration Agency, Japan)
Koichi Suzuki (Japan Aerospace Exploration Agency, Japan)
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
1Japan Manned Space Systems Corporation, Japan, 2East Japan Railway Company
2017-w-17 ( 16:20 – 16:40 )
A study of Applying Past Accident Cases to Software Design Across Domains using Control Structuring Diagram
Kazuki Kakimoto1, Shigeo Yoshikawa2, Hideki Nomoto2
1JAXA: Japan Aerospace eXploration Agency, Tsukuba Japan, 2JAMSS: JApan Manned Space Systems corporation, 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, Shinji Kawaguchi, Taisuke Kanbe, Yasushi Ueda
Research Unit III, Research and Development Directorate, JAXA, Tsukuba, Japan
2017-w-19 ( 17:00 – 17:20 )
Improvement of SA Activities in Spacecraft Software Development by Value Propagation of Standard Process
Tomohito Yamada, Masafumi Katahira
Research Unit III, JAXA, Ibaraki, Japan
Finalist Student Session
[s-1]
Session Date June 8 (Thu) 9:00 – 10:40
Room Sub-Hall
Chairpersons Hironori Sahara (Tokyo Metropolitan University, Japan)
Akira Kakami (University of Miyazaki, Japan)
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, Milano, Italy
2017-s-02-b ( 9:20 – 9:40 )
Parameter Survey on Rotating Magnetic Field Acceleration Method
Takeru Furukawa
Graduate School of Engineering, Tokyo University of Agriculture and Technology, Tokyo, Japan
2017-s-03-b ( 9:40 – 10:00 )
Power Matching between Plasma Source and Electrostatic Acceleration in Helicon Electrostatic Thruster
Yoshiya Nakagawa
Department of Aerospace Engineering, Nagoya University, Nagoya, Japan
2017-s-04-c ( 10:00 – 10:20 )
Electromagnetic Deployment of a Space Membrane Structure using the Geomagnetic Field in LEO
Yuki Yamada
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, The University of Tokyo, Tokyo, Japan
[s-2]
Session Date June 8 (Thu) 11:00 – 12:40
Room Sub-Hall
Chairpersons Kazuma Sekiguchi (Tokyo City University, Japan)
Hideto Mashidori (Tokyo Metropolitan College of Industrial Technology, Japan)
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
Department of Advanced Energy, The University of Tokyo, Kashiwa, 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, 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, The University of Tokyo, 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, Tokyo, Japan
2017-s-10-e ( 12:20 – 12:40 )
Ballistic Range Experiment of Sphere in Dusty Atmosphere
Chihiro Masaki
Department of Advanced Energy, The University of Tokyo, Chiba, Japan
[s-3]
Session Date June 8 (Thu) 14:00 – 15:40
Room Sub-Hall
Chairpersons Makoto Matsui (Shizuoka University, Japan)
Kazuhiro Toyoda (Kyushu Institute of Technology, Japan)
2017-s-11-f ( 14:00 – 14:20 )
Magnetic Plasma Deorbit 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, Nihon University, Chiba, 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, The University of Tokyo, 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, Tokyo, Japan
2017-s-15-k ( 15:20 – 15:40 )
The Study of the Space-based Observation of Lunar Impact Flashes
Ryota Fuse
Department of Aerospace Engineering, Nihon University, Chiba, Japan
[s-4]
Session Date June 8 (Thu) 16:00 – 17:40
Room Sub-Hall
Chairpersons Hirokazu Masui (Kyushu Institute of Technology, Japan)
Hideto Mashidori (Tokyo Metropolitan College of Industrial Technology, Japan)
2017-s-16-q ( 16:00 – 16:20 )
Study of Heater Electric Power Control with Autonomous Distributed System
Keisuke Umeda
Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan
2017-s-17-r ( 16:20 – 16:40 )
Dynamics and Control of Double-tethered Space-Tug System after Tether Rupture
Keying Yang
Beijing Institute of Technology, Beijing, China
2017-s-18-r ( 16:40 – 17:00 )
Analysis for the Amount of Electron-Hole Pair in Floride Polymer Irradiated by Electron Beam
Shugo Yoshida
Electric Measurement and Machine Control Laboratory, Tokyo City University, Tokyo, Japan
2017-s-19-r ( 17:00 – 17:20 )
Construction of the Carrier Mobilities Measurement System by Time of Flight Method
Kazuki Kodama
