Curriculum Vitaes

Hajime Yano

  (矢野 創)

Profile Information

Affiliation
Assistant Professor, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
Assistant Professor, Graduate Institute for Advanced Studies, Space and Astronautical Science Program, The Graduate University for Advanced Studies
Guest Associate Professor, Graduate School of System Design Management, Keio University
(Concurrent)Visiting Associate Professor, Institute of Advanced Biosciences
Affiliate Associate Professor, Graduate School of Science and Engineering, Hosei University
Adjunct Lecturer, School of Engineering Department of Space Systems Engineering, Kyushu Institute of Technology
Research Affiliate, Media Lab, Space Exploration Initiative, Massachusetts Institute of Technology
Degree
Ph.D. in Space Sciences(Oct, 1995, University of Kent at Canterbury, United Kingdom)

Researcher number
00321571
ORCID ID
 https://orcid.org/0000-0002-4125-0802
J-GLOBAL ID
200901039611171139
researchmap Member ID
1000292032

External link

Prof. Hajime Yano is a space scientist, professor, and project manager of JAXA/ISAS, Japan, who specializes in solar system exploration science and astrobiology, with an emphasis on sample return missions and space experiments. 

 

As an expert in cosmic dust studies and impact physics for over a quarter of the century, his expertise extends to observational, experimental, analytical, and theoretical works of cosmic dust and space debris, as well as planetary protection and planetary defense.  In particular, he has specialized in in-situ detection and collection of cosmic dust and ultimately sample return missions from their parent bodies such as Stardust, Hayabusa, and Hayabusa-2.

 

Hajime has contributed more than 250 refereed papers as a researcher, a co-investigator, or the principal investigator of about 20 past or ongoing space projects from Japan, Europe, and the United States including LDEF, EuReCa, HST, SFU, Nozomi, Stardust, Hayabusa, Leonid-MAC, SSSAT, IKAROS, Tanpopo, BepiColombo, Hayabusa-2, Tanpopo-2, SpaceSkin, EQUULEUS, DESTINY+, Comet Interceptor, and Gateway.   Through these projects, he has accomplished a number of pioneering works that led to major scientific discoveries and “game-changing” movements in solar system exploration.   Since 2007, Hajime holds and maintains a Project Management Professional (PMP) certification and served as Tanpopo-2 project manager.

 

In the space shuttle era, Hajime established post-flight analysis procedures of micrometeoroid and orbital debris impact signatures on retrieved spacecraft surfaces.  Microscopic analyses of several hundred impacts per spacecraft such as LDEF, EuReCa, and HST revealed their origins and formed a fundamental database for dust environment modeling in near-Earth space. The SFU post-flight analysis formed Japan’s first in-situ measurement database of meteoroids and debris.

 

In 1998-2002, Hajime and his team became the world’s first to use high-definition video imagery for astronomical research and their airborne observation onboard the Leonid MAC mission, which yielded both the faintest influx and organic and volatile spectroscopy of the Leonid meteor storm.  The Leonid MAC mission resulted in a quantum leap of meteor science as a “human mission to comets without going to space, by using the atmosphere as a large dust detector”.

 

Hajime developed and operated a number of new instruments for cosmic dust detection and collection.  The detectors include the Nozomi-MDC and DESTINY+ DDA impact-induced plasma detector/analyzer, the BepiColombo-MDM and Gateway ERSA/LVDM acoustic sensors, and the ALADDIN PVDF detectors onboard SSSAT and IKAROS as well as the CLOTH PVDF integrated within MLI thermal blankets onboard EQUULEUS.  All of them are involved in hypervelocity impact calibration experiments and simulations so Hajime has developed stable shotgun techniques for microparticle impacts with two-stage light gas guns at the University of Kent in the U.K., NASA Johnson Space Center in the U.S.A., and ISAS in Japan.    ALADDIN onboard the world’s first interplanetary solar sail IKAROS deployed a 0.54 m2 detection area of cosmic dust impacts; it is the largest dedicated dust detector in the history of solar system exploration and has yielded the finest structure of dust distribution ever between the Earth and Venus.  Hajime has also collaborated with MIT ISN to upgrade the LIPIT dust accelerator for impact calibrations of space instrumentation.  He is now the science lead of the dust impact bumper for JAXA's B1 spacecraft in the Comet Interceptor mission.

 

Intact capture of meteoroids was attempted by foil stuck or aerogel modules used on LDEF, EuReCa, Stardust, Tanpopo, and Tanpopo-2. Hajime was also involved in the development of an ice-melting dust collection device for Japan’s first Antarctic micrometeorite expedition in 1999.  He is now advancing these experiences for future mission concepts like a sample return from Saturn's ring dust and Enceladus’ icy plume as well as impact ejecta from interstellar objects.

 

Also noted is Hayabusa-1&2’s asteroid surface sampling device that resulted in the world’s first asteroid sample return from Itokawa in 2010 and the second of its kind from Ryugu in 2020.  This impact sampling technique that Hajime and his team developed is a robust system suitable for almost any unknown surface conditions of an airless solid body.  Upon the sampling attempt on Itokawa by the Hayabusa-1, Hajime and his colleagues discovered evidence of granular migration on such a small body, which revolutionized ideas of their surface activities and created a new research field of “microgravity geology”.  As future sample return missions are more inclined to organic and volatile-rich small bodies, he is also contributing in the fields of astrobiology, planetary protection, and microgravity experiments.

 

As an educator, Hajime has given a number of classes and lectures for planetary science, astronautical engineering, and project management in universities and institutes worldwide.  He has supervised dozens of Masters and Ph.D. students as well as domestic interns and international students in the field of solar system science and exploration at ISAS.

 

In the international academic community, Hajime has served leading positions in organizing numerous scientific meetings in the collaboration with COSPAR, IAA, IAU, ISTS, and space agencies.  He was the chair of the inaugural meeting of the International Primitive Body Exploration Working Group (IPEWG) in 2008 and the first Asian vice chair of the COSPAR Planetary Protection Panel (PPP) in 2014-2018.  At present, he is the IAA Academician as well as the secretary of the IAA Space Physical Science Commission.  Since 2022, he has been serving as the Chair of the COSPAR Scientific Commission-B on "Space Studies of the Earth-Moon System, Planets, and Small Bodies of the Solar System".

