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
  • Okamoto, C, Ikezaki, K, Imae, N, Yano, H, Tachibana, S, Tsuchiyama, A, Sawada, H, Nakamura, A. M, Tomiyama, T
    44th LPSC, id. 2981, Mar, 2013  
  • A. Yamagishi, S. Yokobori, H. Hashimoto, H. Yano, M. Higashide, M. Tabata, E. Imai, H. Yabuta, K. Kobayashi, H. Kawai
    ISTS Web Paper Archive, 2013(k-49) 1-7, 2013  Peer-reviewed
  • Y. Ogata, H. Yabuta, S. Nakashima, T. Moriwaki, Y. Ikemoto, S. Hasegawa, M. Tabata, S. Yokobori, H. Mita, K. Kobayashi, E. Imai, H, Hashimoto, Y. Kawaguchi, T. Sugino, H. Yano, A. Yamagishi
    ISTS Web Paper Archive, 2013(r-51p) 1-5, 2013  Peer-reviewed
  • A. Yamagishi, S. -I. Yokobori, Y. Yoshimura, M. Yamashita, H. Hashimoto, T. Kubota, H. Yano, J. Haruyama, M. Tabata, K. Kobayashi, H. Honda, Y. Utsumi, T. Itoh, K. Hamase, T. Naganuma, S. Sasaki, H. Miyamoto
    PALEONTOLOGICAL JOURNAL, 46(9) 1087-1088, Dec, 2012  
  • Peter Tsou, Donald E. Brownlee, Christopher P. McKay, Ariel D. Anbar, Hajime Yano, Kathrin Altwegg, Luther W. Beegle, Richard Dissly, Nathan J. Strange, Isik Kanik
    ASTROBIOLOGY, 12(8) 730-742, Aug, 2012  Peer-reviewed
    Life Investigation For Enceladus (LIFE) presents a low-cost sample return mission to Enceladus, a body with high astrobiological potential. There is ample evidence that liquid water exists under ice coverage in the form of active geysers in the "tiger stripes" area of the southern Enceladus hemisphere. This active plume consists of gas and ice particles and enables the sampling of fresh materials from the interior that may originate from a liquid water source. The particles consist mostly of water ice and are 1-10 mu in diameter. The plume composition shows H2O, CO2, CH4, NH3, Ar, and evidence that more complex organic species might be present. Since life on Earth exists whenever liquid water, organics, and energy coexist, understanding the chemical components of the emanating ice particles could indicate whether life is potentially present on Enceladus. The icy worlds of the outer planets are testing grounds for some of the theories for the origin of life on Earth.The LIFE mission concept is envisioned in two parts: first, to orbit Saturn (in order to achieve lower sampling speeds, approaching 2 km/s, and thus enable a softer sample collection impact than Stardust, and to make possible multiple flybys of Enceladus); second, to sample Enceladus' plume, the E ring of Saturn, and the Titan upper atmosphere. With new findings from these samples, NASA could provide detailed chemical and isotopic and, potentially, biological compositional context of the plume. Since the duration of the Enceladus plume is unpredictable, it is imperative that these samples are captured at the earliest flight opportunity. If LIFE is launched before 2019, it could take advantage of a Jupiter gravity assist, which would thus reduce mission lifetimes and launch vehicle costs. The LIFE concept offers science returns comparable to those of a Flagship mission but at the measurably lower sample return costs of a Discovery-class mission.
  • R. Srama, H. Krueger, T. Yamaguchi, T. Stephan, M. Burchell, A. T. Kearsley, V. Sterken, F. Postberg, S. Kempf, E. Gruen, N. Altobelli, P. Ehrenfreund, V. Dikarev, M. Horanyi, Z. Sternovsky, J. D. Carpenter, A. Westphal, Z. Gainsforth, A. Krabbe, J. Agarwal, H. Yano, J. Blum, H. Henkel, J. Hillier, P. Hoppe, M. Trieloff, S. Hsu, A. Mocker, K. Fiege, S. F. Green, A. Bischoff, F. Esposito, R. Laufer, T. W. Hyde, G. Herdrich, S. Fasoulas, A. Jaeckel, G. Jones, P. Jenniskens, E. Khalisi, G. Moragas-Klostermeyer, F. Spahn, H. U. Keller, P. Frisch, A. C. Levasseur-Regourd, N. Pailer, K. Altwegg, C. Engrand, S. Auer, J. Silen, S. Sasaki, M. Kobayashi, J. Schmidt, J. Kissel, B. Marty, P. Michel, P. Palumbo, O. Vaisberg, J. Baggaley, A. Rotundi, H. P. Roeser
    EXPERIMENTAL ASTRONOMY, 33(2-3) 723-751, Apr, 2012  Peer-reviewed
    The Stardust mission returned cometary, interplanetary and (probably) interstellar dust in 2006 to Earth that have been analysed in Earth laboratories worldwide. Results of this mission have changed our view and knowledge on the early solar nebula. The Rosetta mission is on its way to land on comet 67P/Churyumov-Gerasimenko and will investigate for the first time in great detail the comet nucleus and its environment starting in 2014. Additional astronomy and planetary space missions will further contribute to our understanding of dust generation, evolution and destruction in interstellar and interplanetary space and provide constraints on solar system formation and processes that led to the origin of life on Earth. One of these missions, SARIM-PLUS, will provide a unique perspective by measuring interplanetary and interstellar dust with high accuracy and sensitivity in our inner solar system between 1 and 2 AU. SARIM-PLUS employs latest in-situ techniques for a full characterisation of individual micrometeoroids (flux, mass, charge, trajectory, composition()) and collects and returns these samples to Earth for a detailed analysis. The opportunity to visit again the target comet of the Rosetta mission 67P/Churyumov-Gerasimeenternko, and to investigate its dusty environment six years after Rosetta with complementary methods is unique and strongly enhances and supports the scientific exploration of this target and the entire Rosetta mission. Launch opportunities are in 2020 with a backup window starting early 2026. The comet encounter occurs in September 2021 and the reentry takes place in early 2024. An encounter speed of 6 km/s ensures comparable results to the Stardust mission.
