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

 318
  • 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
  • Lewis J. Pinault, Ian A. Crawford, Hajime Yano
    npj Space Exploration, 2(1), Jan 21, 2026  Peer-reviewedLast author
    Detecting and cataloguing spacecraft hardware on the lunar surface remains challenging even after six decades of exploration. We present a lightweight computer vision system, YOLO-ETA (You-Only-Look-Once – Extraterrestrial Artefact), adapted from TinyYOLOv2 for identifying anthropogenic objects in high-resolution Lunar Reconnaissance Orbiter Camera (LROC) imagery. Trained on Apollo landing-site data, YOLO-ETA achieved balanced precision–recall (F1 ≈ 0.60) and an 80% mean confidence score for lander detections in previously unseen images and correctly localised the Luna 16 spacecraft. Applying the model to a 5 × 5 km region surrounding the historically uncertain Luna 9 landing area yielded several high-confidence detections of artificial objects near 7.03° N, –64.33° E. Topographic analysis indicates that the candidate site’s horizon geometry is potentially consistent with Luna 9 surface panoramas. These findings identify promising locations for follow-up imaging and demonstrate that compact, edge-deployable machine-learning models can support future orbital surveys of lunar artefacts and surface assets.

Misc.

 498
  • Yano Hajime, Noguchi Takaaki, Makabe Teruo, Higuchi Ken, Matsunaga Saburo, Fujii Hironori, Miura Yayoi, MinorbodyExploration WG-Sampling SG
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2007 108-108, 2007  
    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), 51st 3J06, 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, 49th 169-171, 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), 51st 3D07, 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), 51st 3J05, 2007  
  • Takagi Yasuhiko, Hasegawa Sunao, Yano Hajime, Teramoto Keisuke, Yamamoto Satoru, Sugita Seiji, Kurosawa Kosuke, Nakada Tesshin, Honda Chikatoshi, Abe Masanao
    宇宙利用シンポジウム, 23rd 182-184, 2007  
    We performed systematic impact cratering experiments in microgravity and vacuum environment with impact velocities larger than 100 m/sec and obtained data on diameter of crater formed in the environment. The experiments showed that the drop tower is an appropriate tool for studies of surface processes on small bodies. The result shows that the formation time and final diameter of crater formed in the glass beads or quartz sand layer are not controlled by the gravity.
  • 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, 23rd 410-413, 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, 28th 21-23, 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, 2007 315, 2007  
  • 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, 6 4204-4213, Dec 1, 2006  
  • 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, 6 3895-3901, Dec 1, 2006  
  • Demura Hirohide, Miyamoto Hideaki, Yano Hajime, Yoshikawa Makoto, Yoshimitsu Tetsuo, SSP Sub-group
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2006 77-77, 2006  
    Our sub-group of SSP (Surface Science Package) has been set up in Minorbody exploration WG. Our goal is establishment of arrangement of surface science instruments for positioning, collecting geologic context, supporting selection of sampling sites, and calibrations of orbiter instruments. Scientific goal is to collect key evidence in sedimentology/stratigraphical geology under the micro-gravity environment. We will report the current status of this sub-group
  • YANO Hajime, HASEGAWA Sunao, Minor Body Exp. WG Sampling Sub-Group, NOGUCHI Takaaki, MATSUNAGA Saburo, Fujii Hirohisa, MIURA Yayoi, MORI Osamu, TSUCHIYAMA Akira, NARAOKA Hiroshi, NAKAMURA Tomoki
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2006 79-79, 2006  