The main belt carbonaceous (B/Cb) asteroid 1995 WF2 is named 8906 Yano.


Awards

 48

Papers

 319
  • Masatoshi Hirabayashi, Masahiko Hayakawa, Yuya Mimasu, Naru Hirata, Takuya Iwaki, Shunichi Kamata, Kohei Kitazato, Toru Kouyama, Naoya Sakatani, Hajime Yano, Koki Yumoto, Masahiro Fujiwara, Sumito Shimomura, Takanao Saiki, Hiroshi Takeuchi, Eri Tatsumi, Yuichi Tsuda, Yasuhiro Yokota, Makoto Yoshikawa, Satoshi Tanaka
    The Planetary Science Journal, May 1, 2026  
  • Junichiro Nakazawa, Hideo Nagatomo, Hajime Yano
    Physics of Plasmas, 33(4) 043906, Apr 1, 2026  Peer-reviewedLast author
    Hypervelocity impacts generate transient, non-equilibrium plasmas whose ionization degree and energy distribution are critical for understanding micrometeoroid impacts and for engineering applications in space exploration. Previous numerical models have often assumed single-temperature equilibrium or embedded simplified ionization schemes directly into hydrodynamics, limiting their ability to capture the early non-equilibrium plasma state. Here, we employ a radiation-hydrodynamics framework that treats electron and ion temperatures separately and incorporates plasma-specific processes, such as thermal conduction, radiation transport, and electron–ion temperature exchange, directly into the governing equations. Ionization is then evaluated in a dedicated post-processing step with a Thomas–Fermi–based model applied to the realistic non-equilibrium plasma conditions produced by the simulation. The model successfully reproduces experimental trends in charge yield and ion temperature distributions across 20–45 km s⁻¹ impacts of iron projectiles on rhodium targets. The velocity scaling shows excellent consistency, differing by only 1% and 0.5% from P. R. Ratcliff, M. J. Burchell, M. J. Cole, T. W. Murphy, and F. Alladfadi, International Journal of Impact Engineering 20, 663 (1997) and M. J. Burchell, M. J. Cole, J. A. McDonnell, and J. C. Zarnecki, Measurement Science and Technology 10, 41 (1999), respectively. These results demonstrate, for the first time, that the velocity dependence of impact-induced ionization can be quantitatively reproduced within a physically consistent two-temperature framework. By explicitly resolving non-equilibrium plasma physics and incorporating geometric effects, our approach achieves what earlier LTE-based or simplified EOS models could not: a predictive and physically grounded description of impact ionization. This establishes a new modeling framework for interpreting measurable impact signatures in laboratory experiments and for extrapolating hypervelocity impact phenomena to space environments.
  • Hajime Yano, Takeshi Imamura, Shuji Matsuura, Naoya Sakatani, Hiroki Ando, Kazuyoshi Arai, Hajime Kawahara, Naoya Ozaki, Yuhito Shibaike, Kakeru Tokunaga, Atsushi Tomiki, Ryu Funase
    Mar 14, 2026  
  • Kunihiko Nishiizumi, Keisuke Nagao, Marc W. Caffee, Ryuji Okazaki, Jozef Masarik, Hisayoshi Yurimoto, Tomoki Nakamura, Takaaki Noguchi, Hiroshi Naraoka, Hikaru Yabuta, Kanako Sakamoto, Kasumi Yogata, Toru Yada, Shogo Tachibana, Sei-ichiro Watanabe, Yuichi Tsuda, Masanao Abe, Kazuya Kumagai, Akiko Miyazaki, Aiko Nakato, Satoru Nakazawa, Masahiro Nishimura, Tatsuaki Okada, Takanao Saiki, Hirotaka Sawada, Satoshi Tanaka, Tomohiro Usui, Koji Wada, Hajime Yano, Makoto Yoshikawa
    METEORITICS & PLANETARY SCIENCE, 61(4) 565-579, Feb 23, 2026  Peer-reviewed

Misc.