Tokyo City University, Tokyo, 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, 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 Motor- Deploying This Motors to Aerospace –
Yukio Fukushima1, Toyohiko Ota1, Kouichi Watanabe2
1Advanced science & intelegence research institute, inc, ASIRI, Japan, 2Fine motion laboratory, FM, Japan
2017-b-22p
Performance of Variable Magnetic Field Ion Engine of Microwave Discharge Type
Yoshiyuki Takao, Yuki Motokawa, Kaka Haku
Department of Integrated System Engineering, Nishinippon Institute of Technology, Fukuoka, 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, Sendai, Japan
2017-b-65p
Thermal Analysis of Steady-State Fully Radiation-Cooled MPD Thrusters Using Permanent Magnets for Manned Mars Exploration
Kengo Chino1, Shota Saito1, Yoshikazu Sugiyama1, Hirokazu Tahara1, Kyoko Takada2
1Department of Mechanical Engineering, Osaka Institute of Technology, Osaka, Japan, 2Department of Intellectual Property, Osaka Institute of Technology, Osaka, 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 Takada2, Tomoyuki Ikeda3
1Department of mechanical engineering, Osaka Institute of Technology, Osaka, Japan, 2Department of Intellectual Property, Osaka Institute of Technology, Osaka, Japan, 3Department of Aeronautics and Astronautics, Tokai University, Kanagawa, Japan
2017-b-67p
Impulse performance of Donut-Spherical Laser Launch System in Stratosphere Air-Pressure Conditions
Duc Thuan Tran, Chongfa Xie, Koichi Mori
Department Engineering, Nagoya University, Nagoya, Japan
2017-b-68p
The Micro-Cathode Arc Thruster for CubeSats
Yong Cao, Zhi Yang, Liang Zheng
Harbin Institute of Technology (Shenzhen)
2017-b-69p
Chemically Augmented Arcjet Thrusters
Yuka Arai, Shoko Shaibagaki, Kai Wada, Mitsutoshi Tsuchiya, Tomoyuki Ikeda, Hideyuki Horisawa
Tokai University, Japan
2017-b-70p
Feasibility Study on Rarefied Propellant Flow Measurement
Yoshinori Nakayama
Department of Aerospace Engineering, National Defense Academy, Yokosuka, 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 Horita2, Shunjiro Shinohara1
1Institute of Engineering, Tokyo University of Agriculture and Technology, Koganei, Tokyo, Japan, 2Graduate School of Engineering, Tokyo University of Agriculture and Technology, Koganei, Tokyo, Japan
2017-b-72p
Postural Control for Beam-Riding Flight of a Microwave Rocket Using an External Magnetic Field
Masayuki Takahashi, Naofumi Ohnishi
Department of Aerospace Engineering, Tohoku University, Sendai, Japan
2017-b-73p
Short-Pulse Operation of a Laser-Assisted Pulsed Plasma Thruster
Hiroaki Kamezaki1, Kota Matsubara2, Kentaro Kato2, Yuji Oigawa2, Hideyuki Horisawa3
1Undergraduate student, Department of Aeronautics and astronautics, Tokai University, Japan, 2Graduate student, Department of Aeronautics and astronautics, Tokai University, Japan, 3Professor, Department of Aeronautics and astronautics, Tokai University, Japan
2017-b-74p
Chemically Augmented Laser-thermal Thrusters
Mitsutoshi Tsuchiya1, Yuka Arai1, Kai Wada1, Miya Isoda1, Shoko Shibagaki1, Tomoyuki Ikeda2, Hideyuki Horisawa3
1Graduate student of Mechanical Engineering, Tokai University, Japan, 2Department of Aerospace and Astronautics Engineering, Associate Professor Tokai University, Japan, 3Department of Aerospace and Astronautics Engineering, Professor, Tokai University, Japan
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, Hamamatsu, Japan
2017-b-77p
Magnetic Field Measurement of Laser-Electromagnetic Hybrid Thrusters
Yuki Murayama1, Toshiaki Ohi1, Kentaro Kato1, Haruhito Kato1, Nao Akashi1, Hideyuki Horisawa2
1Department of Mechanical Engineering Graduate school of Engineering, Tokai University, Hiratsuka, Japan, 2Department of Aeronautics and Astronautics, Tokai University, Hiratsuka, Japan
2017-b-78p
Three-Dimensional Full Particle in Cell (PIC) Analyses of Three-Grid Ion Engine Operations
Takatsugu Honda, Takeshi Miyasaka, Ryo Kawamura, Takeshi Hasegawa, Makoto Asahara
Gifu University, Japan
2017-b-79p
Evaluations of Unsteady Ablation and Exhaust Phenomena on Coaxial Pulsed Plasma Thrusters
