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
Visiting Scientist, Institute of Soldier Nanotechnologies, 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

 47

Papers

 297
  • Aline Percot, Farah Mahieddine, Hajime Yano, Sunao Hasegawa, Makoto Tabata, Akihiko Yamagishi, Hajime Mita, Alejandro Paredes-Arriaga, Marie-Christine Maurel, Jean-François Lambert, Donia Baklouti, Emilie-Laure Zins
    Gels, 10(4) 249, Apr 6, 2024  Peer-reviewed
  • Geraint H. Jones, Colin Snodgrass, Cecilia Tubiana, Michael Küppers, Hideyo Kawakita, Luisa M. Lara, Jessica Agarwal, Nicolas André, Nicholas Attree, Uli Auster, Stefano Bagnulo, Michele Bannister, Arnaud Beth, Neil Bowles, Andrew Coates, Luigi Colangeli, Carlos Corral van Damme, Vania Da Deppo, Johan De Keyser, Vincenzo Della Corte, Niklas Edberg, Mohamed Ramy El-Maarry, Sara Faggi, Marco Fulle, Ryu Funase, Marina Galand, Charlotte Goetz, Olivier Groussin, Aurélie Guilbert-Lepoutre, Pierre Henri, Satoshi Kasahara, Akos Kereszturi, Mark Kidger, Matthew Knight, Rosita Kokotanekova, Ivana Kolmasova, Konrad Kossacki, Ekkehard Kührt, Yuna Kwon, Fiorangela La Forgia, Anny-Chantal Levasseur-Regourd, Manuela Lippi, Andrea Longobardo, Raphael Marschall, Marek Morawski, Olga Muñoz, Antti Näsilä, Hans Nilsson, Cyrielle Opitom, Mihkel Pajusalu, Antoine Pommerol, Lubomir Prech, Nicola Rando, Francesco Ratti, Hanna Rothkaehl, Alessandra Rotundi, Martin Rubin, Naoya Sakatani, Joan Pau Sánchez, Cyril Simon Wedlund, Anamarija Stankov, Nicolas Thomas, Imre Toth, Geronimo Villanueva, Jean-Baptiste Vincent, Martin Volwerk, Peter Wurz, Arno Wielders, Kazuo Yoshioka, Konrad Aleksiejuk, Fernando Alvarez, Carine Amoros, Shahid Aslam, Barbara Atamaniuk, Jędrzej Baran, Tomasz Barciński, Thomas Beck, Thomas Behnke, Martin Berglund, Ivano Bertini, Marcin Bieda, Piotr Binczyk, Martin-Diego Busch, Andrei Cacovean, Maria Teresa Capria, Chris Carr, José María Castro Marín, Matteo Ceriotti, Paolo Chioetto, Agata Chuchra-Konrad, Lorenzo Cocola, Fabrice Colin, Chiaki Crews, Victoria Cripps, Emanuele Cupido, Alberto Dassatti, Björn J. R. Davidsson, Thierry De Roche, Jan Deca, Simone Del Togno, Frederik Dhooghe, Kerri Donaldson Hanna, Anders Eriksson, Andrey Fedorov, Estela Fernández-Valenzuela, Stefano Ferretti, Johan Floriot, Fabio Frassetto, Jesper Fredriksson, Philippe Garnier, Dorota Gaweł, Vincent Génot, Thomas Gerber, Karl-Heinz Glassmeier, Mikael Granvik, Benjamin Grison, Herbert Gunell, Tedjani Hachemi, Christian Hagen, Rajkumar Hajra, Yuki Harada, Johann Hasiba, Nico Haslebacher, Miguel Luis Herranz De La Revilla, Daniel Hestroffer, Tilak Hewagama, Carrie Holt, Stubbe Hviid, Iaroslav Iakubivskyi, Laura Inno, Patrick Irwin, Stavro Ivanovski, Jiri Jansky, Irmgard Jernej, Harald Jeszenszky, Jaime Jimenéz, Laurent Jorda, Mihkel Kama, Shingo Kameda, Michael S. P. Kelley, Kamil Klepacki, Tomáš Kohout, Hirotsugu Kojima, Tomasz Kowalski, Masaki Kuwabara, Michal Ladno, Gunter Laky, Helmut Lammer, Radek Lan, Benoit Lavraud, Monica Lazzarin, Olivier Le Duff, Qiu-Mei Lee, Cezary Lesniak, Zoe Lewis, Zhong-Yi Lin, Tim Lister, Stephen Lowry, Werner Magnes, Johannes Markkanen, Ignacio Martinez Navajas, Zita Martins, Ayako Matsuoka, Barbara Matyjasiak, Christian Mazelle, Elena Mazzotta Epifani, Mirko Meier, Harald Michaelis, Marco Micheli, Alessandra Migliorini, Aude-Lyse Millet, Fernando Moreno, Stefano Mottola, Bruno Moutounaick, Karri Muinonen, Daniel R. Müller, Go Murakami, Naofumi Murata, Kamil Myszka, Shintaro Nakajima, Zoltan Nemeth, Artiom Nikolajev, Simone Nordera, Dan Ohlsson, Aire