 499

Books and Other Publications

 35

Presentations

 598
  • 矢野創, 田端誠, 河合秀幸, 奥平恭子, 山岸明彦
    Viva Origino, Mar 1, 2008
  • 山岸明彦, 小林憲正, 横堀伸一, 矢野創, 橋本博文, 山下雅道
    Viva Origino, Mar 1, 2008
  • 薮下さやか, 小林憲正, 奥平恭子, 矢野創, 山岸明彦
    Viva Origino, Mar 1, 2008
  • 西田淳一, 藤原謙, 松永三郎, 矢野創, 中谷幸司, 森治
    アストロダイナミクスシンポジウム講演後刷り集(Web), Mar, 2008
  • 三和裕一, 矢野創, 森本睦子, 森治, 川口淳一郎
    アストロダイナミクスシンポジウム講演後刷り集(Web), Mar, 2008
  • 山中富夫, 藤原謙, 前野正樹, 西田淳一, 松永三郎, 矢野創, 中谷幸司, 森治
    アストロダイナミクスシンポジウム講演後刷り集(Web), Mar, 2008
  • 高木靖彦, 長谷川直, 矢野創, 杉田精司, 宮本英昭
    宇宙利用シンポジウム, Mar, 2008
  • 山岸明彦, 横堀伸一, 川口壽太郎, YANG Yinjie, 小林憲正, 薮下さやか, 藤崎健太, 矢野創, 山下雅道, 奥平恭子, 長谷川直, 岸本直子, 橋本博文, 田端誠, 河合秀幸, 中嶋悟, 癸生川陽子, 鈴木彰子, 三田肇, 奈良岡浩, 丸茂克美
    宇宙利用シンポジウム, Mar, 2008
  • Sasaki Sho, Ohashi Hideo, Shibata Hiromi, Iwai Takeo, Nogami Kenichi, Yoshikawa Makoto, Yano Hajime, Hasegawa Sunao, Matsumoto Haruhisa, Fujii Masayuki
    宇宙利用シンポジウム, Mar, 2008, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
    A large area dust detector has been developed for detecting dust and debris particles around the Earth. Plane-parallel impact ionization detectors have been developed and we confirmed their capability of detecting interplanetary and interstellar dust particles.
  • 松永三郎, 野口高明, 矢野創, 藤井裕矩, 真壁輝夫, 真壁輝夫, 三浦弥生, 宮本英昭
    太陽系科学シンポジウム, Mar, 2008
  • 吉川真, 矢野創, 川口淳一郎, BARUCCI M. A, MICHEL P
    日本天文学会年会講演予稿集, Feb 20, 2008
  • Fujiwara Ken, Yamanaka Tomio, Nishida Junichi, Matunaga Saburo, Yano Hajime, Mori Osamu
    Jan 24, 2008
    Laboratory for Space Systems, Tokyo Institute of Technology and JAXA/ISAS have proposed tethered sampling method for future asteroid sample returning mission. The tethered sampling mission consists of three procedures: shooting a tethered sampler, a corer, at a high velocity, penetrating the corer into a surface and collecting soil inside, and reeling in the tether and retrieving the corer and soil. This paper reports a dynamics model of tethered corer and tether deployment experiments. The experiment results show validity of the model and effect of bobbin shapes and projection directions o...
  • 野上謙一, 宮地孝, 岩井岳夫, 柴田裕実, 大橋英雄, 佐々木晶, 南繁行, 武智誠次, 河内祐也, 篠原悠紀, 矢野創, 藤井雅之
    UTNL-R(東京大学大学院工学系研究科原子力専攻), 2008
  • 奥平恭子, 野口高明, 長谷川直, 矢野創, 田端誠, 中村智樹, 山岸明彦
    日本地球化学会年会講演要旨集, 2008, 一般社団法人日本地球化学会
    We report on our hypervelocity capture experiments for sample return missions using silica aerogels as capture media. Since aerogels are excellent thermal insulator, there is a possibility that samples might be thermally altered upon capturing. Thus empirical simulation in the lab is essential for rigorous examination of the captured samples. We fired hydrated phyllosilicate mineral particles which were susceptible to heat into aerogel by using two-stage light gas guns. After extraction from aerogel, several kinds of analyses were given to the samples to evaluate their alteration. We introduce results of our previous studies as well as those of preliminary experiments for TANPOPO mission.
  • 山岸明彦, 矢野創, 小林憲正, 横堀伸一, 河合秀幸, 橋本博文, 山下雅道
    日本地球化学会年会講演要旨集, 2008, 一般社団法人日本地球化学会
    TANPOPO, dandelion, is the name of a grass whose seeds with floss are spread by the wind. We propose the analyses of interplanetary migration of microbes, organic compounds and meteoroids on ISS-JEM. Ultra low-density aerogel will be used to capture micrometeoroid and debris. Particles captured by aerogel will be used for several analyses after the initial inspection of the gel and tracks. Careful analysis of the tracks in the aerogel will provide the size and velocity dependence of debris flux. The particles will be analyzed for mineralogical, organic and microbiological characteristics. To test the survival of microbes in space environment, microbial cells will be exposed. Organic compounds are also exposed to evaluate the possible denaturation under the conditions. Aerogels are ready for production in Japan. Aerogels and trays are space proven. All the analytical techniques are ready.
  • Yano Hajime
    Abstracts of Annual Meeting of the Geochemical Society of Japan, 2008, GEOCHEMICAL SOCIETY OF JAPAN
    test
  • 奥平恭子, 野口高明, 矢野創
    日本惑星科学会誌 遊・星・人, Dec 25, 2007
  • 吉川真, 矢野創, 本間幸子, 森本睦子, 橋本樹明, 久保田孝, 岸晃孝, 國中均, 川口淳一郎, 齋藤潤, 秋山演亮, 寺薗淳也
    日本天文学会年会講演予稿集, Aug 20, 2007
  • 阿部新助, 山本真行, 矢野創, 海老塚昇, 渡部潤一, 向井正
    太陽系科学シンポジウム, Jun, 2007
  • 小林憲正, 三田肇, 石川洋二, 山岸明彦, 内海裕一, 山下雅道, 奥平恭子, 高橋淳一, 河崎行繁, 癸生川陽子, 小池惇平, 鈴木彰子, 長沼毅, 杉浦桂, 奈良岡浩, 加藤政博, 橋本博文, 小林克己, 丸茂克美, 矢野創
    宇宙利用シンポジウム, Mar, 2007
  • 高木靖彦, 長谷川直, 矢野創, 寺元啓介, 山本聡, 杉田精司, 黒澤耕介, 仲田哲進, 本田親寿, 安部正真, 藤原顯
    宇宙利用シンポジウム, Mar, 2007
  • YOSHIKAWA Makoto, KOMINATO Takashi, MATSUOKA Masatoshi, SHIRAKAWA Ken’ichi, IKEDA Hitoshi, IKEDA Hitoshi, OHNISHI Takafumi, ABE Shinsuke, MUKAI Tadashi, YANO Hajime, SCHEERES Daniel, GASKELL Robert, SAITO Jun, KUBOTA Takashi, HASHIMOTO Tatsuaki, FUJIWARA Akira, KAWAGUCHI Jun’ichiro
    アストロダイナミクスシンポジウム講演後刷り集, Mar, 2007
  • NAKAYA Koji, MORI Osamu, YANO Hajime, MATUNAGA Saburo
    アストロダイナミクスシンポジウム講演後刷り集, Mar, 2007
  • OTSUKI Masatsugu, KUBOTA Takashi, BANDO Nobutaka, YANO Hajime, HIGUCHI Ken, UO Masashi, HASHIMOTO Tatsuaki
    アストロダイナミクスシンポジウム講演後刷り集, Mar, 2007
  • 吉川真, 矢野創, 本間幸子, 森本睦子, 橋本樹明, 久保田孝, 岸晃孝, 國中均, 森治, 小野瀬直美, 周東三和子, 浅野眞, 川口淳一郎, 齋藤潤, 秋山演亮, 出村裕英, 寺薗淳也, 吉住千亜紀, 尾久土正己
    宇宙科学技術連合講演会講演集(CD-ROM), 2007
  • 松永三郎, 藤原謙, 山中富夫, 前野正樹, 西田淳一, 矢野創, 中谷幸司, 森治
    宇宙科学技術連合講演会講演集(CD-ROM), 2007
  • 松永三郎, 西田淳一, 藤原謙, 中谷幸司, 矢野創, 森治
    構造強度に関する講演会講演集, 2007
  • 横田沙会子, 草川靖大, 土谷健一郎, 千葉竜太朗, 吉川信, 矢野創, 秋山演亮
    宇宙科学技術連合講演会講演集(CD-ROM), 2007
  • 矢野創, 野口高明, 真壁輝夫, 真壁輝夫, 樋口健, 松永三郎, 藤井裕矩, 三浦弥生
    日本惑星科学会秋季講演会予稿集, 2007, 日本惑星科学会
    In the Primitive Body Exploration Program of Japan, we are aiming for sample return missions, by following the Hayabusa's heritage, from surfaces and potentially sub-surfaces of C-type asteroids and CAT objects or D-type asteroids within the next decade. Thus we are currently developing new sampling systems suitable for such targets. In particular, the impact sampling system with corer projectiles and a microgravity tether retraction system as well as tape tether mechanism are evaluated in the microgravity condition. This study summarizes results of those endeavors and future prospects of this challenge.
  • 横堀伸一, 山岸明彦, 川口寿太郎, Yang Yinjie, 奥平恭子, 矢野創, 小林憲正, 丸茂克美, 山下雅道
    平成18年度スペース・プラズマ研究会報告, 2007
  • J. C. Liou, F. J. Giovane, R. D. Corsaro, M. J. Burchell, G. Drolshagen, H. Kawai, M. Tabata, E. G. Stansbery, A. J. Westphal, H. Yano