  • Hajime Yano
    Parity, 27(8) 31-32, 2012  Peer-reviewedInvitedLead authorCorresponding author
  • Sho SASAKI, Masaki FUJIMOTO, Hajime YANO, Takeshi TAKASHIMA, Yasumasa KASABA, Yukihiro TAKAHASHI, Jun KIMURA, Yuichi TSUDA, Ryu FUNASE, Osamu MORI, Stefano CAMPAGNOLA, Yasuhiro KAWAKATSU
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, 10(ists28) Tk_37-Tk_40, 2012  Peer-reviewed
  • Sekine Y., Yabuta H., Kimura J., Furukawa Y., Takano Y., Yano H., Funase R., Takai K., Ishihara M., Shibuya T., Tachibana S., Kuramoto K.
    Planetary People - The Japanese Society for Planetary Sciences, 21(3) 229-238, 2012  Peer-reviewed
    エンセラダスの南極付近から噴出するプリュームの発見は,氷衛星の内部海の海水や海中の揮発性成分や固体成分の直接サンプリングの可能性を示した大きなブレイクスルーであるといえる.これまでカッシーニ探査によって,プリューム物質は岩石成分と相互作用する液体の内部海に由来していることが明らかになったが,サンプリング時の相対速度が大きいこと,質量分析装置の分解能が低いことなどの問題があり,内部海の化学組成や温度条件,海の存続時間など,生命存在の可能性を制約できる情報は乏しい.本論文では,エンセラダス・プリューム物質の高精度その場質量分析とサンプルリターンによる詳細な物質分析を行うことで,内部海の化学組成の解明,初期太陽系物質進化の制約,そして生命存在可能性を探ることを目的とする探査計画を提案する.本提案は,"宇宙に生命は存在するのか"という根源的な問いに対して,理・工学の様々な分野での次世代を担う若手研究者が惑星探査に参入し結集する点が画期的であり,我が国の科学・技術界全体に対しても極めて大きな波及効果をもつ.
  • Nakamura R., Matsuura S., Funase R., Yano H., Mori O., Tsuda Y., Yoshida F., Takato N., Kokubo E.
    Planetary People - The Japanese Society for Planetary Sciences, 21(3) 253-259, 2012  Peer-reviewed
    原始太陽系円盤を構成していた初期物質を探るためには,惑星形成時の熱変成の影響を免れた小惑星・彗星・惑星間塵といった小天体の研究が不可欠である.なかでも木星のラグランジュ点付近に存在するトロヤ群小惑星は,小惑星と彗星の間をつなぐ天体であり,原始太陽系円盤の物質分布や微惑星の成長・移動プロセスを調べる上で重要なターゲットである.本稿では,日本が世界に先駆けて実証したソーラー電力セイル技術を用いたトロヤ群小惑星探査ミッションを提案する.この探査は(1)トロヤ群小惑星の詳細な物質組成や熱史・衝突史を調べることで,その起源と進化を明らかにする, (2)惑星間塵の空間分布を測定することで,彗星・小惑星からの生成率や軌道進化に関する理解を深め,その結果を他の惑星系に応用する, (3)惑星間塵の影響の少ない小惑星帯以遠からの宇宙赤外線背景放射観測によって,宇宙初期に形成された第一世代の星を調べる,という科学目標をあわせ持つ,惑星科学・天文学・宇宙工学の融合ミッションである.
  • Makoto Tabata, Yuko Kawaguchi, Shin-ichi Yokobori, Hideyuki Kawai, Jun-ichi Takahashi, Hajime Yano, Akihiko Yamagishi
    Biol Sci Space, 25(1) 7-12, Dec 29, 2011  Peer-reviewed
    Hydrophobic silica aerogels with ultra-low densities have been designed and developed as cosmic dust capture media for the Tanpopo mission which is proposed to be carried out on the International Space Station. Glass particles as a simulated cosmic dust with 30 \mu m in diameter and 2.4 g/cm^3 in density were successfully captured by the novel aerogel at a velocity of 6 km/s. Background levels of contaminated DNA in the ultra-low density aerogel were lower than the detection limit of a polymerase chain reaction assay. These results show that the manufactured aerogel has good performance as a cosmic dust collector and sufficient quality in respect of DNA contamination. The aerogel is feasible for the biological analyses of captured cosmic dust particles in the astrobiological studies.
  • Katsuhito Ohtsuka, Shinsuke Abe, Takashi Ito, Tomoki Nakamura, Masanao Abe, Hajime Yano, Jun-ichi Watanabe
    PUBLICATIONS OF THE ASTRONOMICAL SOCIETY OF JAPAN, 63(6) L73-L77, Dec, 2011  Peer-reviewed
    Making a survey of Itokawids, i.e., meteor(oid)s originating from Apollo-type near-Earth Asteroid (25143) ltokawa, from among the multiple-station optical meteor orbit data, and employing several orbital similarity criteria, we found five Itokawid candidates. Furthermore, we classified the Itokawid candidates in meteorite types according to their physical data. The physical analyses indicate that all of the candidates evidently belong to not cometary, but asteroidal, meteoroids. Especially, the fireball, MORP 172, is the one candidate that is classified among ordinary/carbonaceous chondrites, as against the four other at carbonaceous chondrites. Hence, the classified meteoritic matter of MORP 172 shows more similarities to Itokawa's surface composition of an LL chondrite analogue than those of the other candidates. Therefore, the fireball is considered to be the strongest of the Itokawid candidates.