Takaaki Goto, Takeshi Miyasaka, Takahiro Kajiwara, Yuki Goto, Koji Nishigaki, Yoshimasa Matsui, Makoto Asahara
Gifu university, Japan
2017-b-80p
Plasma Profiles in a Two-dimensional Anode-layer-type Hall Thruster
Shigeru Yokota1, Hiroki Nawamoto2, Wataru Shimizu2, Junko Yamasaki2, Kohei Shimamura1
1Division of Structure and Energy, University of Tsukuba, Ibaraki, Japan, 2Department of Structure and Energy, University of Tsukuba, Ibaraki, Japan
2017-b-81p
Two-dimensional Hollow Cathode
Moyuru Yonaha1, Junko Yamasaki1, Shigeru Yokota2, Kohei Shimamura2
1Department of Structure and Energy, University of Tsukuba, Ibaraki, Japan, 2Division of Structure and Energy, University of Tsukuba, Ibaraki, Japan
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 Yokota1, Ken Nakatani1, Junko Yamasaki2, Kohei Shimamura2
1Division of Engineering Mechanics and Energy, University of Tsukuba, Tsukuba, Japan, 2Department of Engineering Mechanics and Energy, University of Tsukuba, 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 Cheng1,2, Gerard GóMez1,2, Josep J. Masdemont3, Jianping Yuan1
1School of Astronautics, Northwestern Polytechnical University, Xi’an, China, 2IEEC & Department de Matemàtiques i Informàtica, Universitat de Barcelona, Barcelona, Spain, 3IEEC & Department de Matemàtiques, Universitat Politècnica de Catalunya, Barcelona, Spain
ISTS-2017-d-168p/ISSFD-2017-168p
Reducing the Lunisolar Numerical Ephemerides for Onboard Applications
Jingshi Tang1,2, Haishuo Wang1, Hanyang Liu1, Guanshan Pu1, Lin Liu1,2
1School of Astronomy and Space Science, Nanjing University, China, 2Institute of Space Environment and Astrodynamics, Nanjing University, China
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 Silva1, Maisa Terra1, Claudia Celestino2, Cristiano Melo3
1Technological Institute of Aeronautics, ITA, São José dos Campos, Brazil, 2Federal University of ABC, UFABC, Santo André, Brazil, 3Federal University of Minas Gerais, UFMG, Belo Horizonte, Brazil
ISTS-2017-d-173p/ISSFD-2017-173p
Altitude and Motion 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, Fukuoka, Japan
ISTS-2017-d-175p/ISSFD-2017-175p
Theoretical Analysis on Zero Propellant Maneuver Existent Conditions
Mo-Yao Yu, Ya-Zhong Luo1,2, Hai-Yang Li2
College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, 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-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
1Meijo University Graduate School, Japan, 2DENSO TECHNO Co., Japan, 3Meijo University, Japan
2017-e-44p
Aerodynamic Analysis of Body-Flap in Hypersonic Flow
Lin Huo, Tao Yang
National University of Defence Technology, Changsha, 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 Kuwahara1,2, Ryo Myoen1, Makoto Matsui1
1Department of Engineering, Shizuoka University, Hamamatsu, Japan, 2Japan Atomic Energy Agency, Tokai, Japan
2017-e-46p
Temperature Measurement by Bremsstrahlung Radiation from Laser Sustained Plasma using Diode Laser
Takahiro Ono, Koji Nishimoto, Makoto Matsui
Graduate school of Integrated Science and Technology, Department Engineering, Shizuoka University, Hamamatsu, 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
1Kumoh National Institute of Technology, Gumi, Republic of Korea, 2Hanwha Corporation, Daejeon, Republic of Korea, 3Agency for Defense Development, Daejeon, Republic of Korea
2017-f-103p
Design and Implementation of Single Event Latch-up Measurement and Self-Recovery System for BIRDS CubeSat
Abdulla H. 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
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 Aoki1, Atsushi Bito1
1The University of Shizuoka, Japan, 2Nihon University, Japan
2017-h-25p
Spectral Emissivity Measurements of Molten Metals with an Electrostatic Levitation Furnace
Yuki Watanabe1, Haruka Tamaru2, Junpei T Okada3, Takehiko Ishikawa4,5
1Advanced Engineering Services Co. Ltd., Tsukuba, Japan, 2Human Spaceflight Technology Directorate, Japan Aerospace Exploration Agency, Tsukuba, Japan, 3Institute for Materials Science, Tohoku University, Sendai, Japan., 4Institute of Space and Astronautical Science, JAXA, Tsukuba, Japan, 5SOKENDAI, Japan