    AIAA 57th International Astronautical Congress, IAC 2006, Dec 1, 2006
    To improve the near-Earth meteoroid and orbital debris environment definition, a large area particle sensor/collector is being developed to be placed on the International Space Station (ISS). This instrument, the Large Area Debris Collector (LAD-C), will attempt to record meteoroid and orbital debris impact flux, and capture the same particles with aerogel. After at least one year of deployment, the whole system will be brought back for additional laboratory analysis of the captured meteoroids and orbital debris. This project is led by the U.S. Naval Research Laboratory (NRL) while the U.S. Department of Defense (DoD) Space Test Program (STP) is responsible for the integration, deployment, and retrieval of the system. Additional contributing team members of the consortium include the NASA Orbital Debris Program Office, JAXA Institute of Space and Astronautical Science (ISAS), Chiba University (Japan), ESA Space Debris Office, University of Kent (UK), and University of California at Berkeley. The deployment of LAD-C on the ISS is planned for 2008, with the system retrieval in late 2009.
  • Takashi Kubota, Takashi Kubota, Takashi Kubota, Masatsugu Otsuki, Masatsugu Otsuki, Tatsuaki Hashimoto, Tatsuaki Hashimoto, Tatsuaki Hashimoto, Nobutaka Bando, Nobutaka Bando, Hajime Yano, Hajime Yano, Masashi Uo, Masashi Uo, Ken'ichi Shirakawa, Ken'ichi Shirakawa, Ken'ichi Shirakawa, Jun'ichiro Kawaguchi, Jun'ichiro Kawaguchi, Jun'ichiro Kawaguchi
    Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006, Dec 1, 2006
    Hayabusa spacecraft performed the final descents and touchdowns twice in November 2005. In final descent phase, terrain alignment maneuvers were accomplished to control both altitude and attitude with respect to the surface by using four beams Laser Range Finder onboard. Then Hayabusa spacecraft made dynamic touchdowns the surface of the asteroid by the sampler system to collect samples automatically. This paper presents the terrain alignment maneuver and touchdown scheme. This paper also describes the novel sample horn system and touchdown dynamics. Touchdown tests on the ground are presented. Then the flight results on touchdown dynamics are shown and discussed. Copyright © 2006 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
  • M. Yoshikawa, M. Yoshikawa, H. Ikeda, H. Yano, J. Saito, T. Kubota, T. Hashimoto, A. Fujiwara, J. Kawaguchi, T. Kominato, M. Matsuoka, K. Shirakawa, T. Ohnishi, S. Abe, T. Mukai, R. Gaskell, D. Scheeres
    Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006, Dec 1, 2006
    Hayabusa was moving near Asteroid Itokawa for about three months in 2005. Using tracking and navigation data such as range, Boppler, distance from the asteroid, and optical images taken by navigation cameras, we estimated the mass of Itokawa for several orbital phases. The results are consistent in their error ranges. The estimated mass of Itokawa is 3.51 ± 0.105 (1010kg), from which the density of Itokawa is derived as 1.9 ± 0.13 (g/cm3). This is one of the important characteristics to understand the nature of Itokawa. We are also trying to investigate the accuracy of the ephemeris of this asteroid. Copyright © 2006 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
  • Takashi Kubota, Masatsugu Otsuki, Hajime Yano, Tatsuaki Hashimoto, Nobutaka Bando, Makoto Tamura, Masashi Uo, Ken'ichi Shirakawa, Jun'ichiro Kawaguchi
    AIAA 57th International Astronautical Congress, IAC 2006, Dec 1, 2006
    Hayabusa spacecraft performed the final descents and touchdowns twice in November 2005. In final descent phase, terrain alignment maneuvers were accomplished to control both altitude and attitude with respect to the surface by using four beams Laser Range Finder onboard. Then Hayabusa spacecraft made dynamic touchdowns the surface of the asteroid by the sampler system to collect samples automatically. This paper presents the terrain alignment maneuver and touchdown scheme. This paper also describes the novel sample horn system and touchdown dynamics. Touchdown tests on the ground are presented. Then the flight results on descent and touchdown dynamics are shown and discussed.
  • 野口高明, 土山明, 平田成, 中村良介, 宮本英昭, 出村裕英, 矢野創, 中村智樹, 齋藤潤, 佐々木晶, 橋本樹明, 久保田孝, 石黒正晃, ZOLENSKY M
    形の科学会誌, Oct, 2006
  • 吉川真, 矢野創, 安部正真, 岩田隆浩, 川勝康弘, 田中智, 森治, 吉光徹雄, 藤原顕, 川口淳一郎, 高木靖彦, 出村裕英, 野口高明, 宮本英昭
    日本天文学会年会講演予稿集, Aug 20, 2006
  • 矢野創, 安部正真, 藤原顕
    太陽系科学シンポジウム, Mar, 2006
  • TANAKA Satoshi, KOBAYSHI Naoki, YANO Hajime, FUJIMURA Akio
    Proc ISAS Lunar Planet Symp (Inst Space Astronaut Sci), Mar, 2006
  • UENO Munetaka, ISHIGURO Masateru, USUI Fumihiko, YANO Hajime, IMAMURA Takeshi, NAKAMURA Masato, SATOH Takehiko, KIMATA Masafumi
    Proc ISAS Lunar Planet Symp (Inst Space Astronaut Sci), Mar, 2006
  • Okudaira Kyoko, Yano Hajime, Onose Naomi, Hasegawa Sunao
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2006, THE JAPANESE SOCIETY FOR PLANETARY SCIENCES
    Silica aerogel has been used as a suitable capture medium for solid microparticles with hypervelocity. The authors have been conducting experiments for evaluation of thermal alteration of particles captured by silica aerogel and energy partition. In this study, formation of penetration tracks in aerogel was observed and recorded by a high-speed camera. Excavation process of a single track, so-called a "carrot track" made by a 500 micron-Al<SUB>2</SUB>O<SUB>3</SUB> grain was observed. At first a thin track grew in the direction of penetration and then it started to swell into a "carrot". Assuming that brighter part represents higher temperature/pressure area, shock wave dissipation in aerogel can be recognized. Combining this and our previous results, this study aims at finding empirical facts constraining energy partition.
  • Yoshikawa Makoto, Yoshimitsu Tetsuo, Takagi Yasuhiko, Demura Hirohide, Noguchi Takaaki, Miyamoto Hideaki, Kawaguchi Jun'ichiro, Fujiwara Akira, Abe Masanao, Iwata Tkahiro, Kawakatsu Yasuhiro, Tanaka Satoshi, Mori Osamu, Yano Hajime
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2006, THE JAPANESE SOCIETY FOR PLANETARY SCIENCES
