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
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

 316
  • 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, Feb 23, 2026  
  • 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.
  • André Galli, Heather Smith, Michel Blanc, Bernard Foing, Hélène Boithias, Scott J. Bolton, Soyoung Chung, Athena Coustenis, Eric Dautriat, Jean-Pierre de Vera, Peter Doran, François Dubrulle, Fatemeh Fazel Hesar, Carolin Frueh, Shaifali Garg, Niklas Hedman, Kyeong J. Kim, Stéphanie Lizy-Destrez, Andreas Losch, Alessandra Marino, Christopher McKay, Patrick Michel, Olivier Mousis, Antonino Salmeri, Udit Shah, Shine S. R., Michael Sims, Jean-Claude Worms, Hajime Yano
    Life Sciences in Space Research, Dec 18, 2025  Peer-reviewedLast author
    In response to the growing importance of space exploration, the objectives of the COSPAR Panel on Exploration (PEX) are to provide high quality, independent science input to support the development of a global space exploration program, to promote space sciences as a key element of this program, to contribute to maximize its scientific return via enhanced international cooperation, and to take action to safeguard the scientific assets of solar system bodies. This paper summarizes the presentations of the two panel sessions at the COSPAR assembly 2024 and identifies the most intensely discussed recent topics of interest or concern for space exploration. These topics include environment stewardship of celestial bodies, space debris, resource utilization, the Moon, Mars, and other celestial bodies that we want to explore with planetary protection measures, preservation of dark and quiet skies, potential atmospheric pollution, space as an independent goal of sustainable development, human spaceflight, agile and affordable space programs, and the early preparation of a new edition of the COSPAR exploration roadmap.
  • Matthew J. Genge, Natasha V. Almeida, Matthias van Ginneken, Lewis Pinault, Tobias Salge, Penelope J. Wozniakiewicz, Hajime Yano, Steven J. Desch
    Nature Communications, 16(6466), Jul 23, 2025  Peer-reviewed
    Chondrules are a characteristic feature of primitive Solar System materials and are common in all primitive meteorites except the CI-chondrites. They are thought to form owing to melting of solid dust aggregates by energetic processing within the solar nebula and thus record fundamental processes within protoplanetary disks. We report the discovery of abundant altered microchondrules (>350 ppm) with modal sizes of 6–8 µm within sample A0180 from C-type asteroid Ryugu. These microchondrules have similar log-normal size and shape distributions to normal-sized chondrules, implying evolution by similar size-sorting. We suggest here formation of microchondrules in an outer Solar System chondrule factory, located in the Jovian pressure-bump, followed by turbulent diffusion and concentration relative to chondrules by intense turbulence. Meridional flows could have also separated microchondrules from chondrules and deliver them sunwards of the pressure bump via Lindblad torque flows. Contrary to conventional wisdom, we thus propose that the concentration of fine-grained, unprocessed grains could mean the most primitive asteroids did not have to form at the largest heliocentric distances.

Misc.