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 Channel
Hiroki Yamashita, Yoshihisa Takayama
Tokai University, Japan
2017-j-28p
Estimation of Data Transmission Quality under Atmospheric Effects in Free-space Laser Communication
Eiji Taira, Hiroki Yamashita, Yoshihisa Takayama
The University of Tokai, Japan
2017-j-29p
Studies on Optical Link Establishment by using Retro-reflector in Free-space Optical Communications
Keiji Oda, Yoshihisa Takayama
Tokai University, 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
Tokai University ,japan
2017-j-31p
Considerations of Optical Communication Link Design between the Earth and Mars
Yuta Ishizuka, Yoshihisa Takayama
Tokai University, Japan
2017-k-63p
Performance Model Simulation of Ganymede Laser Altimeter (GALA) for the JUICE Mission
Hiroshi Araki1, Ko Ishibashi2, Noriyuki Namiki1, Hirotomo Noda1, Masanori Kobayashi2, Keigo Enya3, Masanobu Ozaki3, Takahide Mizuno3, Yoshifumi Saito3, Kazuyuki Touhara3, Shoko Oshigami1, Shingo Kashima1, Jun Kimura4, Shingo Kobayashi5, Gregor Steinbruegge6, Alexander Stark6, Christian Althaus6, Simone Del Togno6, Kay Lingenauber6, Hauke Hussmann6
1National Astronomical Observatory of Japan, Tokyo, Japan, 2Planetary Exploration Research Center, Chiba Institute of Technology, Chiba, Japan, 3Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 4Osaka University, Osaka, Japan, 5National Institute of Radiological Science, Chiba, Japan, 6German Aerospace Center (DLR), Berlin, Germany
2017-k-64p
Science Objectives of the Ganymede Laser Altimeter (GALA) for the JUICE Mission
Jun Kimura1, Shunichi Kamata2, Koji Matsumoto3, Shoko Oshigami4, Noriyuki Namiki5, Kiyoshi Kuramoto6, Sho Sasaki1, Keigo Enya7, Hauke Hussmann8, Kay Lingenauber8
1Department of Earth and Space Science, Osaka University, Osaka, Japan, 2Creative Research Institution, Hokkaido University, Hokkaido, Japan, 3RISE Project Office, National Astronomical Observatory of Japan, Iwate, Japan, 4Center for Computational Astrophysics, National Astronomical Observatory of Japan, Tokyo, Japan, 5RISE Project Office, National Astronomical Observatory of Japan, Tokyo, Japan, 6Department of Cosmosciences, Hokkaido University, Hokkaido, Japan, 7Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Kanagawa, Japan, 8Institute of Planetary Research, DLR, Berlin, Germany
2017-k-65p
Optical/Mechanical Design for the Focal Plane Receiver of the Ganymede Laser Altimeter (GALA) for the Jupiter Icy Moon Explorer (JUICE) Mission
Keigo Enya1,2, Masanori Kobayashi3, Ko Ishibashi3, Shingo Kobayashi4, Noriyuki Namiki2,5, Hiroshi Araki2,5, Hirotomo Noda2,5, Shoko Oshigami6, Jun Kimura7, Satoru Iwamura8, Naofumi Fujishiro9, Teruhito Iida10, Hiroyuki Nakagawa11, Okiharu Kirino11, Chihiro Hatakeyama12, Takeshi Yokozawa12, Naoki Matsui12, Masayuki Fujii12, Toshihiko Yamawaki1, Kazuyuki Touhara1, Christian Althaus13, Simone Del Togno13, Judit Jänchen13, Belinda Borgs13, Thomas Behnke13, Kay Lingenauber13, Reinald Kallenbacha13, Hauke Hussmann13
1Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Kanagawa, Japan, 2The Graduate University for Advanced Studies, Japan, 3Planetary Exploration Research Center, Chiba Institute of Technology, Chiba, Japan, 4National Institute of Radiological Science,National Institutes for Quantum and Radiological Science and Technology, Chiba, Japan, 5RISE Project Office, National Astronomical Observatory of Japan, Tokyo, Japan, 6Center for Computational Astrophysics, National Astronomical Observatory, Tokyo, Japan, 7Department of Earth and Space Science, Osaka University, Osaka, Japan, 8MRJ, Kanagawa, Japan, 9Astro-Opt, Tokyo, Japan, 10PTI CO., LTD, 11Crystal Optics Inc., 12MEISEI ELECTRIC CO., LTD, 13DLR, Institute of Planetary Research, Berlin, Germany
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
1Earth Observation Research Center, JAXA, Tsukuba, Japan, 2Faculty of Life and Environmental Sciences, University of Tsukuba, Tsukuba, Japan
2017-q-15p