    As a post-Hayabusa mission in 2010's, our working group has been developing a new sampling system for C-type and other primitive asteroid surface and sub-surface materials, based upon technology and operation established and lessons learned by Hayabusa's touch-and-go sampling attempt at the S-type asteroid Itokawa in 2005. Both impact sampling with corer projectiles and a microgravity tether retraction system are under the development as well as shaped charge excavation on free asteroidal surface. This study summarizes results of those endeavors and future prospects of this challenge.
  • Shibata Hiromi, Takechi Seiji, Onishi Toshiyuki, Fujiwara Akira, Yano Hajime, Guruen Eberhart, Srama Ralf, Nogami Ken'ichi, Miyachi Takashi, Kuraza Genei, Ohashi Hideo, Fujii Masayuki, Sasaki Sho, Iwai Takeo, Minami Shigeyuki
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2006 83-83, 2006  
    The Mercury Dust Monitor (MDM) will be onboard the BepiColombo MMO spacecraft which will be launched in 2013. The MDM is an array of lightweight and heat resistant piezoelectric (lead-zirconate-titanate; PZT) detector in order to measure momentum and incoming direction of hypervelocity micro-particles around Mercury. Two major scientific interests are flux and origin variations on interplanetary meteoroid complex inside 1 AU, and the in-situ investigation of the near-Mercury dust environment.The MDM consists of 4 flat PZT plates whose size is 4cm x 4cm and 1mm thick for each PZT. The calibration experiments of this system are made using micro-particle accelerators at HIT, Univ. Tokyo in Japan and at MPI-K in Germany. By analyzing impact signal, rough momentum and velocity of impact particles can be determined. Only the output signal within a few hundred nanoseconds immediately after impact is analyzed, which is free from interference with reflected waves and could contain an impact hysteresis. The following results are obtained; 1. Output amplitude is proportional to the momentum of particles below 6 km/s, 2. rise-time is related to the particle velocity above 10km/s, 3. there exists a transition region in between, and 4. the sensitivity is confirmed to be independent of the element thickness.
  • Miyamoto Hideaki, Saito Jun, Yano Hajime, Sasaki Shou, Demura Hirohide, Hirata Naru, Ishiguro Masaaki, Michikami Tatsuhiro, Nakamura Akiko, Nakamura Ryousuke
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2006 74-74, 2006  
    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.
  • 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), 50th 2H14, 2006  
  • 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 26-26, 2006  
    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.
  • 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 7-7, 2006  
    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.
  • Okudaira Kyoko, Yano Hajime, Onose Naomi, Hasegawa Sunao
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2006 104-104, 2006  
    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-Al2O3 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.
  • Nakamura Ryosuke, Nakamura Akiko, Hirata Naru, Abe Shinsuke, Ishiguro Masateru, Yano Hajime
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2006 2-2, 2006  
    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.
  • Abe Shinsuke, Yamamoto Masa-yuki, Yano Hajime, Ebizuka Noboru, Watanabe Jun-ichi, Mukai Tadashi
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2006 107-107, 2006  
    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.
  • 矢野創, 安部正真, 藤原顕
    太陽系科学シンポジウム, 27th 45-48, 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, 2006 86, 2006  
  • S. Diniega, H. Yano, D. Scheeres
    International Astronautical Federation - 56th International Astronautical Congress 2005, 2 1009-1016, Dec 1, 2005  