  • Ryosuke Nakamura, Bo Chen, Masashi Matsuoka, Hirokazu Yamamoto, Akihide Kamei, Kazuki Nakamura, Hajime Yano
    PUBLICATIONS OF THE ASTRONOMICAL SOCIETY OF JAPAN, 63(5) 995-1001, Oct, 2011  Peer-reviewedLast author
    HAYABUSA was the first asteroid sample return mission launched from Uchinoura, Japan in 2003. The sample capsule re-entered the Earth's atmosphere at approximately 13:50 (UT) on 2010 June 13th, and safely landed on the Woomera Prohibited Area (WPA) in Australia. The capsule had to be found and retrieved as soon as possible to reduce any contamination risk. On the morning of the June 13th and 14th, the landing area was imaged by using Remote Sensing Instrument (RSI) onboard the Formosat-2 satellite to locate the HAYABUSA re-entry module, consisting of a capsule and a parachute. In spite of an accurate geometric registration and radiance comparison of the image pair, no statistically significant radiance variation was found on the landing site. It was demonstrated through this experiment, however, that satellite imagery could be a promising backup tool for the prompt discovery and retrieval of the sampling capsule of the HAYABUSA follow-on mission if we can utilize space-borne imagers with sub-meter spatial resolution and short revisit capability.
  • A. Yamagishi, S. Yokobori, M. Yoshimura, H. Hashimoto, T. Kubota, H. Yano, J. Haruyama, M. Tabata, K. Kobayashi, H. Honda, Y. Utsumi, T. Saiki, T. Itoh, A. Miyakawa, K. Hamase, T. Naganuma, H. Mita, K. Tonokura, S. Sasaki, H. Miyamoto
    ISTS Web Paper Archives, 2001(k-15) 1-6, 2011  Peer-reviewed
    JAXAが検討している火星探査において,生命探査を行う意義について述べ,具体的方法を提案した。
  • S. Yokobori, Y. Yang, K. Fujisaki, Y. Kawaguchi, T. Sugino, H. Hashimoto, K. Okudaira, M. Tabata, H. Kawai, Y. Yoshimura, T. Tsuji, I. Narumi, N. Hayashi, H. Yano, M. Yamashita, K. Kobayashi, A. Yamagishi, Wg Tanpopo
    ORIGINS OF LIFE AND EVOLUTION OF BIOSPHERES, 40(6) 547-548, Dec, 2010  
    微生物の惑星間移動および地球外有機物の地球への伝搬を検証するための宇宙実験「たんぽぽ」について,その目的と準備状況について述べた。
  • YAMAGISHI Akihiko, YOKOBORI Shin-ichi, YOSHIMURA Yoshitaka, YAMASHITA Masamichi, HASHIMOTO Hirofumi, KUBOTA Takashi, YANO Hajime, HARUYAMA Junichi, TABATA Makoto, KOBAYASHI Kensei, HONDA Hajime, UTSUMI Yuichi, SAIKI Tsunemasa, ITOH Takashi, MIYAKAWA Atsuo, HAMASE Kenji, NAGANUMA Takeshi, MITA Hajime, TONOKURA Kenichi, SASAKI Sho, MIYAMOTO Hideaki
    Biological sciences in space, 24(2) 67-82, Oct 1, 2010  Peer-reviewed
  • Masatoshi Hirabayashi, Mutsuko Y. Morimoto, Hajime Yano, Jun'ichiro Kawaguchi, Julie Bellerose
    ICARUS, 206(2) 780-782, Apr, 2010  Peer-reviewed
    This note discusses the stability of collinear equilibrium points around a rotating system composed of two masses rigidly connected by a massless rod in the case, where the centripetal force outweighs the gravitational force. It is found that a stable region appears at L(1) when the ratio of gravitational to centripetal acceleration is less than 0.125, and that there is always no stable area at L(2) and L(3); the result is applied to the fast rotating Asteroid 2000EB(14). (C) 2009 Elsevier Inc. All rights reserved.
  • Takaaki Noguchi, Akira Tsuchiyama, Naru Hirata, Hirohide Demura, Ryosuke Nakamura, Hideaki Miyamoto, Hajime Yano, Tomoki Nakamura, Jun Saito, Sho Sasaki, Tatsuaki Hashimoto, Takashi Kubota, Masateru Ishiguro, Michael E. Zolensky
    ICARUS, 206(1) 319-326, Mar, 2010  Peer-reviewed
    On the sub-kilometer S-type asteroid, 25143 Itokawa, some boulders on rough terrains seem to be exposed without any powdery material covering. Based on surface morphological features, there are two major types of boulders: one has rounded edges and corners (rounded boulders), while the other has angular edges and corners (angular boulders). The surface features of the rounded boulders suggest that they have hardness heterogeneity and that some may be breccias. The angular boulders appear to be more resistant to impact disruption than the rounded ones, which may be due to a difference in lithology. The major constituents of Itokawa may be LL chondrite-like brecciated lithology (rounded boulders) along with a remarkable number of boulders suggesting that lithology is atypical among LL chondrites (angular boulders). Some of both types of boulders contain intersecting and stepped planar foliations. Comparison with meteorite ALH76009 suggests that the planar foliations may be marks where rocks were torn apart. As lithified breccias cannot be formed on present-day sub-kilometer-sized Itokawa, it is reasonable that boulders with various lithologies on Itokawa were formed on its large ancestor(s). The rubble-pile structure of Itokawa suggested by its low density (similar to 1.9 g/cm(3)) indicates that boulders on Itokawa are reassembled fragments formed by catastrophic disruption of large ancestor(s). (C) 2009 Elsevier Inc. All rights reserved.