 495

Books and Other Publications

 35

Presentations

 595
  • Christian Ziach, Tra Mi Ho, Christian Grimm, Ross Findlay, Caroline Lange, Lars Witte, Michael Wrasmann, Jens Biele, Stephan Ulamec, Tilman Spohn, Muriel Deleuze, Jean Pierre Bibring, Tatsuaki Okada, Hajime Yano, Jeffrey Hendrikse
    Proceedings of the International Astronautical Congress, IAC, Jan 1, 2013
    The Memorandum of Understanding signed between the Japanese Aerospace Exploration Agency (JAXA) and the German Aerospace Centre (DLR) during the 63rd International Astronautical Congress (IAC) in Naples, paves the way for the Mobile Asteroid Surface Scout (MASCOT) participation in JAXAs Hayabusa-II mission. Like its famous predecessor, Hayabusa-II is foreseen to study and return samples from a Near-Earth Asteroid. In contrast to the previous mission, Hayabusa-II will also include a small lander package being developed by DLR and the Centre National d'Etudes Spatiales (CNES): the aforementioned MASCOT. Scheduled for a launch in 2014, Hayabusas-II journey will take 4 years until it will arrive at 1999JU3, a C-type asteroid. Following the initial remote sensing operations, MASCOT will be released to the surface and perform its science operations at its first location. Once this is complete, MASCOT will be able to 'hop' from one measurement site to the next. The payload suite will comprise a near-infrared microscope (MicrOmega, IAS Paris), a camera (CAM, DLR Berlin), a radiometer (MARA, DLR Berlin) and a magnetometer (MAG, TU Braunschweig). Realizing MASCOTs mission is difficult due to the strict mission requirements, the harsh landing environment and a short development time for a piggyback deep space mission. Aiming for high performance and reliability requires creative design solutions and novel developments in order to meet all challenges and to stay inside the mass limit of 11 kg. The status of MASCOT up to end of Phase B was presented at the 63rd IAC. With a flight model delivery scheduled for March 2014, the mission is now in the final stage of development and testing. The results of these tests have shown the strict limits of the structure and thermal design, and highlighted the risk in such a short project development. Lessons have also been learned regarding margin policy for such small spacecraft. Despite these challenges, the project is on-track, with all delivery milestones expected to be met. These last few months will serve to verify all of the design assumptions, before the launch in late 2014.
  • Ross Findlay, Tra Mi Ho, Caroline Lange, Susanne Wagenbach, Lars Witte, Christian Ziach, Jens Biele, Christian Krause, Stephan Ulamec, Tilman Spohn, Tatsuaki Okada, Hajime Yano
    Proceedings of the International Astronautical Congress, IAC, Dec 1, 2012