  • A Tsuchiyama, K Uesugi, T Nakano, H Yano, K Okudaira, T Noguchi
    METEORITICS & PLANETARY SCIENCE, 40(9) A158-A158, Sep, 2005  
  • H Yano, T Okazaki, AM McDonnell, M Nakano, T Noguchi, K Okudaira, A Tsuchiyama
    METEORITICS & PLANETARY SCIENCE, 40(9) A171-A171, Sep, 2005  
  • 野口 高明, 矢野 創, 小天体探査WGサンプリングサブグループ
    宇宙科学シンポジウム, 5 242-245, Jan 6, 2005  
  • 出村 裕英, 矢野 創, 吉光 徹雄
    宇宙科学シンポジウム, 5 246-248, Jan 6, 2005  
  • 宮地孝, 藤井雅之, 長谷部信行, 蔵座元英, 佐々木晶, 岩井岳夫, 野上謙一, 大橋英雄, 松本晴久, 矢野創, 柴田裕実, 南繁行, 大西俊之, 武智誠次, GRUEN E., SRAMA R.
    宇宙航空研究開発機構特別資料 JAXA-SP-, (05-024), 2005  
  • 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, 1 423-427, 2005  
  • 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, 2 816-818, 2005  
  • 冨樫悟, 田中和生, 矢野創, 秋山演亮
    宇宙科学技術連合講演会講演集(CD-ROM), 49th 2A05, 2005  
  • Kasuga Toshihiro, Watanabe Jun-ichi, Yamamoto Tetsuo, Ebizuka Noboru, Kawakita Hideyo, Yano Hajime
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2005 28-28, 2005  
    High-Definition TV spectra in the ultraviolet -- visible region were obtained during the 2002 Leonid aircraft campaign. We analyzed 20 meteor spectra obtained from the 1767 (7-revolution) and 1866 (4-revolution) trails on November 19, 2002, and identified the neutral atoms, mainly MgI, FeI, CaI, and NaI in the observed wavelengths between 300--650nm. The singly ionized atomic emissions, CaII and MgII lines, also appeared in the spectrum. The abundances of metallic atoms, the electronic excitation temperature and electron density are obtained for each spectrum, assuming the Boltzmann distribution for the number of each energy level. The metallic abundances of Fe, Ca and Na relative to Mg are slightly lower than solar abundances in average. We could not find out any evidence of space weathering on Leonid meteoroids between 1767 and 1866 trails. We can support the idea that silicate and carbon-mixed silicate are preserved in interplanetary space at least several hundred years. Bands of CHON -- related molecules, such as OH and CN, are not detected in this study.
  • Saito Yasuyuki, Yoshida Shinsuke, Yano Hajime, Tanaka Satoshi, Horai Ki-ichi
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2005 51-51, 2005  
    Thermal inertia of the (25143) Itokawa has observed on the ground observation. As the (25143)Itokawa has high thermal inertia (~750-1000J/m2/s0.5/K) from the results of the ground observation, it is thought that there are no regolith on the it's surface and it is covered by naked rock. We will show the existence possibility of the regolith assuming two layers model even the body has high thermal inertia.
  • Okazaki Takahide, Tsuchiyama Akira, Yano Hajime, Nakano Tsukasa, Uesugi Kentaro, Noguchi Takaaki, Okudaira Kyouko, McDonnell J.A.M.
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2005 107-107, 2005  
    In initial analyses of meteoroids, it is crucial to obtain basic information by non-destructive methods as farther detailed analyses usually involve destructive processes. We conducted synchrotron microtomography for intact captured samples in a space exposed aerogel module onboard the European Retrievable Carrier (EuReCa) spacecraft in the low earth orbit during 1992-93. The X-ray microtomography measurements were performed at BL47XU in SPring-8, Japan. Using synchrotron radiation as an X-ray source, we can obtain CT images with the effective spatial resolution of about 1 mm and quantitative values of X-ray linear absorption coefficients by high flux density and monochromatic X-rays. Subtraction method, with which the aerogel specimens were imaged at X-ray energies just above and below the K-absorption edge of Fe, showed no Fe in the samples, suggested their impactors might be artificial orbital debris. We also obtained three-dimensional structures of sub-mm sized impact tracks and the distributions of sample fragments and condensed aerogel particles along the interior of the tracks. This research shows the effectiveness of impact tracks and samples captured in aerogel with synchrotron microtomography in sub-mm scale; it can be applied to the Stardust samples that will return in January 2006.