Olesk, Harald Ottacher, Naoya Ozaki, Christophe Oziol, Manish Patel, Aditya Savio Paul, Antti Penttilä, Claudio Pernechele, Joakim Peterson, Enrico Petraglio, Alice Maria Piccirillo, Ferdinand Plaschke, Szymon Polak, Frank Postberg, Herman Proosa, Silvia Protopapa, Walter Puccio, Sylvain Ranvier, Sean Raymond, Ingo Richter, Martin Rieder, Roberto Rigamonti, Irene Ruiz Rodriguez, Ondrej Santolik, Takahiro Sasaki, Rolf Schrödter, Katherine Shirley, Andris Slavinskis, Balint Sodor, Jan Soucek, Peter Stephenson, Linus Stöckli, Paweł Szewczyk, Gabor Troznai, Ludek Uhlir, Naoto Usami, Aris Valavanoglou, Jakub Vaverka, Wei Wang, Xiao-Dong Wang, Gaëtan Wattieaux, Martin Wieser, Sebastian Wolf, Hajime Yano, Ichiro Yoshikawa, Vladimir Zakharov, Tomasz Zawistowski, Paola Zuppella, Giovanna Rinaldi, Hantao Ji
    Space Science Reviews, 220(1), Jan 24, 2024  Peer-reviewed
    Abstract Here we describe the novel, multi-point Comet Interceptor mission. It is dedicated to the exploration of a little-processed long-period comet, possibly entering the inner Solar System for the first time, or to encounter an interstellar object originating at another star. The objectives of the mission are to address the following questions: What are the surface composition, shape, morphology, and structure of the target object? What is the composition of the gas and dust in the coma, its connection to the nucleus, and the nature of its interaction with the solar wind? The mission was proposed to the European Space Agency in 2018, and formally adopted by the agency in June 2022, for launch in 2029 together with the Ariel mission. Comet Interceptor will take advantage of the opportunity presented by ESA’s F-Class call for fast, flexible, low-cost missions to which it was proposed. The call required a launch to a halo orbit around the Sun-Earth L2 point. The mission can take advantage of this placement to wait for the discovery of a suitable comet reachable with its minimum $\varDelta $V capability of $600\text{ ms}^{-1}$. Comet Interceptor will be unique in encountering and studying, at a nominal closest approach distance of 1000 km, a comet that represents a near-pristine sample of material from the formation of the Solar System. It will also add a capability that no previous cometary mission has had, which is to deploy two sub-probes – B1, provided by the Japanese space agency, JAXA, and B2 – that will follow different trajectories through the coma. While the main probe passes at a nominal 1000 km distance, probes B1 and B2 will follow different chords through the coma at distances of 850 km and 400 km, respectively. The result will be unique, simultaneous, spatially resolved information of the 3-dimensional properties of the target comet and its interaction with the space environment. We present the mission’s science background leading to these objectives, as well as an overview of the scientific instruments, mission design, and schedule.
  • G. Abdellaoui, S. Abe, J. H. Adams, D. Allard, G. Alonso, L. Anchordoqui, A. Anzalone, E. Arnone, K. Asano, R. Attallah, H. Attoui, M. Ave Pernas, R. Bachmann, S. Bacholle, M. Bagheri, M. Bakiri, J. Baláz, D. Barghini, S. Bartocci, M. Battisti, J. Bayer, B. Beldjilali, T. Belenguer, N. Belkhalfa, R. Bellotti, A. A. Belov, K. Benmessai, M. Bertaina, P. F. Bertone, P. L. Biermann, F. Bisconti, C. Blaksley, N. Blanc, S. Blin-Bondil, P. Bobik, M. Bogomilov, K. Bolmgren, E. Bozzo, S. Briz, A. Bruno, K. S. Caballero, F. Cafagna, G. Cambié, D. Campana, J. N. Capdevielle, F. Capel, A. Caramete, L. Caramete, R. Caruso, M. Casolino, C. Cassardo, A. Castellina, O. Catalano, A. Cellino, K. Černý, M. Chikawa, G. Chiritoi, M. J. Christl, R. Colalillo, L. Conti, G. Cotto, H. J. Crawford, R. Cremonini, A. Creusot, A. Cummings, A. de