  • KOSCHNY Detlef, BARUCCI Antonella, YOSHIKAWA Makoto, BÖHNHARDT Hermann, BRUCATO John, CORADINI Marcello, DOTTO Elisabetta, FRANCHI Ian, F. GREEN Simon, JOSSET Jean-Luc, KAWAGUCHI Junichiro, MICHEL Patrick, MUINONEN Karri, OBERST Jürgen, YANO Hajime, BINZEL Richard, AGNOLON David, ROMSTEDT Jens
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, 8(27) Tk_13-Tk_21, 2010  Peer-reviewed
    Marco Polo is a mission to return a sample from a near-Earth object of primitive type (class C or D). It is foreseen as a collaborative effort between the Japan Aerospace Exploration Agency (JAXA) and the European Space Agency (ESA). Marco Polo is currently in a Phase-A study (status as of summer 2009). This paper focuses on the scientific requirements provided to the industrial study consortia in Europe as well as the possible mission scenario at the target object in order to achieve the overall mission science objectives. The main scientific reasons for going to a near-Earth object are to...
  • NOGUCHI Takaaki, HITARA Naru, TSUCHIHYAMA Akira, DEMURA Hirohide, NAKAMURA Ryosuke, MIYAMOTO Hideaki, YANO Hajime, NAKAMURA Tomoki
    Planetary people, 19(1) 12-22, 2010  Peer-reviewed
  • Julie Bellerose, Hajime Yano, Daniel J. Scheeres
    Advances in the Astronautical Sciences, 135 747-764, 2010  
    This paper analyses the solar influence at and within binary asteroid systems. Applications are for spacecraft missions in terms of both orbit dynamics and the evaluation of hazards due to dust. Natural phenomena are first discussed, such as sun interactions on the surface leading to dust levitation, which is especially important for small Near Earth asteroids and binary systems due to possible coupling with the binary dynamics. We then state mathematical expressions for analysis and go over basic methods and tools such as averaging to show the solar radiation pressure perturbations. Finally, we show simulations for current targets of interest, for both spacecraft and dust/particles applications.
  • BELLEROSE Julie, YANO Hajime
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN, 8(27) Tk_29-Tk_33, 2010  
    107P/4015 Wilson-Harrington is one of the most intriguing objects, being known for having a cometary history as well as Near Earth Object characteristics, which could answer questions regarding both the origin of life and formation and evolution of small bodies. We first briefly summarize the knowledge state of this small body, leading to its actual classification. We then look at its main dynamical characteristics to prepare for a near future rendezvous and sampling mission, and we make comparisons between the target of the Rosetta mission, 67P/Churyumov-Gerasimenko, for which the spacecraft is carrying a lander, and the targets of Hayabusa and of the Hayabusa Follow-on Mission, Itokawa and 1999 JU3. Finally, we investigate the local stability properties in both proximity of the target and on the surface, and show simulations, to discuss approach strategies.
  • BELLEROSE Julie, YANO Hajime
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN, 8(27) Tk_23-Tk_28, 2010  
    The small body exploration is to be continued by going to take samples of the C-type asteroid (162173) 1999 JU3. Although the mission and spacecraft may integrate lessons learned from the Hayabusa mission, many differences exist. In order to best adapt the proximity phase, we give a comparison between 1999 JU3 and Itokawa, the target of the Hayabusa mission which is coming back in June 2010 with samples, and we show simulations of the dynamics of 1999 JU3. Since landers may take a more important role in the coming small body missions, we also show simulations of deployment and landing, as well as fundamental surface dynamics to assess performance and fate of moving objects on the surface. It is shown that intermediate regions of 1999 JU3 may be regions where loose particles gathered. Finally, we discuss lander science opportunity for local refinement of the target gravity model and internal distribution.
  • IWAI Takeo, NAKAMURA Maki, OHASHI Hideo, SHIBATA Hiromi, MIYACHI Takashi, TAKECHI Seiji, YANO Hajime, SASAKI Sho, FUJII Masayuki, NOGAMI Ken-ichi, GRÜN Eberhard, SRAMA Ralf
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN, 8(27) Pk_7-Pk_10, 2010  
    Temperature dependence of piezoelectric response of a Lead Zirconate Titanate (PZT) sensor for Mercury Dust Monitor (MDM) was investigated with an electrostatic accelerator. The temperature dependence was not so substantial between room temperature and 423 K. This fact leads to good sensor performance and a simplified data analysis during the mission.
  • BELLEROSE Julie, YANO Hajime
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN, 8(27) Pk_39-Pk_44, 2010  Peer-reviewedLast authorCorresponding author
    To date, the Jupiter-Sun Lagrangian points are populated with almost 4500 asteroids, for which their formation and history are still debated. In the current work, we look at rationales for a mission to Jovian Trojan asteroids, and discuss the scientific benefits to investigate binary systems and contact binary systems. We summarized the dynamics for a solar sail mission, which is currently thought to go along the Europa Jupiter System Mission (EJSM), and we show a case study of the contact binary Hektor, and its moon S/2006, which offer the most suitable conditions for spacecraft operations. Trojans asteroids offer many opportunities, and we list some of the targets in time.