    The JAXA Hayabusa-II mission is the follow-up to the original Hayabusa mission launched in 2003 \ which succeeded in returning the first dust particles from a near-Earth asteroid to Earth. JAXA intends to launch Hayabusa-II in 2014 for similar measurements of the asteroid 1999 JU3, a C-type asteroid, and invited the German Aerospace Centre (DLR) to contribute a small lander package to the mission. Based on this invitation, DLR is developing the Mobile Asteroid Surface Scout (MASCOT) to complement the main spacecraft's scientific objectives, with the Centre National d'Etudes Spatiales (CNES) providing payload and subsystem support. MASCOT will provide in-situ surface science and allow investigation of up to three sites on the asteroid surface. A short on-asteroid lifetime of two complete asteroid rotations (-16 hours) will provide measurements under different illuminations and thermal conditions, with Hayabusa-II being used to transmit all of the scientific data back to Earth. The harsh landing environment and strict mission requirements lead to some difficult design challenges. An innovative "hopping" mechanism will allow MASCOT to leap across the asteroid surface in bounds of up to 220m, albeit robustness of this concept must first be proven in a comprehensive suite of simulations and tests. Mass, limited to 10 kg, is critical: savings via the use of a carbon-fibre main structure and simplified subsystems allows the carriage of four scientific payloads, namely a multispectral wide angle camera, a radiometer, a magnetometer and an IR microscope. Thermal control is a challenge given the contrasting requirements of deep-space cruise and on- surface operation. Available energy also puts a strict limit on operations and restricts the lifetime of the mission. Copyright © (2012) by the International Astronautical Federation.
  • H. Sawada, S. Tachibana, R. Okazaki, C. Okamoto, H. Yano, Y. Miura
    Proceedings of the International Astronautical Congress, IAC, Dec 1, 2012
    Japan Aerospace Exploration Agency (JAXA) plans to launch the small asteroid explorer "HAYABUSA2" in 2014, following the HAYABUSA mission. By improving the HAYABUSA probe, we are planning to visit the small asteroid "1999JU3", and aiming sample-return from an asteroid of different type from Itokawa. The 1999JU3 is a C- Type asteroid, considered to contain more organic or hydrated materials than S-type asteroids like ITOKAWA. The basic configuration of the spacecraft is mainly the same as HAYABUSA, with several minor modifications. The spectroscopic equipment and sampling system will be improved to be more suitable to C-type asteroids, because the surface of C-type asteroids is expected to differ from that of S-type ones. We will report the details of the sampling system of HAYABUSA2, and introduce our developing status of the sampling system. Copyright © (2012) by the International Astronautical Federation.
  • 荒川 政彦, 門野 敏彦, 高木 靖彦, 和田 浩二, 平田 成, 小林 正規, 本田 理恵, 白井 慶, 早川 雅彦, 岡本 千里, 小川 和律, 矢野 創, 中澤 暁, 飯島 祐一, 佐伯 孝尚, 今村 裕志, 澤田 弘崇
    日本惑星科学会秋期講演会予稿集, Oct 24, 2012
  • 柴田 裕実, 野上 謙一, 藤井 雅之, 大橋 英雄, 小林 正規, 佐々木 晶, 矢野 創, 木村 宏, 武智 誠次, 岩井 岳夫, 長谷川 直, 平井 隆之, 服部 真季, 宮地 孝, Srama Ralf, Grun Eberhart
    日本惑星科学会秋期講演会予稿集, Oct 24, 2012
  • MITSUTA Tomohiko, YANO Hajime, HIRATA Naru, WADA Koji, ARAKAWA Masahiko