Castro Gónzalez, C. de la Taille, L. del Peral, J. Desiato, A. Diaz Damian, R. Diesing, P. Dinaucourt, A. Djakonow, T. Djemil, A. Ebersoldt, T. Ebisuzaki, J. Eser, F. Fenu, S. Fernández-González, S. Ferrarese, G. Filippatos, W. Finch, C. Fornaro, M. Fouka, A. Franceschi, S. Franchini, C. Fuglesang, T. Fujii, M. Fukushima, P. Galeotti, E. García-Ortega, D. Gardiol, G. K. Garipov, E. Gascón, E. Gazda, J. Genci, A. Golzio, P. Gorodetzky, R. Gregg, A. Green
    Astroparticle Physics, 154, Jan, 2024  
    The Extreme Universe Space Observatory on a Super Pressure Balloon 1 (EUSO-SPB1) was launched in 2017 April from Wanaka, New Zealand. The plan of this mission of opportunity on a NASA super pressure balloon test flight was to circle the southern hemisphere. The primary scientific goal was to make the first observations of ultra-high-energy cosmic-ray extensive air showers (EASs) by looking down on the atmosphere with an ultraviolet (UV) fluorescence telescope from suborbital altitude (33 km). After 12 days and 4 h aloft, the flight was terminated prematurely in the Pacific Ocean. Before the flight, the instrument was tested extensively in the West Desert of Utah, USA, with UV point sources and lasers. The test results indicated that the instrument had sensitivity to EASs of ⪆3 EeV. Simulations of the telescope system, telescope on time, and realized flight trajectory predicted an observation of about 1 event assuming clear sky conditions. The effects of high clouds were estimated to reduce this value by approximately a factor of 2. A manual search and a machine-learning-based search did not find any EAS signals in these data. Here we review the EUSO-SPB1 instrument and flight and the EAS search.
  • Kohji Tsumura, Shuji Matsuura, Kei Sano, Takahiro Iwata, Hajime Yano, Kohei Kitazato, Kohji Takimoto, Manabu Yamada, Tomokatsu Morota, Toru Kouyama, Masahiko Hayakawa, Yasuhiro Yokota, Eri Tatsumi, Moe Matsuoka, Naoya Sakatani, Rie Honda, Shingo Kameda, Hidehiko Suzuki, Yuichiro Cho, Kazuo Yoshioka, Kazunori Ogawa, Kei Shirai, Hirotaka Sawada, Seiji Sugita
    Earth, Planets and Space, 75(121), Jun 4, 2023  Peer-reviewed
    The zodiacal light (ZL) is sunlight scattered by interplanetary dust (IPD) in the optical wavelengths. The spatial distribution of IPD in the Solar system may hold an important key to understanding the evolution of the Solar system and material transportation within it. The IPD number density can be expressed as n(r)∼r^{−α}, and the result of α∼1.3 was obtained by the previous observations from the interplanetary space by Helios 1/2 and Pioneer 10/11 in the 1970s and 1980s. However, no direct measurements of α based on the ZL observation from the interplanetary space outside the Earth's orbit have been conducted since then. Here we introduce the initial result of the ZL radial profile at optical wavelengths observed at 0.76-1.06 au by ONC-T with Hayabusa2# mission in 2021-2022. The obtained ZL brightness is well reproduced by the model brightness, but there is a small excess of the observed ZL brightness over the model brightness at around 0.9 au. The obtained radial power-law index is α=1.30±0.08, which is consistent with the previous results based on the ZL observations. The dominant uncertainty source in α arises from the uncertainty in the Diffuse Galactic Light estimation.