    The observation of Asteroid Itokawa by Hayabusa spacecraft has brought us a lot of new knowledge for very small (about 500m in length) S-type asteroid. We already have started to consider next space mission to small bodies in the solar system. For the next asteroid mission, we would like to explore C-type asteroid, which is also major type in the asteroid belt. This type of asteroid is supposed to have organic matter or water more than S-type asteroid, and it is important to study the material related to life. In this paper, we present the current plan for the next exploration to asteroids. We also want to encourage many researchers to join our asteroid mission.
  • Takagi Yasuhiko, Abe Masanao, Hasegawa Sunao, Yano Hajime, Yamamoto Satoru, Sugita Seiji, Teramoto Keisuke, Kurosawa Kousuke, Nakata Tesshin, Honda Chikatoshi
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2006, THE JAPANESE SOCIETY FOR PLANETARY SCIENCES
    Impact cratering experiments in microgravity environment were performed using a drop tower. The results showed no gravity effect. Details of experimental procedures and results will be presented at the session.
  • 矢野創, 藤原顕, 長谷川直, 安部正真, 高山和喜, 吉田和哉, 高木靖彦, 土屋和雄, 花田俊也, 八坂哲雄
    宇宙科学技術連合講演会講演集(CD-ROM), 2006
  • Miyamoto Hideaki, Yano Hajime, Sasaki Shou, Demura Hirohide, Hirata Naru, Ishiguro Masaaki, Michikami Tatsuhiro, Nakamura Akiko, Nakamura Ryousuke, Saito Jun
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2006, THE JAPANESE SOCIETY FOR PLANETARY SCIENCES
    In November, 2005, the Hayabusa spacecraft successfully touch-downed at the smooth terrain of the asteroid, Itokawa, whose longest axis is as small as ~500m. At the decent phase for the touch down and its rehearsals, more than 30 unprecedentedly high-resolution images are obtained at different locations/areas of Itokawa. The widths of some of these images are too narrow, which required significant effort in estimating their exact locations. In this talk, we will report how we rectified these images into low-resolution images and briefly discuss geological characteristics apparent on these images.
  • 阿部新助, 山本真行, 矢野創, 海老塚昇, 渡部潤一, 向井正
    日本惑星科学会秋季講演会予稿集, 2006, 日本惑星科学会
    On the night of January 15 2006, Stardust Reentry Capsule observing campaing was carried out using imagers and spectrographs onboad NASA's airbone DC-8. In order to understand physical processes occuring in natural meteors and meteorites, we performed spectroscopy using an intensified high-definition TV observation with a reflection grating 500 grooves/mm in the wavelength between 300 and 650 nm. The capsule, 0.8 m in diameter, entered the atmosphere by the speed of 12.9 km/s, which was the fastest artificial objects in our history.
  • 中村良介, 中村昭子, 平田成, 阿部新助, 石黒正晃, 矢野創
    日本惑星科学会秋季講演会予稿集, 2006, 日本惑星科学会
    Japanese Asteroid Explorer Hayabusa completed the surface mapping of the target S-type asteroid Itokawa during the rendez-vous phase between September and November in 2005. Furthermore, Hayabusa obtained several very high-resolution images during the descent to the surface for capturing surface sample materials. On these high resolution images , we have found several bright dots of a few centimeter size on boulders darkened by space-weathering. The bright dots are likely to be small craters produced by the hypervelocity impacts of meteoroids. We present the preliminary counting results of such small craters and discuss the implication on the meteoroids flux, timescale of space weathering and resurfacing on Itokawa.
  • TAKAGI Yasuhiko, YANO Hajime
    Proc ISAS Lunar Planet Symp (CD-ROM), 2006
  • T. Miyachi, M. Fujii, N. Hasebe, G. Kuraza, K. Nogami, T. Iwai, S. Sasaki, H. Ohashi, S. Hasegawa, H. Yano, H. Shibata, E. Grün, R. Srama, N. Okada, T. Tou
    IEEE Nuclear Science Symposium Conference Record, Dec 1, 2005
    Hypervelocity collisions of microparticles with a lead-zirconate-titanate piezoelectric element are examined. The waveforms thus obtained depend on the velocities during collision, and are classified into three categories. In particular, the first cycle of the signal observed immediately after collision is essential to obtain information on the impact. In each category, experimental formulas that are functions of the impact velocity are established based on experimental data. It is concluded that a single piezoelectric element can potentially measure the velocity and/or momentum of hypervelocity microparticles in real time. In the abovementioned context, the new dust detectors are described. © 2005 IEEE.
  • S. Diniega, H. Yano, D. Scheeres
    International Astronautical Federation - 56th International Astronautical Congress 2005, Dec 1, 2005
    We used analyses and simulation, based on pre-Hayabusa encounter models, to determine the possible distribution of regolith on 25143 Itokawa. Current knowledge was drawn from many studies about cratering dynamics in the strength regime and in porous material, ejecta velocity distributions, and 25143 Itokawa's probable interior structure. Based on all of this, it has been shown that this asteroid should not have a deep, global regolith layer like that found on 433 Eros. Instead, small and thin (millimeters to centimeters) patches of regolith will probably be found near the source craters. However, this study does not take into account secondary processes which can redistribute and size-sort regolith. Finally, the types of observations and analyses of 25143 Itokawa which would be most useful in constraining future studies, and in estimating the influence of secondary processes, are outlined. The current paper does not make any observations about 25143 Itokawa based on the new mission data, reserving such analysis for later studies.
  • M. Tabata, I. Adachi, T. Fukushima, H. Kawai, H. Kishimoto, A. Kuratani, H. Nakayama, S. Nishida, T. Noguchi, K. Okudaira, Y. Tajima, H. Yano, H. Yokogawa, H. Yoshida
    IEEE Nuclear Science Symposium Conference Record, Dec 1, 2005
    New production methods of silica aerogel with high and low refractive indices have been developed. A very slow shrinkage of alcogel at room temperature has made possible producing aerogel with high refractive indices of up to 1.265 without cracks. Even higher refractive indices than 1.08, the transmission length of the aerogel obtained from this technique has been measured to be about 10 to 20 mm at 400 nm wave length. A mold made of alcogel which endures shrinkage in the supercritical drying process has provided aerogel with the extremely low density of 0.009g/cm3, which corresponds to the refractive index of 1.002. We have succeeded producing aerogel with a wide range of densities. © 2005 IEEE.