  • Sasaki, Sho, Fujimoto, Masaki, Takashima, Takeshi, Yano, Hajime, Kasaba, Yasumasa, Takahashi, Yukihiro, Kimura, Jun, Okada, Tatsuaki, Kawakatsu, Yasuhiro, Tsuda, Yuichi, Kawaguchi, Jun-ichiro, Funase, Ryu, Mori, Osamu, Morimoto, Mutsuko, Ikoma, Masahiro, Naganuma, Takeshi, Yamaji, Atsushi, Hussmann, Hauke, Kurita, Kei, Working Group, Jupiter
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, 8(ists27), 2010  Peer-reviewed
  • K. Nogami, M. Fujii, H. Ohashi, T. Miyachi, S. Sasaki, S. Hasegawa, H. Yano, H. Shibata, T. Iwai, S. Minami, S. Takechi, E. Gruen, R. Srama
    PLANETARY AND SPACE SCIENCE, 58(1-2) 108-115, Jan, 2010  Peer-reviewed
    In order to clarify the dust environment around Mercury, we have proposed that the Mercury dust monitor (MDM) should be onboard the BepiColombo/Mercury magnetosphere orbiter (MMO). The main objective of the project is to obtain new data on the flux and momentum of the interplanetary meteoroid complex near Mercury (0.31-0.47 AU). The MDM uses lightweight and heat-resistant piezoelectric ceramic sensors made of lead zirconate titanate (PZT). Four square plates of PZT, 40 mm x 40 mm x 2 mm each, will be installed on a side panel of the MMO. Upon colliding with a dust particle, the piezoelectricity of PZT generates a transient voltage signal. It is easy to determine the time of the impact event from which the incident direction is roughly estimated using the spin angle of the MMO. To extract kinetic information on incident particles from the output signals of the PZT sensor, calibration experiments have been carried out with hypervelocity dust particles from two Van de Graaff dust accelerators at the Max-Planck-Institut fur Kernphysik and the University of Tokyo. (C) 2008 Elsevier Ltd. All rights reserved.
  • Julie Bellerose, Hajime Yano, Daniel J. Scheeres
    ASTRODYNAMICS 2009, VOL 135, PTS 1-3, 135 747-+, 2010  Peer-reviewed
    This paper analyses the solar influence at and within binary asteroid systems. Applications are for spacecraft missions in terms of both orbit dynamics and the evaluation of hazards due to dust. Natural phenomena are first discussed, such as sun interactions on the surface leading to dust levitation, which is especially important for small Near Earth asteroids and binary systems due to possible coupling with the binary dynamics. We then state mathematical expressions for analysis and go over basic methods and tools such as averaging to show the solar radiation pressure perturbations. Finally, we show simulations for current targets of interest, for both spacecraft and dust/particles applications.
  • Hajime Mita, Akihiko Yamagishi, Hajime Yano, Kyoko Okudaira, Kensei Kobayashi, Shin-ichi Yokobori, Makoto Tabata, Hideyuki Kawai, Hirofumi Hashimoto
    ORIGINS OF LIFE AND EVOLUTION OF BIOSPHERES, 39(3-4) 371-372, Aug, 2009  Peer-reviewed
  • Shin-ichi Yokobori, Akihiko Yamagishi, Yinjie Yang, Kenta Fujisaki, Hirofumi Hashimoto, Hideyuki Kawai, Kensei Kobayashi, Hajime Mita, Kyoko Okudaira, Makoto Tabata, Hajime Yano, Masamichi Yamashita, Yoshitaka Yoshimura
    ORIGINS OF LIFE AND EVOLUTION OF BIOSPHERES, 39(3-4) 377-378, Aug, 2009  Peer-reviewed
  • M. A. Barucci, M. Yoshikawa, P. Michel, J. Kawagushi, H. Yano, J. R. Brucato, I. A. Franchi, E. Dotto, M. Fulchignoni, S. Ulamec
    EXPERIMENTAL ASTRONOMY, 23(3) 785-808, Mar, 2009  Peer-reviewed
    MARCO POLO is a joint European-Japanese sample return mission to a Near-Earth Object. This Euro-Asian mission will go to a primitive Near-Earth Object (NEO), which we anticipate will contain primitive materials without any known meteorite analogue, scientifically characterize it at multiple scales, and bring samples back to Earth for detailed scientific investigation. Small bodies, as primitive leftover building blocks of the Solar System formation process, offer important clues to the chemical mixture from which the planets formed some 4.6 billion years ago. Current exobiological scenarios for the origin of Life invoke an exogenous delivery of organic matter to the early Earth: it has been proposed that primitive bodies could have brought these complex organic molecules capable of triggering the pre-biotic synthesis of biochemical compounds. Moreover, collisions of NEOs with the Earth pose a finite hazard to life. For all these reasons, the exploration of such objects is particularly interesting and urgent. The scientific objectives of MARCO POLO will therefore contribute to a better understanding of the origin and evolution of the Solar System, the Earth, and possibly Life itself. Moreover, MARCO POLO provides important information on the volatile-rich (e.g. water) nature of primitive NEOs, which may be particularly important for future space resource utilization as well as providing critical information for the security of Earth. MARCO POLO is a proposal offering several options, leading to great flexibility in the actual implementation. The baseline mission scenario is based on a launch with a Soyuz-type launcher and consists of a Mother Spacecraft (MSC) carrying a possible Lander named SIFNOS, small hoppers, sampling devices, a re-entry capsule and scientific payloads. The MSC leaves Earth orbit, cruises toward the target with ion engines, rendezvous with the target, conducts a global characterization of the target to select a sampling site, and delivers small hoppers (MINERVA type, JAXA) and SIFNOS. The latter, if added, will perform a soft landing, anchor to the target surface, and make various in situ measurements of surface/subsurface materials near the sampling site. Two surface samples will be collected by the MSC using "touch and go" manoeuvres. Two complementary sample collection devices will be used in this phase: one developed by ESA and another provided by JAXA, mounted on a retractable extension arm. After the completion of the sampling and ascent of the MSC, the arm will be retracted to transfer the sample containers into the MSC. The MSC will then make its journey back to Earth and release the re-entry capsule into the Earth's atmosphere.