Misc.

 489
  • 平井隆之, 矢野創
    日本惑星科学会秋季講演会予稿集(Web), 2014 "O13-01", 2014  
  • 岡本千里, 池崎克俊, 今栄直也, 矢野創, 橘省吾, 土山明, 澤田弘崇, 長谷川直, 中村昭子, 富山隆將
    日本惑星科学会秋季講演会予稿集(Web), 2014 "O11-01", 2014  
  • KAZAMA Ryo, YANO Hajime, KURODA Yoji, ADACHI Tadashi, KIKUCHI Yoshitaka, OTA Kohei, TSUMAKI Yuichi, SUGAI Atsuhisa, MINETA Takashi, TADAKUMA Riichiro, YOSHIMITSU Tetsuo, KUBOTA Takashi
    The Proceedings of JSME annual Conference on Robotics and Mechatronics (Robomec), 2014 _1P2-K03_1-_1P2-K03_2, 2014  
    JAXA is planning to launch Hayabusa 2 in December 2014. Hayabusa 2 will be equipped with an asteroid exploration rover which is developed by the consortium of universities. A goal of the rover is establishment of the technology for locomotion on asteroid surface. In our previous work, we proposed a new moving mechanism called "Environment-Driven Torquer, EDT." The EDT is driven by environment temperature with bimetal. In other words, the EDT can move the rover without both battery and CPU. We have developed an engineering model with magnet latch. In this paper, performance evaluation of the EDT is executed by free-fall experiments in ZARM.
  • Yano Hajime, Yamagishi Akihiko, Hashimoto Hirofumi, Yokobori Shin-ichi, Kobayashi Kensei, Yabuta Hikaru, Mita Hajime, Tabata Makoto, Kawai Hideyuki, Higashide Masumi, Okudaira Kyoko, Sasaki Satoshi, Imai Eiichi, Kawaguchi Yuko, Uchibori Yukio, Kodaira Satoshi, Tanpopo Project Team
    Dec, 2013  
    International Astrobiology Workshop 2013 (November 28-30, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan
  • Kiyonaga Yusuke, Sasaki Satoshi, Odashima T., Okudaira Kyoko, Imai Eiichi, Yano Hajime, Kawaguchi Yuko, Yamagishi Akihiko
    Dec, 2013  
  • 岡本 千里, 池崎 克俊, 今栄 直也, 矢野 創, 橘 省吾, 土`山 明, 澤田 弘崇, 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, 2013 "O8-03", Nov 20, 2013  
  • Chisato Okamoto, Hajime Yano, Makoto Tanaka, Takayuki Hirai, Sunao Hasegawa, Makoto Tabata, Naoko Ogawa, Takeo Iwai, Kyoko Okudaira
    Proceedings of Japan Geoscience Union Meeting 2013, U07-P2, May, 2013  
  • ARAKAWA Masahiko, SAIKI Takanao, WADA Koji, KADONO Toshihiko, TAKAGI Yasuhiko, OKAMOTO Chisato, YANO Hajime, HAYAKAWA Masahiko, NAKAZAWA Satoru, HIRATA Naru, KOBAYASHI Masanori, MICHEL Patrick, JUTZI Martin, IMAMURA Hiroshi, OGAWA Kazunori, IIJIMA Yuichi, HONDA Rie, ISHIBASHI Ko, HAYAKAWA Hajime, SAWADA Hirotaka
    The proceedings of 44th Lunar and Planetary Science Conference, abstract 1904, Mar, 2013  
  • 森治, 佐伯孝尚, 白澤洋次, 津田雄一, 松浦周二, 矢野創, 船瀬龍, 中村良介, 米徳大輔
    日本航空宇宙学会年会講演会講演集(CD-ROM), 44th, 2013  
  • 岩田稔, 本田一貴, 岡本千里, 矢野創
    宇宙科学技術連合講演会講演集(CD-ROM), 57th, 2013  
  • 船瀬龍, 森治, 白澤洋次, 津田雄一, 矢野創
    航空原動機・宇宙推進講演会講演論文集(CD-ROM), 53rd, 2013  
  • 小田島拓, 松本剛征, 矢口勇一, 奥平恭子, 清永悠介, 佐々木聰, 矢野創, 今井栄一, 出村裕英, 山岸明彦
    可視化情報学会誌, 33(Suppl.2), 2013  
  • 横堀伸一, 山岸明彦, 小林憲正, 矢野創, 田端誠, 山下雅道, 橋本博文, 奥平恭子, 薮田ひかる, 今井栄一, 三田肇, 丸茂克美, 河合秀幸, 河口優子, 川本幸徳, SARKER Palash Kumar, 江藤碧, 古川天
    スペース・プラズマ研究会・講演集(Web), 2012 25 (WEB ONLY), 2013  
  • 奥平恭子, 長谷川直, 小野瀬直美, 矢野創, 田端誠, 河合秀幸
    可視化情報学会誌, 33(Suppl.2) 217‐218, 2013  