Development of Next Generation Lithium-Ion Cells for Spacecraft
Makoto Kawase1, Hitoshi Naito1, Yuki Nakajima1, Chisa Yamada1, Masazumi Segawa2, Hiroaki Kusawake1
1Research and Development Directorate, Tsukuba, Japan, 2GS Yuasa Technology Ltd, Kyoto, Japan
2017-q-16p
A Primary Study of Windmill Structure for Planetary Exploration
Kanata Ogiso1, Hideto Mashidori2
1Toyohashi University of Technology, Toyohashi, Japan, 2Tokyo Metropolitan College of Industrial Technology, Tokyo, Japan
2017-q-17p
Pseudo-Resonator Method for Power Delivery through Metal Barriers based on Magnetic Resonance Coupling
Keisuke Ohno, Kohei Shimamura, Shigeru Yokota
Department of Engineering Mechanics and Energy, University of Tsukuba, Ibaraki, Japan
2017-q-18p
Wireless Power Transmission for the Small Space Satellite via Magnetic Resonant Coupling
Naoki Kuwabara, Keisuke Ohno, Kohei Shimamura, Shigeru Yokota
Department of Engineering Mechanics and Energy, The University of Tsukuba, Ibaraki, Japan
2017-q-19p
A 94 GHz Rectifier and a Waveguide-to-microstrip Transducer Development Towards Wireless Power Transmission
Kosumo Matsui1, Waku Hatakeyama1, Kohei Shimamura2, Yuki Okamoto3, Ayako Mizushima4, Hiroyuki Koizumi1, Kimiya Komurasaki1
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Department of Engineering Mechanics and Energy, University of Tsukuba, Ibaraki, Japan, 3Department of Electrical Engineering and Information Systems, the University of Tokyo, Tokyo, Japan, 4VLSI Design and Education Center (VDEC), the University of Tokyo, Tokyo, Japan
2017-r-60p
Unfolding Analysis for Space Webs with Pseudo-flexural Elements
Chen Qingquan, Zhang Qingbin, Tang Qiangang, Gao Qingyu
College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, China
2017-r-61p
Flexible Joint Arm and End-effector for Space Debris Capture
Shin-Ichiro Nishida, Daisuke Uenaka, Atsufumi Shimizu, Shintaro Nakatani
Tottori University, Tottori, Japan
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 (JAXA), Tsukuba, Japan
2017-r-65p
Graphical Methodology for the Preliminary Design of an Ion-Beam Shepherd Mission
Hodei Urrutxua1, Claudio Bombardelli2
1Astronautics Group, University of Southampton, United Kingdom, 2Space Dynamics Group, Technical University of Madrid, Spain
2017-r-66p
Development of a Retractable Twine Gripper for Debris-Capture
Keisuke Taga, Hiroki Nakanishi, Mitsushige Oda
Dept. of Mechanical engineering, Tokyo Institute of Technology, Tokyo, 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, Melbourne, Australia, 2Department of Aerospace Engineering, Tokyo Metropolitan University, Hino, 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
1National Institute of Technology Akashi College. Advanced Course Department of Mechanical and Electrical System Engineering, Japan, 2Department of Electrical and Computer Engineering, National Institute of Technology Akashi College, Japan
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 Ewang1,2, Horyu IV Team 1, Kazuhiro Toyoda1, Mengu Cho1
1Laboratory of Spacecraft Environment INteraction Engineering (La SEINE), Kyushu Institute of Technology, Japan, 2Department of Research and Development, ARCSSTE-E, O.A.U. Campus Ile-Ife, Osun, Nigeria
2017-r-71p
Measuring 5.8 GHz-band Microwave Emission from Hypervelocity Impacts of Different Combinations of Projectile and Target Materials
Yuki Mando1, Ryouhei Sakamoto2, Eriko Soma3, Ichiro Shiota4, Takayuki Hirai5, Hiroki Kurita6, Masatake Kawada7, Koji Tanaka3
1The Graduate University for Advanced Studies, Sagamihara, Kanagawa, Japan, 2Hosei University, Koganei, Tokyo, Japan, 3The Institute of Space and Astronautical Science, JAXA, Sagamihara, Kanagawa, Japan, 4Kogakuin University, Hachioji, Tokyo, Japan, 5JAXA, Chofu, Tokyo, Japan, 6Shizuoka University, Hamamatsu, Shizuoka, Japan, 7Tokushima University, Tokushima, Tokushima, Japan
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
1R.O.C. Naval Academy, Taiwan, 2CCIT, National Defense University, Taiwan, 3National Chung-Shan Institute of Science and Technology, Taiwan