  • H. Hashimoto, T. Kaneko, H. Mita, S. Nakashima, H. Naraoka, K. Okudaira, J. Takahashi, Y. Takano, A. Yamagishi, M. Yamashita, H. Yano, S. Yokobori
    Origins of Life and Evolution of Biospheres, 39(1) 4, Feb, 2009  Peer-reviewed
  • S. Yokobori, A. Yamagishi, Y. Yang, K. Fujisaki, H. Hashimoto, H. Kawai, H. Mita, K. Okudaira, M. Tabata, H. Yano, M. Yamashita, Y. Yoshimura
    Origins of Life and Evolution of Biospheres, 39(1) 64-65, Feb, 2009  Peer-reviewed
  • 山岸明彦, 矢野創, 小林憲正, 横堀伸一, 橋本博文, 山下雅道, 田端誠, 河合秀幸
    Viva Origino, 36(1/4) 72-76, 2009  Peer-reviewed
    TANPOPO, dandelion, is the name of a grass whose seeds with floss are spread by the wind. We propose the analyses of interplanetary migration of microbes, organic compounds and meteoroids on ISS-JEM. Ultra low-density aerogel will be used to capture micrometeoroid and debris. Particles captured by aerogel will be used for several analyses after the initial inspection of the gel and tracks. Careful analysis of the tracks in the aerogel will provide the size and velocity dependence of debris flux. The particles will be analyzed for mineralogical, organic and microbiological characteristics. To test the survival of microbes in space environment, microbial cells will be exposed. Organic compounds are also exposed to evaluate the possible denaturation under the conditions. Aerogels are ready for production in Japan. Aerogels and trays are space proven. All the analytical techniques are ready.
  • Saburo MATUNAGA, Tomio YAMANAKA, Ken FUJIWARA, Masaki MAENO, Junichi NISHIDA, Takuro IKEDA, Hajime YANO, Takeru MAKABE, Osamu MORI
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN, 7(ists26) Pk_23-Pk_28, 2009  Peer-reviewed
  • YAMAGISHI Akihiko, YANO Hajime, OKUDAIRA Kyoko, KOBAYASHI Kensei, YOKOBORI Shin-ichi, TABATA Makoto, KAWAI Hideyuki, YAMASHITA Masamichi, HASHIMOTO Hirofumi, NARAOKA Hiroshi, MITA Hajime
    Trans Jpn Soc Aeronaut Space Sci Space Technol Jpn (Web), 7(ists26) TK.49-TK.55 (J-STAGE), 2009  Peer-reviewed
  • A. Yamagishi, H. Yano, K. Okudaira, S. Yokobori, M. Tabata, H. Kawai, M. Yamashita, H. Hashimoto, H. Naraoka, H. Mita
    Proceedings of International Symposium on Space Technology and Science, 27 2008-k-05, 1-5, 2008  Peer-reviewed
  • T. Ebisuzaki, Y. Uehara, H. Ohmori, K. Kawai, Y. Kawasaki, M. Sato, Y. Takizawa, M. E. Bertaina, F. Kajino, T. Sawabe, K. Inoue, A. Sasaki, M. Sakata, Y. Yamamoto, M. Nagano, N. Inoue, T. Shibata, N. Sakaki, Y. Uchihori, Y. Takahashi, H. Shimizu, Y. Arai, Y. Kurihara, H. Fujimoto, S. Yoshida, Y. Mizumoto, S. Inoue, K. Asano, T. Sugiyama, J. Watanabe, H. Ikeda, M. Suzuki, T. Imamura, H. Yano, T. Murakami, D. Yonetoku, Y. Itow, M. Taguchi, M. Nagata, S. Nagataki, S. Abe, T. Tajima, J. H. Adams, S. Mitchell, M. J. Christl, J. Watts, A. English, Y. Takahashi, K. Pitalo, J. Hadaway, J. Geary, P. Readon, H. Crawford, C. Pennypacker, K. Arisaka, D. Cline, P. Gorodetsky, P. Salin, T. Patzark, A. Maurissen, M. Valentin
    NUCLEAR PHYSICS B-PROCEEDINGS SUPPLEMENTS, 175(SUPPL.: COMPLETE) 237-240, Jan, 2008  Peer-reviewed
    The motivations, characteristics and potential performance of the JEM-EUSO project are briefly discussed.
  • Hideaki Miyamoto, Hajime Yano, Daniel J. Scheeres, Shinsuke Abe, Olivier Barnouin-Jha, Andrew F. Cheng, Hirohide Demura, Robert W. Gaskell, Naru Hirata, Masateru Ishiguro, Tatsuhiro Michikami, Akiko M. Nakamura, Ryosuke Nakamura, Jun Saito, Sho Sasaki
    SCIENCE, 316(5827) 1011-1014, May, 2007  Peer-reviewed
    High-resolution images of the surface of asteroid Itokawa from the Hayabusa mission reveal it to be covered with unconsolidated millimeter-sized and larger gravels. Locations and morphologic characteristics of this gravel indicate that Itokawa has experienced considerable vibrations, which have triggered global-scale granular processes in its dry, vacuum, microgravity environment. These processes likely include granular convection, landslide-like granular migrations, and particle sorting, resulting in the segregation of the fine gravels into areas of potential lows. Granular processes become major resurfacing processes because of Itokawa's small size, implying that they can occur on other small asteroids should those have regolith.
  • A. F. Cheng, O. Barnouin-Jha, N. Hirata, H. Miyamoto, R. Nakamura, H. Yano
    GEOPHYSICAL RESEARCH LETTERS, 34(9), May, 2007  Peer-reviewedLast author
    The outcomes of asteroid collisional evolution are presently unclear: are most asteroids larger than 1 km size gravitational aggregates reaccreted from fragments of a parent body that was collisionally disrupted, while much smaller asteroids are collisional shards that were never completely disrupted? The 16 km mean diameter S-type asteroid 433 Eros, visited by the NEAR mission, has surface geology consistent with being a fractured shard. The Hayabusa spacecraft visited an S-asteroid smaller than 1 km, namely 25143 Itokawa. Here we report the first comparative analyses of Itokawa and Eros geology. Itokawa lacks a global lineament fabric, and its blocks, craters, and regolith are inconsistent with formation and evolution as a fractured shard, unlike Eros. Itokawa is not a scaled-down Eros, but formed by a distinct process of catastrophic disruption and reaccumulation.