  • 横堀伸一, 河口優子, 清水康之, 川尻成俊, 白石啓祐, 杉野朋弘, 高橋勇太, YANG Yinjie, 谷川能章, 橋本博文, 林宣宏, 東出真澄, 今井栄一, 河合秀幸, 小林憲正, 三田肇, 中川和道, 鳴海一成, 奥平恭子, 佐藤勝也, 田端誠, 富田(横谷)香織, 薮田ひかる, 矢野創, 吉田聡, 山岸明彦
    Viva Origino, 41(Supplement) 20, 2013  
  • Yokobori Shin-ichi, Kawaguchi Yuko, Shimizu Yasuyuki, Kawashiri Narutoshi, Shiraishi Keisuke, Sugino Tomohiro, Takahashi Yuta, Yang Yinjie, Tanigawa Yoshiaki, Hashimoto Hirofumi, Hayashi Nobuhiro, Higashide Masumi, Imai Eiichi, Kawai Hideyuki, Kobayashi Kensei, Mita Hajime, Nakagawa Kazumichi, Narumi Issay, Okudaira Kyoko, Satoh Katsuya, Tabata Makoto, Tomita-Yokotani Kaori, Yabuta Hikaru, Yano Hajime, Yoshida Satoshi, Yamagishi Akihiko, TANPOPO WG
    Viva origino, 41 20-20, 2013  
  • 小林 憲正, 古川 天, 川本 幸徳, 金子 竹男, 大林 由美子, 三田 肇, 奥平 恭子, 矢野 創, 田端 誠, 橋本 博文, 横堀 伸一, 山岸 明彦, たんぽぽWG
    Abstracts Fall Meeting of the Japanese Society for Planetary Sciences, 2013 "O5-02", 2013  
  • 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, 2 1239-1250, 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, 3 1642-1653, 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, 3 1636-1641, 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.
  • Takayuki Hirai, Hajime Yano, Chisato Okamoto, Naoko Ogawa, Sunao Hasegawa, Makoto Tabata, Masayuki Fujii, Makoto Tanaka, Takeo Iwai, Kyoko Okudaira
    Proceedings of 45th ISAS Lunar and Planetary Symposium, Aug, 2012  
  • MITSUTA Tomohiko, YANO Hajime, HIRATA Naru, WADA Koji, ARAKAWA Masahiko
    Proceedings of 39th COSPAR Scientific Assembly, B0.4-0016-12, Jul, 2012  
  • MITSUTA Tomohiko, HIRATA Naru, WADA Koji, YANO Hajime, ARAKAWA Masahiko
    Proceedings of Asteroids, Comets, Meteors 2012, abstract 6476, May, 2012  
  • Hajime Yano, Takayuki Hirai, Chisato Okamoto, Masayuki Fujii, Naoko Ogawa, Makoto Tanaka, IKAROS-ALADDIN Team
    12th Space Science Symposium, P3-053, Jan, 2012  
  • 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
    日本惑星科学会秋季講演会予稿集(Web), 2012 114-114, 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), 56th ROMBUNNO.1S20, 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), 56th ROMBUNNO.3A16, 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), 2011 39 (WEB ONLY), 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, 28th 230-232, 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, 28th 228-229, 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, 28th 220-223, 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, 40(Supplement) 29-29, 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, GRUEN Eberhart
    日本惑星科学会秋季講演会予稿集(Web), 2012 26-26, 2012  
  • Takanao Saiki, Hirotaka Sawada, Chisato Okamoto, Hajime Yano, Yasuhiko Takagi, Yasuhiro Akahoshi, Makoto Yoshikawa
    62nd International Astronautical Congress 2011, IAC 2011, 2 1343-1348, 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.
  • YANO Hajime
    The journal of the Japanese Society for Dental Materials and Devices, 30(5) 291-291, Sep 25, 2011  
  • Hajime Yano, Takayuki Hirai, Chisato Okamoto, Naoko Ogawa, Makoto Tanaka, The IKAROS-ALADDIN Team
    Abstracts of 8th Annual General Meeting of Asia Oceania Geosciences Society (AOGS 2011), PS02-A047, Aug, 2011  Peer-reviewed