  • 田中智, 小林直樹, 矢野創, 藤村彰夫
    日本地震学会秋季大会講演予稿集, 2005 16, 2005  
  • 矢野 創, 臼井 文彦, 笠羽 康正
    宇宙科学シンポジウム, 4 207-210, Jan 8, 2004  
  • 臼井 文彦, 矢野 創, 長谷川 直
    宇宙科学シンポジウム, 4 215-218, Jan 8, 2004  
  • 矢野 創, 中村 良介, 横田 康弘
    宇宙科学シンポジウム, 4 219-222, Jan 8, 2004  
  • 藤原 顕, 矢野 創, 安部 正真
    宇宙科学シンポジウム, 4 417-420, Jan 8, 2004  
  • 矢野 創, 安部 正真, 吉光 徹雄
    宇宙科学シンポジウム, 4 357-360, Jan 8, 2004  
  • 阿部 正真, 矢野 創
    35th Lunar and planetary Science Conference (Huston) CD-ROM, 2004  
  • 矢野 創, 阿部 正真
    35th Lunar and planetary Science Conference (Huston) CD-ROM, 2004  
  • H. Yamakawa, Y. Kawakatsu, M. Morimoto, M. Abe, H. Yano
    International Astronautical Federation - 55th International Astronautical Congress 2004, 10 6597-6604, 2004  
  • Tsuchiyama Akira, Nakamura Kentaro, Uesugi Kentaro, Nakano Tsukasa, Yano Hajime, Okudaira Kyoko, Nakamura Keiko, Noguchi Takaaki, Nakamura Tomoki
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2004 111-111, 2004  
    Analytical methods using synchrotron radiation imaging for extraterrestrial small samples, such as micrometeorites and IDPs, have been developed. Observation of dust tracks as well as dust particles in an aerogel dust collector is possible by micro-radiography using refraction imaging. This method can be applied to Stardust mission sample, which will be returned from comet Wild-2 in January, 2006. Density measurement of micrometeorites by micro-tomography can be applied to Hayabusa mission sample, which will be returned from S-type asteroid ITOKAWA in June, 2007.
  • Teramoto Keisuke, Yano Hajime
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2004 87-87, 2004  
    To apply for possible asteroid interior exploration in the future, this study aims to better understand basic physical property of granular materials such as space exposed regolith regarding elastic waves. We have discovered speed of sound in regolith simulants made of glass bead is independent on porosity but dependent on grain size in the 40 - 220 micrometers range. Although actual cases are more complexed, these results suggest the possibility of using velocity measurement of elastic wave of to investigate regolith size on asteroidal surfaces.
  • Kasuga Toshihiro, Yamamoto Tetsuo, Watanabe Jun-ichi, Ebizuka Noboru, Kawakita Hideyo, Yano Hajime
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2004 21-21, 2004  
    本研究では、2002年に2世代のダストトレイルから観測されたしし座流星群の金属元素アバンダンスについて議論する。しし座流星群からは、Mg, Fe, Ca, Naなどの金属元素が観測されている。これらのアバンダンスをダストトレイルの形成年代別に比較することにより、ダスト中に含まれる金属元素の物質進化の議論が可能となる。本学会ではこれらについて報告する。
  • YANO Hajime, ABE Masanao, KAWAKATSU Yasuhiro, MORI Osamu, YOSHIMITSU Tetsuo, FUJIWARA Akira, Minor Body Exploration Working Group
    Abstracts for fall meeting of the Japanese Society for Planetary Science, 2004 110-110, 2004  
    Following up Hayabusa's heritage for asteroid sample return, the 'Minor Body Exploration Working Group' was officially approved this March, in order to design and propose a next generation minor body exploration mission by the end of FY 2006. At present, strategic developments include a sampling mechanism to retain stratigraphic information on a C-type asteroid surface and a rover system to observe the filed of occurrence of samples. This talk discusses its scientific objectives, possible mission targets, and status of such strategic developments.
  • 臼井文彦, 矢野創, 長谷川直, 石黒正晃, 上野宗孝
    日本天文学会年会講演予稿集, 2004 271, 2004  
  • 上野宗孝, 石黒正晃, 臼井文彦, 矢野創, 今村剛, 中村正人, 佐藤毅彦, 木股雅章
    日本天文学会年会講演予稿集, 2004 265, 2004  