  • Takaaki Noguchi, Tomoki Nakamura, Kyoko Okudaira, Hajime Yano, Seiji Sugita, Mark J. Burchell
    METEORITICS & PLANETARY SCIENCE, 42(3) 357-372, Mar, 2007  Peer-reviewed
    Outside the Earth's atmosphere, silica aerogel is one of the best materials to capture fine-grained extraterrestrial particles in impacts at hypervelocities. Because silica aerogel is a superior insulator, captured grains are inevitably influenced by frictional heat. Therefore, we performed laboratory simulations of hypervelocity capture by using light-gas guns to impact into aerogels fine-grained powders of serpentine, cronstedtite, and Murchison CM2 meteorite. The samples were shot at > 6 km s(-1) similar to the flyby speed at comet P/Wild-2 in the Stardust mission. We investigated mineralogical changes of each captured particle by using synchrotron radiation X-ray diffraction (SR-XRD), transmission electron microscope (TEM), and field emission scanning electron microscope (FE-SEM). SR-XRD of each grain showed that the majority of the bulk grains keep their original mineralogy. In particular, SR-XRD, and TEM investigations clearly exemplified the presence of tochilinite whose decomposition temperature is about 300 degrees C in the interior of the captured Murchison powder. However, TEM study of these grains also revealed that all the samples experienced melting and vesiculation on the surface. The cronstedtite and the Murchison meteorite powder show remarkable fracturing, disaggregation, melting, and vesiculation. Steep thermal gradients, about 2500 degrees C/mu m were estimated near the surface of the grains (< 2 mu m thick) by TEM observation. Our data suggests that the interior of > 4 mu m across residual grains containing abundant materials that inhibit temperature rise would have not experienced > 300 degrees C at the center.
  • Shinsuke Abe, Noboru Ebizuka, Hajime Yano, Jun-Ichi Watanabe, Jiri Borovicka
    ADVANCES IN SPACE RESEARCH, 39(4) 538-543, 2007  Peer-reviewed
    An ultraviolet-visible spectrum between 300 and 450 nm of a cometary meteoroid originated from 55P/Tempel-Tuttle was investigated. The spectroscopy was carried out an intensified high definition TV camera with a slit-less reflection grating during the 2001 Leonid meteor shower over Japan. A best fit calculation mixed with atoms and molecules confirmed the first discovery of (N2+B2)Sigma(+)(u) -> X-2 Sigma(+)(g) bands in the UV meteor spectrum. N-2(+) temperature was estimated to 10,000 K with a low number density of 1.55 x 10(5) cm(-3). We also discuss the possibility that enhanced emissions in a meteor and a train around 310 nm are caused by the band head of OH A(2)Sigma(+) -> X-2 Pi. Since cometary dust may have contributed organics and water to the Earth from its early period until now, OH A-X (0, 0) must be investigated. (c) 2007 Published by Elsevier Ltd on behalf of COSPAR.
  • 山岸明彦, 矢野創, 奥平恭子, 小林憲正, 横堀伸一, 田端誠, 河合秀幸
    Biological Sciences in Space, 21(3) 67-75, 2007  Peer-reviewed
    TANPOPO, dandelion, is the name of a grass whose seeds with floss are spread by the wind. We propose the analyses of interplanetary migration of microbes, organic compounds and meteoroids on ISS-JEM. Ultra low density aerogel will be used to capture micrometeoroid and debris. Particles captured by aerogel will be used for several analyses after the initial inspection of the gel and tracks. Careful analysis of the tracks in the aerogel will provide the size and velocity dependence of debris flux. The particles will be analyzed for mineralogical, organic and microbiological characteristics. To test the survival of microbes in space environment, microbial cells will be exposed. Organic compounds are also exposed to evaluate the possible denaturation under the conditions. Aerogels are ready for production in Japan. Aerogels and trays are space proven. All the analytical techniques are ready.
  • OKUDAIRA Kyoko, NOGUCHI Takaaki, YANO Hajime
    Planetary people, 16(4) 316-321, 2007  Peer-reviewedLast author
  • Michael E. Zolensky, Thomas J. Zega, Hajime Yano, Sue Wirick, Andrew J. Westphal, Mike K. Weisberg, Iris Weber, Jack L. Warren, Michael A. Velbel, Akira Tsuchiyama, Peter Tsou, Alice Toppani, Naotaka Tomioka, Kazushige Tomeoka, Nick Teslich, Mitra Taheri, Jean Susini, Rhonda Stroud, Thomas Stephan, Frank J. Stadermann, Christopher J. Snead, Steven B. Simon, Alexandre Simionovici, Thomas H. See, Francois Robert, Frans J. M. Rietmeijer, William Rao, Murielle C. Perronnet, Dimitri A. Papanastassiou, Kyoko Okudaira, Kazumasa Ohsumi, Ichiro Ohnishi, Keiko Nakamura-Messenger, Tomoki Nakamura, Smail Mostefaoui, Takashi Mikouchi, Anders Meibom, Graciela Matrajt, Matthew A. Marcus, Hugues Leroux, Laurence Lemelle, Loan Le, Antonio Lanzirotti, Falko Langenhorst, Alexander N. Krot, Lindsay P. Keller, Anton T. Kearsley, David Joswiak, Damien Jacob, Hope Ishii, Ralph Harvey, Kenji Hagiya, Lawrence Grossman, Jeffrey N. Grossman, Giles A. Graham, Matthieu Gounelle, Philippe Gillet, Matthew J. Genge, George Flynn, Tristan Ferroir, Stewart Fallon, Denton S. Ebel, Zu Rong Dai, Patrick Cordier, Benton Clark, Miaofang Chi, Anna L. Butterworth, Donald E. Brownlee, John C. Bridges, Sean Brennan, Adrian Brearley, John P. Bradley, Pierre Bleuet, Phil A. Bland, Ron Bastien
    SCIENCE, 314(5806) 1735-1739, Dec, 2006  Peer-reviewed
    The bulk of the comet 81P/Wild 2 ( hereafter Wild 2) samples returned to Earth by the Stardust spacecraft appear to be weakly constructed mixtures of nanometer-scale grains, with occasional much larger ( over 1 micrometer) ferromagnesian silicates, Fe-Ni sulfides, Fe-Ni metal, and accessory phases. The very wide range of olivine and low-Ca pyroxene compositions in comet Wild 2 requires a wide range of formation conditions, probably reflecting very different formation locations in the protoplanetary disk. The restricted compositional ranges of Fe-Ni sulfides, the wide range for silicates, and the absence of hydrous phases indicate that comet Wild 2 experienced little or no aqueous alteration. Less abundant Wild 2 materials include a refractory particle, whose presence appears to require radial transport in the early protoplanetary disk.