  • Hajime Yano, Takayuki Hirai, Chisato Okamoto, Naoko Ogawa, Makoto TANAKA, IKAROS-ALADDIN Team
    Proceedings of The 21st Workshop on Astrodynamics and Flight Mechanics, Jul, 2011  
  • KOBAYASHI Masanori, MIYACHI Takashi, NAKAMURA Maki H., SUGITA Seiji, IWAI Takeo, TAKECHI Seiji
    2011(19) 43-48, Jun 30, 2011  
  • Hajime Yano, Takayuki Hirai, Chisato Okamoto, Naoko Ogawa, Makoto TANAKA, IKAROS-ALADDIN Team
    Proceedings of Japan Geoscience Union Meeting 2011, PPS022-13, May, 2011  
  • Hajime Yano, Makoto Tanaka, Chisato Okamoto, Takayuki Hirai, Naoko Ogawa, Sunao Hasegawa, Takeo Iwai, Kyoko Okudaira
    Abstracts of 42nd Lunar and Planetary Science Conference (LPSC 2011), 2647, Mar, 2011  Peer-reviewed
  • Morishita Hiroyuki, Morii Shota, Matunaga Saburo, Yano Hajime, Okamoto Chisato
    2010(19) "K2-1"-"K2-5", 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 analysis of the sampling mechanism are described and discussed.
  • 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
    日本惑星科学会秋季講演会予稿集(Web), 2011 85-85, 2011  
  • 岡田達明, 矢野創, 津田雄一, 久保田孝, 吉光徹雄, HO Tra-Mi, WITTE Lars, ULAMEC Stephan, DITTUS Hans-Joerg, SPOHN Tilman, BIBRING Jean-Pierre, BOUSQUET Pierre
    日本惑星科学会秋季講演会予稿集(Web), 2011 124-124, 2011  
  • OGATA YUICHIRO, Imai Eichi, Hashimoto Hirofumi, Mita Hajime, Kobayashi Kensei, Yano Hajime, Yamashita Masamichi, Yamagishi Akihiko, TANPOPO Working Group, Yabuta Hikaru, Nakashima Satoru, Okudaira Kyoko, Moriwaki Taro, Ikemoto Yuka, Hasegawa Sunao, Tabata Makoto, Yokobori Shinichi
    Abstracts of Annual Meeting of the Geochemical Society of Japan, 58th 175-175, 2011  
    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。
  • Morishita Hiroyuki, Morii Shota, Matunaga Saburo, Yano Hajime, Okamoto Chisato
    The Proceedings of the Space Engineering Conference, 19th _K2-1_-_K2-5_, 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 analysis of the sampling mechanism are described and discussed.
  • 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, 53rd 173-175, 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), 55th ROMBUNNO.3A15, 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, 39(Supplement) 1-1, 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), 20th 24 (WEB ONLY), 2011  
  • Yoshimura Yoshitaka, Hashimoto Hirofumi, Yokobori Shinichi, Yano Hajime, Mita Hajime, Tabata Makoto, Kobayashi Kensei, Yamashita Masamichi, Kawasaki Yukishige
    宇宙利用シンポジウム, 27th(26) 181-182, 2011  
    Search for extraterrestrial life is an important scientific issue, since it is associated with fundamental question of science, such as the origin of life or universal concepts of biology. However, astrobiology requires a road map that summarizes research subjects and the perspective of space missions. This study team aim to define our road map based on the latest achievements of planetary science and current plans of astrobiology in worldwide. Among many research subjects, we focus on a case study of search for life on Mars. In this report, we discussed the road map to search extraterrestrial life, biomarkers, and instruments.joint hosting: The Science Council of Japan