Teaching Experience

 5

Research Projects

 43

Industrial Property Rights

 8

Academic Activities

 24
  • Planning, Management, etc., Panel moderator, Session chair, etc., Supervision (editorial)
    Committee of Space Research (COSPAR) (Yokohama, Kanagawa, japan), Aug 8, 2026 - Present
  • Planning, Management, etc., Panel moderator, Session chair, etc., Supervision (editorial), Review, evaluation
    OPENS-0 Pre-Project Preparation Team, JAXA/ISAS (JAXA/ISAS (Online)), Apr, 2025 - Present
    Scopes: Aiming to be launched in the late 2020s, the OPENS-0 is an engineering demonstration mission of key enabling technologies for a 100-kg class spacecraft to independently explore the outer planet region, e.g., Saturn's ring flyby. Inevitably, the spacecraft is limited in its resources and operational capabilities compared to legacy spacecraft. Thus, the OPENS-0 is designed to maximize its scientific output by employing "multi-purpose" instruments such as optical navigation cameras for observing zodiacal light, main belt asteroid morphology, and Saturn's ring structure. It is also planned to use the ultra-stable oscillator and deep space transponder for radio occultation of the solar flare, the planetary atmospheres, and Saturn's ring, as well as the PVDF-layered MLI for micrometeoroid flux at 1-10 AU heliocentric distance and dust structure in the vicinity of Saturn's ring. This workshop is aimed at the following three scopes. (1) The workshop will present the mission concept and its potential scientific opportunities of the OPENS-0 to the international science community at the earliest stage of the mission formulation. (2) The solicited talks will review outcomes from the cruising science investigations conducted by past and present deep space missions to provide lessons learned and remaining scientific challenges for the OPENS-0 mission. (3) The OPENS-0 team will identify potential candidates for the future OPENS-0 international science team among the participants who express their interest in joining the mission.
  • Supervision (editorial), Peer review, Others
    新興出版社啓林館, Jul, 2017 - Present
  • Planning, Management, etc., Panel moderator, Session chair, etc., Peer review
    International Academy of Astronautics (IAA), Apr, 2017 - Present
  • Planning, Management, etc., Panel moderator, Session chair, etc., Supervision (editorial), Review, evaluation
    Mar 2, 2026 - Mar 4, 2026

Social Activities

 3

Media Coverage

 98
  • 日本学術会議, 代表派遣会議出席報告, 国際活動, Apr, 2026 Internet
    2026年3月15日~17日、COSPAR運営に関する科学的知見からのアドバイス、8月開催予定総会のプログラム編成の確定、2027年、2029年開催のシンポジウムのテーマ・候補地に関する議論、COSPAR独自の宇宙探査ロードマップに関する討議等。
  • 公益財団法人AFS日本協会, AFS日本協会, AFS日本協会>AFSからのお知らせ>AFS活動レポート, Mar 10, 2026 Internet
    2026年2月14日-15日、東京・代々木のオリンピックセンターにて、日本各地で活動するAFSボランティアを対象とした「全国ボランティア大会」が開催されました。ボランティア大会はボランティア自身が企画、運営している集まりです。ボランティアがそれぞれの体験や学びを共有しあい、互いを高め合うため、2年に1回開催されています。2026年のテーマは「ミライを描こう~AFSの魅力は無限大∞~」です。全国各地から約170人のAFSボランティアが集まりました。
  • Interesting Engineering, Interesting Engineering, Space, Feb 13, 2026 Internet
    The algorithm scanned a 5×5-kilometer area in the Oceanus Procellarum region, identifying several spots exhibiting “artificial soil disturbances.”
  • Euro Weekly News, Euro Weekly News, World News, Feb 12, 2026 Internet
    British-led researchers believe they may have identified the long-lost landing site of Luna 9, the Soviet spacecraft that became the first human-made object to achieve a soft landing on the Moon in 1966. Using artificial intelligence to analyse high-resolution lunar imagery, the team has reported several “high-confidence detections of artificial objects” in a specific region of the Moon’s surface.
  • NDTV, NDTV, Science, Feb 12, 2026 Internet
    While the findings are promising, they are not yet definitive proof of Luna 9's location.