    Proceedings of 39th COSPAR Scientific Assembly, Jul, 2012
  • MITSUTA Tomohiko, HIRATA Naru, WADA Koji, YANO Hajime, ARAKAWA Masahiko
    Proceedings of Asteroids, Comets, Meteors 2012, May, 2012
  • 高野淑識, 高井研, 渋谷岳造, 矢野創, 船瀬龍, 関根康人, 吉村義隆, 山岸明彦, 木下大輔, TSOU Peter, TSOU Peter, TSOU Peter
    宇宙利用シンポジウム, Mar, 2012
  • 河口優子, 杉野朋弘, 川尻成俊, 白石啓祐, YANG Yinjie, 小林憲正, 田端誠, 長谷川直, 今井栄一, 河合秀幸, 奥平恭子, 橋本博文, 山下雅道, 矢野創, 横堀伸一, 山岸明彦
    Viva Origino, Mar 1, 2012
  • Kawaguchi Yuko, Sugino Tomohiro, Kawashiri Narutoshi, Shiraishi Keisuke, Yang Yinjie, Kobayashi Kensei, Tabata Makoto, Hasegawa Sunao, Imai Eiichi, Kawai Hideyuki, Okudaira Kyoko, Hashimoto Hirofumi, Yamashita Masamichi, Yano Hajime, Yokobori Shin-ichi, Yamagishi Akihiko
    Viva origino, Mar 1, 2012
  • 山岸明彦, 河口優子, 杉野朋弘, YANG Yinjie, 横堀伸一, 矢野創, 橋本博文, 田端誠, 太刀川純孝, 長谷川直, 小林憲正, 河合秀幸, 中嶋悟, 藪田ひかる, 奥平恭子, 三田肇, 保田浩志, 中川和道
    宇宙利用シンポジウム, Mar, 2012
  • 横堀伸一, 春山純一, 矢野創, 鳴海一成, 三田肇, 高橋淳一
    宇宙利用シンポジウム, Mar, 2012
  • 横堀伸一, 山岸明彦, 河口優子, 杉野朋弘, 川尻成俊, 白石啓祐, 小林憲正, 大林由美子, KUMAR Palash Sarker, 小野恵介, 川本幸徳, 山下雅道, 橋本博文, 矢野創, 長谷川直, 田端誠, 丸茂克美, 中嶋悟, 藪田ひかる, 緒方雄一朗, 河合秀幸, 奥平恭子, 三田肇, 奈良岡浩, 今井栄一
    スペース・プラズマ研究会・講演集(Web), 2012
  • 橘省吾, 澤田弘崇, 岡崎隆司, 岡本千里, 矢野創
    宇宙科学技術連合講演会講演集(CD-ROM), 2012
  • 船瀬龍, 森治, 白澤洋次, 津田雄一, 矢野創
    宇宙科学技術連合講演会講演集(CD-ROM), 2012
  • Takanao Saiki, Hirotaka Sawada, Chisato Okamoto, Hajime Yano, Yasuhiko Takagi, Yasuhiro Akahoshi, Makoto Yoshikawa
    62nd International Astronautical Congress 2011, IAC 2011, Dec 1, 2011
    The Japanese asteroid explorer HAYABUSA launched in 2003 arrived at its target asteroid ITOKAWA in September, 2005. HAYABUSA has made amount of scientific discoveries and technological achievements during its stay at ITOKAWA and it came back to the Earth on June 13, 2010. Under this situation, the next asteroid exploration mission started. The spacecraft is called HAYABUSA-2. Although its design basically follows HAYABUSA, some new components are planned to be equipped in HAYABUSA-2 mission. A small carry-on impactor is one of the new challenges that were not seen with HAYABUSA. One of the most important scientific objectives of HAYABUSA-2 is to investigate chemical and physical properties of the internal materials and the internal structures in order to understand the formation history of small bodies. In order to achieve this objective, the impactor is required to remove the surface regolith and create an artificial crater on the surface of the asteroid. Ulis paper presents the overview of our small carry-on impactor system and impact operation of HAYABUSA-2 mission. And how to improve this impactor when it is applied to another small body exploration mission is also presented in this paper. Copyright ©2011 by the International Astronautical Federation. All rights reserved.
  • NAKAMURA Ryosuke, CHEN Bo,MATSUOKA Masashi, YAMAMOTO Hirokazu, KAMEI Akihide, NAKAMURA Kazuki, YANO Hajime
    Publ Astron Soc Jpn, Oct 25, 2011
  • Ho Tra-Mi, Witte Lars, Ulamec Stephan, Dittus Hans-Joerg, Spohn Tilman, Bibring Jean-Pierre, Bousquet Pierre