Books and Other Publications

 30

Presentations

 505

Teaching Experience

 5

Works

 26

Research Projects

 38

Industrial Property Rights

 8

Academic Activities

 5
  • Review, evaluation
    日本学術振興会, Jul 1, 2021 - Jun 30, 2023
  • Review, evaluation
    日本学術振興会, Jul 1, 2021 - Jun 30, 2023
  • Review, evaluation
    日本学術振興会, Jul 1, 2021 - Jun 30, 2023
  • Planning/Implementing academic research
    Keck Institute for Space Studies, California Institute of Technology, USA (Keck Institute for Space Studies, California Institute of Technology, USA), Oct 24, 2022 - Apr, 2023
    Long-period comets (LPCs) and interstellar objects (ISOs) are under-explored yet fascinating targets for planetary science, planetary defense, and astrophysics. LPCs contain volatiles preserved from the formation of the solar system and sampling those pristine ices would provide key data points to constrain the temperature and chemistry of the protoplanetary disk and early solar system dynamics. ISOs are mysterious targets of which we have only identified two so far, but are predicted to be numerous. ISOs are samples of exoplanetary systems and their in-situ exploration would bring additional perspective to our understanding of the solar system formation. While fascinating, these targets also are extremely challenging to explore closely, often arriving with little lead times, with extremely high energies, and on poorly constrained trajectories. To date, no dedicated spacecraft has been sent to explore an ISO or LPC. The short detection times before solar system departure associated with ISOs are incompatible with traditional spacecraft development schedules and funding timelines. Near Earth Object (NEO) exploration and, especially, potentially hazardous asteroid (PHA) mitigation and planetary defense share similar characteristics. The short-notice of a PHA would necessitate similar technical strategies to rapidly mitigate a potential impact. This one-week KISS workshop will unite experts in small bodies science, relevant instruments, ISO and LPC design, and mission implementation to tackle some of the most challenging aspects of developing and executing a mission to an LPC, ISO, or NEO. While the community has been unable to obtain key measurement requirements for the past LPCs and ISOs that have flown near Earth, through focused study, community building, and concept development, we can work to ensure that there are no more missed opportunities in the future!
  • Review, evaluation
    日本学術振興会, Dec, 2019 - Jan, 2020