Books and Other Publications

 35

Presentations

 596
  • Hajime YANO, Takeshi IMAMURA, Shuji MATSUURA, Naoya SAKATANI, Hiroki ANDO, Kazuyoshi ARAI, Hajime KAWAHARA, Naoya OZAKI, Yuhito SHIBAIKE, Kakeru TOKUNAGA, Atsushi TOMIKI, Ryu FUNASE, JAXA/ISAS OPENS, Pre-Project Candidate Team
    The European Geosciences Union (EGU) 2026 General Assembly, May 4, 2026, The European Geosciences Union  Invited
    In 2025, JAXA/ISAS selected "OPENS-0" (Outer Planet Exploration by Novel and Small Spacecraft-Zero), which aims to demonstrate key enabling technologies for a single, small spacecraft to conduct outer planet exploration, as the first mission for its newly-created "Eco and Fast" small-class category. While the 100-kg-class OPENS-0 spacecraft has severe limitations in both resources and operational capabilities, unlike legacy outer plane missions, its lighter mass and smaller size can be advantages for power and thermal management, as well as delta-V requirements. Although the spacecraft design cannot enjoy abundant resources for dedicated scientific payloads, the OPENS-0 maximizes its scientific outputs, during 10+ years of the interplanetary cruising and multiple flyby occasions, with several "multi-purpose" instruments such as (1) the optical navigation telescopic and wide-field cameras to observe the "Pale Blue Dot" as a reference of Earth-like exoplanets, zodiacal light variation through the Main Asteroid Belt, extragalactic background light in the outer planet region, main belt asteroid morphology; (2) the ultra-stable oscillator and deep space transponder for radio occultation of the solar flare, and the planetary atmospheres of Venus and Saturn; and (3) the PVDF-layered MLI for interplanetary micrometeoroid flux at 1-10 AU heliocentric distance. Once the spacecraft eventually arrives in the vicinity of Saturn at the finale of the mission, all three instruments will be coordinated for integrated sciences focused on Saturn's ring structures, ranging from the retrograde satellite dust torus to the E-ring region, as well as the main rings and gaps, in complementary spatial resolutions among them. How to cite: Yano, H., Imamura, T., Matsuura, S., Sakatani, N., Ando, H., Arai, K., Kawahara, H., Ozaki, N., Shibaike, Y., Tokunaga, K., Tomiki, A., and Funase, R.: Cruising and Flyby Sciences with Multi-Purpose Instruments onboard Japan's First Outer Planet Exploration Spacecraft "OPENS-0", EGU General Assembly 2026, Vienna, Austria, 3–8 May 2026, EGU26-17424, https://doi.org/10.5194/egusphere-egu26-17424, 2026.
  • H. Yano, R. Funase, N. Ozaki, K. Tokunaga, O. Mori, Y. Takao, Y. Saito, ISAS OPENS Pre-Project Candidate Team, ISAS OPENS, Research Group
    Mar 27, 2026
  • T. Arai, M. Kobayashi, K. Ishibashi, H. Kimura, T. Okamoto, O. Okudaira, F. Yoshida, M. Yamada, K. Wada, H. Senshu, H. Akitaya, R. Srama, H. Krüger, M. Ishiguro, T. Nakamura, H. Yabuta, S. Sasaki, J. Watanabe, T. Ito, T. Ootsubo, K. Ohtsuka, T. Morota, J. Beniyama, S. Tachibana, T. Mikouchi, T. Hiroi, T. Sekiguchi, S. Abe, S. Urakawa, S. Matsuura, M. Ito, A. Yamaguchi, T. Noguchi, M. Komatsu, K. Nakamura-Messenger, N. Hirata, H. Demura, G. Komatsu, H. Kaneda, S. Marshall, E. Tatsumi, Y. Yokota, H. Yano, M. Yoshikawa, N. Ozaki, T. Yamamoto, H. Toyota, K. Nishiyama, H. Imamura, T. Takashima
    The 56th Lunar and Planetary Science Conference, Mar 15, 2026, Lunar and Planetary Institute
  • 矢野創, 船瀬龍, 尾崎直哉, 徳永翔, 森治, 高尾勇輝, ISAS OPENS, プリプロジェクト準備チーム, 宇宙工学委員会, OPENS, リサーチグループ
    第27回惑星圏シンポジウム(SPS2026) ・外惑星探査ワークショップ, Mar 4, 2026, 東北大学理学部 惑星プラズマ・大気研究センター  Invited
  • 横堀伸一, 三田肇, 安部智子, 奥平恭子, 加藤浩, 木村駿太, 久米篤, 佐々木康隆, 富田-横谷香織, 永井大樹, 日渡祐二, Maeng Chang-Hyun, 山岸明彦, 矢野創, 藤田知道
    第40回 宇宙環境利用シンポジウム, Mar 2, 2026, JAXA宇宙科学研究所

Teaching Experience

 5

Research Projects

 43

Industrial Property Rights

 8

Academic Activities

 23
  • 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
  • Planning, Management, etc., Panel moderator, Session chair, etc., Supervision (editorial), Review, evaluation
    Committee of Space Research(COSPAR) (Nicosia, Cyprus), Nov 3, 2025 - Nov 7, 2025
    Building on the success of the B3.2 Scientific Event at the 2024 COSPAR Scientific Assembly in Busan, this Scientific Event brings together COSPAR scientists and new space participants to advance new research opportunities on the Moon, in Earth orbit, and across deep space. The year 2025 has seen the first fully successful commercial landing on the Moon, with more possibly following before this symposium. New science and data opportunities range from lunar subsurface thermal properties, electrodynamic dust interactions, and studies of the interaction of solar wind and Earth's magnetic field, to experiments in resource beneficiation and new electrolytic processes on the lunar surface. Near-Earth objects are now targets of the off-Earth mining industry and planetary defense for both governmental and private sectors. Deep space exploration to Mars and beyond also involves emerging space agencies, and CubeSats and small sats are rapidly being utilized for their missions. New space startups are also introducing new data gathering capabilities from Earth orbit, including a fusion of new sensor and communication technology for monitoring, analysing, and mitigating natural and human hazards on Earth. This event will highlight the technology gaps that current space science can address by promoting collaborations and partnerships among new space entrepreneurs, the COSPAR Associates community, established space agencies, and legacy industry players.

Social Activities

 3

Media Coverage

 96
  • 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.
  • GIzmode, Gizmode, Space & Spaceflight, Feb 12, 2026 Internet
    Luna 9 had a bouncy touchdown on the lunar surface in 1966, becoming the first spacecraft to land on the Moon.

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