    Abstracts Fall Meeting of the Japanese Society for Planetary Sciences, Oct 23, 2011
  • 池崎 克俊, 矢野 創, 岡本 千里, 橘 省吾, 今栄 直也, 土山 明, 長谷川 直, 中村 昭子, 富山 隆將
    日本惑星科学会秋期講演会予稿集, Oct 23, 2011
  • YANO Hajime
    The journal of the Japanese Society for Dental Materials and Devices, Sep 25, 2011
  • 柴田裕実, 池田卓矢, 野上謙一, 藤井雅之, 小林正規, 宮地孝, 大橋英雄, 佐々木晶, 岩井岳夫, 中村真季, 木村宏, 武智誠次, 平井隆之, 矢野創, 長谷川直, 岡田長也, GRUEN Eberhart, SRAMA Ralf
    応用物理学会学術講演会講演予稿集(CD-ROM), Aug 16, 2011
  • 横堀伸一, 鳴海一成, 春山純一, 三田肇, 矢野創, 高橋淳一
    宇宙利用シンポジウム, Mar, 2011
  • 山岸明彦, 河口優子, 杉野智弘, YANG Yinjie, 横堀伸一, 吉村義隆, 辻尭, 小林憲正, 藤崎健太, 田端誠, 長谷川直, 橋本博文, 矢野創, 山下雅道, 河合秀幸, 中嶋悟, 藪田ひかる, 奥平恭子, 三田肇, 浜瀬健司, 中川和道
    宇宙利用シンポジウム, Mar, 2011
  • 吉村義隆, 山岸明彦, 内海裕一, 長沼毅, 本多元, 山下雅道, 橋本博文, 横堀伸一, 宮川厚夫, 河崎行繁, 伊藤隆, 矢野創, 佐々木晶, 才木常正
    宇宙利用シンポジウム, Mar, 2011
  • 善場祐介, 矢野創, 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, 2011
  • 横堀伸一, YANG Yinjie, 河口優子, 杉野朋弘, 高橋勇太, 鳴海一成, 高橋裕一, 林宣宏, 吉村義隆, 田端誠, 河合秀幸, 矢野創, 奥平恭子, 今井栄一, 長谷川直, 橋本博文, 三田肇, 薮田ひかる, 小林憲正, 山下雅道, 山岸明彦
    Viva Origino, Mar 1, 2011
  • Yokobori S, Yang Yinjie, Kawaguchi Y, Sugino T, Takahashi Y, Narumi I, Takahashi Y, Hayashi N, Yoshimura Y, Tabata M, Kawai H, Yano H, Okudaira K, Imai E, Hasegawa S, Hashimoto H, Mita H, Yabuta H, Kobayashi K, Yamashita M, Yamagishi A, TANPOPO Workin Group
    Viva origino, Mar 1, 2011
  • Morishita Hiroyuki, Morii Shota, Matunaga Saburo, Yano Hajime, Okamoto Chisato
    Jan 27, 2011
    The minorbody explorer called "HAYABUSA" conducted sampling mission on the minorbody "ITOKAWA", and now it is planning to develop next minorbody explorers. The LSS, laboratory for space systems at the Tokyo Institute of Technology, and JAXA, propose the adhesive based sampling system for next minorbody explorers. By using this sampling system, it becomes possible to get larger size and heavier mass samples compare with the samples which are able to get by HAYABUSA's sampling system. In this paper, Description of the adhesive based sampling system, results of evaluation experiments and analy...
  • 森井翔太, 森下拓往, 松永三郎, 矢野創, 澤田弘崇
    宇宙科学技術連合講演会講演集(CD-ROM), 2011
  • 渡辺英幸, 松枝達夫, 久保田伸幸, 上垣栄一, 山岸明彦, 橋本博文, 矢野創
    宇宙科学技術連合講演会講演集(CD-ROM), 2011
  • 森治, 矢野創, 川口淳一郎, 善場祐介
    宇宙科学技術連合講演会講演集(CD-ROM), 2011
  • 横堀伸一, 山岸明彦, YANG Yinjie, 河口優子, 杉野朋弘, 高橋勇太, 小林憲正, 大林由美子, PALASH Sarker Kumar, 小野恵介, 川本幸徳, 山下雅道, 橋本博文, 矢野創, 長谷川直, 田端誠, 丸茂克美, 中嶋悟, 藪田ひかる, 緒方雄一朗, 河合秀幸, 奥平恭子, 三田肇, 奈良岡浩, 今井栄一, 林宣宏, 浜瀬健司
    スペース・プラズマ研究会・講演集(Web), 2011
  • 矢野創, 岡本千里, 田中真, 平井隆之, 長谷川直, 田端誠, 尾川順子, 岩井岳夫, 奥平恭子
    スペース・プラズマ研究会・講演集(Web), 2011
  • 森下拓往, 森井翔太, 松永三郎, 矢野創, 岡本千里
    宇宙科学技術連合講演会講演集(CD-ROM), 2011
  • 森井翔太, 森下拓往, 松永三郎, 矢野創, 澤田弘崇
    構造強度に関する講演会講演集, 2011
  • 森下拓往, 森井翔太, 松永三郎, 矢野創, 岡本千里
    日本機械学会スペース・エンジニアリング・コンファレンス(CD-ROM), 2011
  • 緒方雄一朗, 薮田ひかる, 中嶋悟, 奥平恭子, 森脇太郎, 池本夕佳, 長谷川直, 田端誠, 横堀伸一, 今井栄一, 橋本博文, 三田肇, 小林憲正, 矢野創, 山下雅道, 山岸明彦
    日本地球化学会年会講演要旨集, 2011, 一般社団法人日本地球化学会