Other

 10

教育内容やその他の工夫

 1
  • Date(From)
    2012/04/01
    Subjcet
    LABAM: Laboratory for Astrobiology and Astromaterial
    Summary
    研究室理念: 宇宙塵をキーワードとする宇宙探査・実験によって可能となるアストロバイオロジーと地球外物質研究を融合して、惑星系、地球型惑星、生命の起源と進化を実証的に解明することを目指すとともに、近隣の学際研究への応用・連携を通じて人類社会の持続的なフロンティア拡大に貢献する。

その他教育活動上特記すべき事項

 10
  • Date(From)
    2023/04
    Subjcet
    総合研究大学院大学・先端学術院・宇宙科学コース(併任)
    Summary
    助教:矢野創
    (継続中)
  • Date(From)
    2019/04
    Subjcet
    九州工業大学 工学部宇宙システム工学科 (兼任)
    Summary
    非常勤講師:矢野創
    (継続中)
  • Date(From)
    2019/04
    Subjcet
    慶応義塾大学 先端生命科学研究所(兼任)
    Summary
    訪問准教授: 矢野創
    (継続中)
  • Date(From)
    2017/04
    Date(To)
    2020/03
    Subjcet
    東京大学大学院 工学系研究科航空宇宙工学専攻(兼任)
    Summary
    非常勤講師:矢野創
  • Date(From)
    2016/04
    Subjcet
    法政大学大学院 理工学研究科(併任)
    Summary
    連携准教授: 矢野創
    JAXA-法政大学連携大学院協定に基づく。(継続中)
    2016-2023年は客員准教授。
  • Date(From)
    2012/04
    Subjcet
    JAXA宇宙科学研究所・学際科学研究系・宇宙生命物質科学研究室(本務)
    Summary
    助教:矢野創
    (継続中)
  • Date(From)
    2010/09
    Subjcet
    慶応義塾大学大学院 システムデザインマネジメント研究科(兼任)
    Summary
    特別招聘准教授: 矢野創
    (継続中)
  • Date(From)
    2003/10
    Date(To)
    2023/03
    Subjcet
    総合研究大学院大学・物理科学研究科・宇宙科学専攻(併任)
    Summary
    助教: 矢野創
  • Date(From)
    2003/10
    Date(To)
    2012/03
    Subjcet
    JAXA宇宙科学研究所・太陽系科学研究系(本務)
    Summary
    助教:矢野創
  • Date(From)
    1999/05
    Date(To)
    2003/09
    Subjcet
    文部科学省宇宙科学研究所・惑星科学研究系(本務)
    Summary
    教授: 藤原顕
    助手: 安部正真、矢野創

● 指導学生等の数

 9
  • Fiscal Year
    2026年度(FY2026)
    Doctoral program
    1
    Master’s program
    5
    Students under Cooperative Graduate School System
    5
    Students under Commissioned Guidance Student System
    1
    Students under Skills Acquisition System
    4
  • Fiscal Year
    2025年度(FY2025)
    Doctoral program
    1
    Master’s program
    6
    Students under Cooperative Graduate School System
    6
    Students under Skills Acquisition System
    2
    JSPS Research Fellowship (Young Scientists)
    1
  • Fiscal Year
    2024年度(FY2024)
    Doctoral program
    1
    Master’s program
    5
    Students under Cooperative Graduate School System
    5
    Students under Skills Acquisition System
    3
    Internship students
    1
    JSPS Research Fellowship (Young Scientists)
    1
    Others
    インターンは総研大国際オリエンテーション制度による留学生(イタリア/スウェーデン)
  • Fiscal Year
    2023年度(FY2023)
    Doctoral program
    1
    Master’s program
    3
    Students under Cooperative Graduate School System
    3
    Students under Skills Acquisition System
    3
    JSPS Research Fellowship (Young Scientists)
    1
    Others
    留学生: 1
  • Fiscal Year
    2022年度(FY2022)
    Doctoral program
    1
    Master’s program
    2
    Students under Cooperative Graduate School System
    2
    Students under Skills Acquisition System
    2
  • Fiscal Year
    2021年度(FY2021)
    Doctoral program
    1
    Master’s program
    3
    Students under Cooperative Graduate School System
    3
    Students under Skills Acquisition System
    1
  • Fiscal Year
    2020年度(FY2020)
    Master’s program
    5
    Students under Cooperative Graduate School System
    5
    Students under Skills Acquisition System
    1
  • Fiscal Year
    2019年度(FY2019)
    Master’s program
    6
    Students under Cooperative Graduate School System
    6
    Students under Skills Acquisition System
    2
  • Fiscal Year
    2018年度(FY2018)
    Master’s program
    5
    Students under Cooperative Graduate School System
    5
    Students under Skills Acquisition System
    2
    Others
    留学生:1

● 指導学生の表彰・受賞

 8
  • Student Name
    中澤淳一郎
    Student affiliation
    総合研究大学院大学
    Award
    日本学術振興会若手研究者海外挑戦プログラム
    Date
    2025年3月-8月
  • Student Name
    中澤淳一郎
    Student affiliation
    総合研究大学院大学
    Award
    総合研究大学院大学研究派遣プログラム
    Date
    2025年2月ー3月
  • Student Name
    中澤淳一郎
    Student affiliation
    総合研究大学院大学
    Award
    トビタテ留学日本代表プログラム
    Date
    2025年2月-2026年3月
  • Student Name
    中澤淳一郎
    Student affiliation
    総合研究大学院大学
    Award
    第32回衛星設計コンテスト・アイデア大賞「氷衛星への超小型衝突探査機ICICLEs」
    Date
    2024年11月
  • Student Name
    中澤淳一郎
    Student affiliation
    総合研究大学院大学
    Award
    日本学術振興会特別研究員(DC)
    Date
    2023年4月-2026年3月
  • Student Name
    中澤淳一郎
    Student affiliation
    総合研究大学院大学
    Award
    帝人久村奨学金授与、公益財団法人帝人奨学会
    Date
    2023年4月
  • Student Name
    中澤淳一郎
    Student affiliation
    総合研究大学院大学
    Award
    帝人久村奨学金授与、公益財団法人帝人奨学会
    Date
    2021年6月
  • Student Name
    芹澤遼太
    Student affiliation
    法政大学大学院(ISAS連携大学院生)
    Award
    COSPAR Student Travel Grant Award、COSPAR, 彗星サンプルリターンを目指したCNT微粒子捕集材の実験的研究と数値解析による形状設計
    Date
    2020年7月