Social Activities

 2

Media Coverage

 24

Other

 7

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)
    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
  • 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)
    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)
    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)
    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)
    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)
    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)
    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)
    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)
    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)

● 指導学生等の数

 6
  • 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
  • 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
    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

● 指導学生の表彰・受賞

 4
  • 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
  • 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
    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
    日本学術振興会特別研究員(DC)
    Date
    2023年4月

● 指導学生の顕著な論文

 23
  • Student name
    Shoya IWATA
    Student affiliation
    法政大学大学院(連携大学院生)
    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
    Francesc TINTO
    Student affiliation
    仏・国際宇宙大学院(夏季インターン学生)
    Author(s), journal, volume number, pagination (year of publication)
    ISUーMSS修士論文 Individual Project Report (2002)
    Title
    Evaluation of Effects of Regolith Size Distribution on Visible Near IR Asteroid Spectroscopy
  • Student name
    Serina DINIEGA
    Student affiliation
    仏・国際宇宙大学院
    Author(s), journal, volume number, pagination (year of publication)
    ISUーMSS修士論文 Individual Project Report (2004)
    Title
    Regolith Distribution Model for Sub-kilometer Ellipsoidal Asteroids
  • Student name
    Keisuke TERAMOTO
    Student affiliation
    東京大学大学院
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2005)
    Title
    Measurements of Sound Speed in Granular Materials Simulated Regolith
  • Student name
    Kyoko OKUDAIRA
    Student affiliation
    総合研究大学院大学
    Author(s), journal, volume number, pagination (year of publication)
    博士論文(2006)
    Title
    Evaluation of Micrometeoroid Analogs Alteration on Capturing by Aerogel
  • Student name
    Teruo MAKABE
    Student affiliation
    東京大学大学院
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2007)
    Title
    The Determination of Projectile Shape for Asteroid Impact Sampling System
  • Student name
    Takayuki HIRAI
    Student affiliation
    総合研究大学院大学
    Author(s), journal, volume number, pagination (year of publication)
    博士論文(2014)
    Title
    A New Cosmic Dust Distribution Model inside the Earth’s Orbit Based on IKAROS-ALADDIN Results
  • Student name
    Hiroyuki MOCHIZUKI
    Student affiliation
    法政大学大学院(連携大学院生)
    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
  • 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
    Ritsuko JITSUKAWA
    Student affiliation
    法政大学大学院(連携大学院生)
    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
    Eigo ISHIKAWA
    Student affiliation
    法政大学大学院(連携大学院生)
    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
    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
    Keita YAMAMOTO
    Student affiliation
    法政大学大学院(連携大学院生)
    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(連携大学院生)
    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(連携大学院生)
    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
    Kosuke KANDO
    Student affiliation
    法政大学大学院(連携大学院生)
    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(連携大学院生)
    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
    Ryota SERIZAWA
    Student affiliation
    法政大学大学院(連携大学院生)
    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
    Yuki TAKEDA
    Student affiliation
    法政大学大学院(連携大学院生)
    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
    Kota ISAWA
    Student affiliation
    法政大学大学院(連携大学院生)
    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

● 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

 3
  • 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
  • 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
    2023年6月ー現在 科学データ利用委員会・委員