    始原小天体有機物は、太陽系および生命原材料物質の起源と進化を理解するための重要な情報を記録している。「たんぽぽ計画」では、大気圏突入時の熱変成や地上での汚染を受けていない宇宙塵を、国際宇宙ステーション上に超低密度シリカエアロゲルを設置して回収を試みる予定である。しかし、この方法では、宇宙塵のエアロゲルへの衝突により変成する可能性を考慮する必要がある。そこで本研究では、宇宙科学研究所・スペースプラズマ実験施設の二段式高速ガス銃を用いて、隕石微粒子の高速衝突模擬実験を行い、マーチソン隕石微粒子をシリカエアロゲルに撃ち込んだものを取り出し、2枚のアルミ板にはさみハンドプレスして圧着された隕石微粒子を、片方のアルミ板に載せた状態で、赤外顕微分光装置と顕微ラマン分光装置で測定を行った。また、SPring-8, BL43IRの高輝度赤外顕微分光装置IFS120HRでイメージング測定を行い、衝突前後の隕石有機物の分子構造の変化を見出すことを目的とした。
  • Makoto Yoshikawa, Junichiro Kawaguchi, Hajime Yano, Yuichi Tsuda
    61st International Astronautical Congress 2010, IAC 2010, Dec 1, 2010
    Hayabusa spacecraft finally came back to the earth on June 13, 2010. It has a quite dramatic story and we had a lot of experiences about planetary mission. And now we have proposed Hayabusa follow-on mission, Hayabusa-2. It is an asteroid sample return mission again, but the type of the target asteroid is C-type, which is different from the target of Hayabusa, Itokawa (S-type). The scale of the spacecraft is similar to Hayabusa, but many parts will be modified so that we will not have the troubles that we experienced in Hayabusa. Also the spacecraft has new equipment, which is called impactor. The impactor will make an artificial crater on the surface of the asteroid, and we will try to get the sample inside the crater. Then we can get much fresh material. The planned launch year is 2014 or 2015, arriving at the target asteroid 1999 JU3 in 2018, and coming back to the earth 2020. We hope we can start this mission as soon as possible. Copyright ©2010 by the International Astronautical Federation. All rights reserved.
  • Claudia Dietze, F. Herrmann, S. Kuß, C. Lange, M. Scharringhausen, L. Witte, T. Van Zoest, H. Yano
    61st International Astronautical Congress 2010, IAC 2010, Dec 1, 2010
    To enhance the currently studied asteroid sample return mission HAYABUSA-2 by in-situ science the Institute of Space Systems of the German Aerospace Center (DLR) is in lead of a proposal for a lander called MASCOT (Mobile Asteroid Surface Scout). Its mass of 10 kg lies in between those of the HAYABUSA small lander MINERVA (1 kg) and the legged ROSETTA comet lander PHILAE (100 kg). In the successfully completed feasibility study the design of the MASCOT converged to a landing package with 10 kg total mass, 3 kg of payload and the capability of hopping. As a result of its reduced size and the highly demanding constraints regarding e.g. mobility, the design as well as the landing and mobility cannot be adapted from MINERVA and PHILAE. This paper is intended to give an overview over the demanding landing and mobility concept for MASCOT. The current MASCOT baseline design is presented, which has to deal with tight budgetary limitations leading to a consolidated and widely integrated design, while still offering excellent performance in terms of mobility and resulting science. The focus lies on the mission analysis tasks and the mobility concept, which is studied in detail during the ongoing preliminary design phase. The general mission constraints including the parameters of the target asteroid (162173) 1999 JU3 are presented, while emphasis is put on the modelling of the asteroid's inhomogeneous gravity