● 指導学生の顕著な論文

 29
  • Student name
    Junichiro NAKAZAWA
    Student affiliation
    SOKENDAI (Graduate University of Advanced Studies)
    Author(s), journal, volume number, pagination (year of publication)
    Ph.D. Thesis
    Title
    Mass Spectrometry Techniques for Sublimated Gas from Organic-Bearing Microparticles by Hypervelocity Impacts
  • Student name
    増地 大陸
    Student affiliation
    法政大学大学院理工学研究科(JAXA/ISAS連携大学院)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2026)
    Title
    月周回有人拠点Gatewayに搭載されるダスト検出器LVDMにおける極低速衝突粒子の粒径および速度の推定
  • Student name
    伊藤 海音
    Student affiliation
    法政大学大学院理工学研究科(JAXA/ISAS連携大学院)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2026)
    Title
    ポリイミドフォームを用いた複合バンパーシールドからの衝突破片放出の抑制
  • Student name
    Seira MOROZUMI
    Student affiliation
    法政大学大学院理工学研究科(JAXA/ISAS連携大学院)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2025)
    Title
    原子状酸素が存在するISSきぼう曝露部の垂直配向カーボンナノチューブによる低速衝突物の捕集性能と捕集物の調査
  • Student name
    Ryoya SANO
    Student affiliation
    法政大学大学院理工学研究科(JAXA/ISAS連携大学院)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2025)
    Title
    スペースデブリ防御バンパーにおけるAl合金およびAFRP中間材の比較検討
  • Student name
    Gaia Lucrezia DALLA PRIA
    Student affiliation
    Lulea University of Technology, Sweden
    Author(s), journal, volume number, pagination (year of publication)
    Special Assignment in Space Science and Technology as a Part of Master's Degree (2025)
    Title
    Microscopic Analysis of Low-velocity Impact Signatures on the Tanpopo-2 Aerogel Panels and Possible Origin
  • Student name
    Shoya IWATA
    Student affiliation
    法政大学大学院理工学研究科(JAXA/ISAS連携大学院)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2024)
    Title
    Smart MLI宇宙実証機の地上校正による有効性検証と地球―月圏ダスト分布計測
  • Student name
    Simon MAILLOT
    Student affiliation
    仏・高等科学技術学院(IPSA)
    Author(s), journal, volume number, pagination (year of publication)
    Engineering-level Internship Report as a Partial Filfullment of the MEng. Degree(2023)
    Title
    Modelling of Hypervelocity Impact Microparticle Environment for the EQUULEUS Mission
  • Student name
    中澤 淳一郎
    Student affiliation
    総合研究大学院大学
    Author(s), journal, volume number, pagination (year of publication)
    特別研究I・修士論文相当(2023)
    Title
    固体微粒子の超高速衝突により生じる破砕・昇華・電離物質の包括的な捕集システムの開発
  • Student name
    和久井 穀貴
    Student affiliation
    法政大学大学院理工学研究科(連携大学院生)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2023)
    Title
    たんぽぽ プロジェクト 1 および 2 の捕集パネルから 導く微粒子の衝突エネルギ推定と経年変化
  • Student name
    Kota ISAWA
    Student affiliation
    法政大学大学院理工学研究科(JAXA/ISAS連携大学院)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2022)
    Title
    エアロゲルによる宇宙固体微粒子の衝突捕集に関する実験および数値解析
  • Student name
    Yuki TAKEDA
    Student affiliation
    法政大学大学院理工学研究科(JAXA/ISAS連携大学院)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2022)
    Title
    宇宙往還した垂直配向カーボンナノチューブによる低速衝突不定形粒子の捕集
  • Student name
    Ryota SERIZAWA
    Student affiliation
    法政大学大学院理工学研究科(JAXA/ISAS連携大学院)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2021)
    Title
    彗星サンプルリターンを目指したCNT微粒子捕集材の実験的研究と数値解析による形状設計
  • Student name
    Kosuke KANDO
    Student affiliation
    法政大学大学院理工学研究科(JAXA/ISAS連携大学院)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2021)
    Title
    宇宙科学研究に向けたレーザー励起微粒子衝突実験装置射出部の最適化
  • Student name
    Erika MINAKAMI
    Student affiliation
    法政大学大学院理工学研究科(JAXA/ISAS連携大学院)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2021)
    Title
    微粒子環境モデルの更新に向けたたんぽぽ捕集パネル 構造部上の衝突痕分析
  • Student name
    Keita YAMAMOTO
    Student affiliation
    法政大学大学院理工学研究科(JAXA/ISAS連携大学院)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2020)
    Title
    ISSに搭載されたエアロゲル捕集材による超高速微粒子衝突頻度の経年変化に及ぼす二次イジェクタと遮蔽効果の影響
  • Student name
    Shuto OIZUMI
    Student affiliation
    法政大学大学院理工学研究科(JAXA/ISAS連携大学院)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2020)
    Title
    彗星ランデブーサンプルリターンを目指した垂直配向カーボンナノチューブの微粒子捕集性能の評価
  • Student name
    Haruki NAKANO
    Student affiliation
    法政大学大学院理工学研究科(JAXA/ISAS連携大学院)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2020)
    Title
    圧電性薄膜センサに衝突した微粒子の質量推定のための出力信号周波数分析
  • Student name
    Maximilian EITEL
    Student affiliation
    独・シュトッツガルト大学院
    Author(s), journal, volume number, pagination (year of publication)
    技術研修報告書(2019)
    Title
    Tanpopo Particle Impact Analysis
  • Student name
    Eigo ISHIKAWA
    Student affiliation
    法政大学大学院理工学研究科(JAXA/ISAS連携大学院)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2019)
    Title
    小天体ランデブーミッションに向けた低中速衝突ダストの検出回路の開発

● 専任大学名

 1
  • Affiliation (university)
    総合研究大学院大学(SOKENDAI)

● 所属する所内委員会

 4
  • ISAS Committee
    2025年12月-現在 高頻度宇宙科学実験プログラム検討タスクフォース・委員
  • ISAS Committee
    2023年6月-現在 科学データ利用委員会・委員
  • ISAS Committee
    2016年12月 - 2018年12月 宇宙理工学合同委員会下・宇宙科学の今後20年の構想を検討する委員会・委員
  • ISAS Committee
    2006年4月 - 2019年3月 大学共同利用スペースプラズマ(現・超高速衝突実験)専門委員会・委員