field. Therefore different gravitational models are implemented and their effect on the descent trajectory is compared. Of equal importance is the design support by investigating the two major mobility aspects, i.e. the self-uprighting mechanism and hopping over the asteroid's surface. These two issues are studied by applying both multi-body system and contact dynamics approaches. Moreover, this analysis will support the design of the actuator system for uprighting and hopping. After a presentation of the surface modelling and simulation approach an overview over first results and a short outlook on future mobility analysis and test activities for MASCOT is given. Copyright ©2010 by the International Astronautical Federation. All rights reserved.
  • 岡本 千里, 矢野 創, 田中 真, 長谷川 直, 田端 誠, 岩井 岳夫, 奥平 恭子, 尾川 順子, 平井 隆之
    日本惑星科学会秋期講演会予稿集, Oct 6, 2010
  • 岡田 達明, 矢野 創, 津田 雄一, 久保田 孝, 照井 冬人, 吉川 真, 平田 成, 出村 裕英, Ho Tra-Mi, Witte Lars, Zoest Tim van, Spohn Tilman, Bibring Jean-Pierre
    日本惑星科学会秋期講演会予稿集, Oct 6, 2010
  • 高木 靖彦, 中村 良介, 北里 宏平, 岡田 達明, 矢野 創, 津田 雄一, 佐伯 孝尚, 岡本 千里, 吉川 真, はやぶさ, プリプロジェクトチーム
    日本惑星科学会秋期講演会予稿集, Oct 6, 2010
  • 山岸 明彦, 横堀 伸一, 吉村 義隆, 山下 雅道, 橋本 博文, 久保田 孝, 矢野 創, 春山 純一, 田端 誠, 小林 憲正, 本多 元, 内海 裕一, 才木 常正, 伊藤 隆, 宮川 厚夫, 浜瀬 健司, 長沼 毅, 三田 肇, 戸野倉 賢一, 佐々木 晶, 宮本 英昭
    日本惑星科学会秋期講演会予稿集, Oct 6, 2010
  • TSUCHIYAMA A, MASHIO E, IMAI Y, NOGUCHI T, MIURA Y, YANO H, NAKAMURA T
    日本鉱物科学会年会講演要旨集, Apr 7, 2010
  • 野口高明, 平田成, 土山明, 出村裕英, 中村良介, 宮本英明, 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, ゾレンスキー マイケル・E
    日本惑星科学会誌 遊・星・人, Mar 25, 2010
  • 柴田裕実, 野上謙一, 宮地孝, 藤井雅之, 大橋英雄, 平井隆之, 佐々木晶, 岩井岳夫, 中村真季, 武智誠次, 矢野創, 長谷川直, 小林正規, 岡田長也, GRUEN Eberhart, SRAMA Ralf
    応用物理学関係連合講演会講演予稿集(CD-ROM), Mar 3, 2010
  • 河口優子, 杉野朋弘, YANG Yinjie, 吉村義隆, 辻尭, 小林憲正, 橋本博文, 田端誠, 山下雅道, 矢野創, 河合秀幸, 三田肇, 奥平恭子, 横堀伸一, 山岸明彦
    Viva Origino, Mar 1, 2010
  • 伏見英彦, 河合純, 平子智章, 大林由美子, 金子竹男, 小林憲正, 三田肇, 藪田ひかる, 今井栄一, 奥平恭子, 田端誠, 長谷川直, 河合秀幸, 丸茂克美, 橋本博文, 矢野創, 山下雅道, 横堀伸一, 山岸明彦
    Viva Origino, Mar 1, 2010
  • 小林憲正, 伏見英彦, 三田肇, 中川和道, 藪田ひかる, 高橋淳一, 奥平恭子, 矢野創, 橋本博文, 山岸明彦
    Viva Origino, Mar 1, 2010
  • 山岸明彦, 河口優子, 杉野智弘, YANG Yinjie, 横堀伸一, 吉村義隆, 辻尭, 小林憲正, 藤崎健太, 田端誠, 長谷川直, 橋本博文, 矢野創, 山下雅道, 河合秀幸, 奥平恭子
    宇宙利用シンポジウム, Mar, 2010

Teaching Experience

 5

Research Projects

 42

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

 80
  • 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

 8
  • 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

 26
  • 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
  • Student name
    Ritsuko JITSUKAWA
    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
    多層断熱材一体型微粒子衝突センサの性能評価
  • Student name
    Maximilian SOMMER
    Student affiliation
    独・シュトッツガルト大学院(JSPSサマープログラム留学生)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2018)
    Title
    Modelling Resonant Features in the Zodiacal Cloud
  • Student name
    Hiroyuki MOCHIZUKI
    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(2018)
    Title
    複層薄膜貫通型微粒子衝突センサへの信号積分回路付与による質量推定精度の向上

● 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