  • Don Brownlee, Peter Tsou, Jerome Aleon, Conel M. O'D. Alexander, Tohru Araki, Sasa Bajt, Giuseppe A. Baratta, Ron Bastien, Phil Bland, Pierre Bleuet, Janet Borg, John P. Bradley, Adrian Brearley, F. Brenker, Sean Brennan, John C. Bridges, Nigel D. Browning, John R. Brucato, E. Bullock, Mark J. Burchell, Henner Busemann, Anna Butterworth, Marc Chaussidon, Allan Cheuvront, Miaofang Chi, Mark J. Cintala, B. C. Clark, Simon J. Clemett, George Cody, Luigi Colangeli, George Cooper, Patrick Cordier, C. Daghlian, Zurong Dai, Louis D'Hendecourt, Zahia Djouadi, Gerardo Dominguez, Tom Duxbury, Jason P. Dworkin, Denton S. Ebel, Thanasis E. Economou, Sirine Fakra, Sam A. J. Fairey, Stewart Fallon, Gianluca Ferrini, T. Ferroir, Holger Fleckenstein, Christine Floss, George Flynn, Ian A. Franchi, Marc Fries, Z. Gainsforth, J. -P. Gallien, Matt Genge, Mary K. Gilles, Philipe Gillet, Jamie Gilmour, Daniel P. Glavin, Matthieu Gounelle, Monica M. Grady, Giles A. Graham, P. G. Grant, Simon F. Green, Faustine Grossemy, Lawrence Grossman, Jeffrey N. Grossman, Yunbin Guan, Kenji Hagiya, Ralph Harvey, Philipp Heck, Gregory F. Herzog, Peter Hoppe, Friedrich Hoerz, Joachim Huth, Ian D. Hutcheon, Konstantin Ignatyev, Hope Ishii, Motoo Ito, Damien Jacob, Chris Jacobsen, Stein Jacobsen, Steven Jones, David Joswiak, Amy Jurewicz, Anton T. Kearsley, Lindsay P. Keller, H. Khodja, A. L. David Kilcoyne, Jochen Kissel, Alexander Krot, Falko Langenhorst, Antonio Lanzirotti, Loan Le, Laurie A. Leshin, J. Leitner, L. Lemelle, Hugues Leroux, Ming-Chang Liu, K. Luening, Ian Lyon, Glen MacPherson, Matthew A. Marcus, Kuljeet Marhas, Bernard Marty, Graciela Matrajt, Kevin McKeegan, Anders Meibom, Vito Mennella, Keiko Messenger, Scott Messenger, Takashi Mikouchi, Smail Mostefaoui, Tomoki Nakamura, T. Nakano, M. Newville, Larry R. Nittler, Ichiro Ohnishi, Kazumasa Ohsumi, Kyoko Okudaira, Dimitri A. Papanastassiou, Russ Palma, Maria E. Palumbo, Robert O. Pepin, David Perkins, Murielle Perronnet, P. Pianetta, William Rao, Frans J. M. Rietmeijer, Francois Robert, D. Rost, Alessandra Rotundi, Robert Ryan, Scott A. Sandford, Craig S. Schwandt, Thomas H. See, Dennis Schlutter, J. Sheffield-Parker, Alexandre Simionovici, Steven Simon, I. Sitnitsky, Christopher J. Snead, Maegan K. Spencer, Frank J. Stadermann, Andrew Steele, Thomas Stephan, Rhonda Stroud, Jean Susini, S. R. Sutton, Y. Suzuki, Mitra Taheri, Susan Taylor, Nick Teslich, Kazu Tomeoka, Naotaka Tomioka, Alice Toppani, Josep M. Trigo-Rodriguez, David Troadec, Akira Tsuchiyama, Anthony J. Tuzzolino, Tolek Tyliszczak, K. Uesugi, Michael Velbel, Joe Vellenga, E. Vicenzi, L. Vincze, Jack Warren, Iris Weber, Mike Weisberg, Andrew J. Westphal, Sue Wirick, Diane Wooden, Brigitte Wopenka, Penelope Wozniakiewicz, Ian Wright, Hikaru Yabuta, Hajime Yano, Edward D. Young, Richard N. Zare, Thomas Zega, Karen Ziegler, Laurent Zimmerman, Ernst Zinner, Michael Zolensky
    SCIENCE, 314(5806) 1711-1716, Dec, 2006  Peer-reviewed
    The Stardust spacecraft collected thousands of particles from comet 81P/Wild 2 and returned them to Earth for laboratory study. The preliminary examination of these samples shows that the nonvolatile portion of the comet is an unequilibrated assortment of materials that have both presolar and solar system origin. The comet contains an abundance of silicate grains that are much larger than predictions of interstellar grain models, and many of these are high-temperature minerals that appear to have formed in the inner regions of the solar nebula. Their presence in a comet proves that the formation of the solar system included mixing on the grandest scales.
  • M. Yoshikawa, H. Ikeda, H. Yano, J. Saito, T. Kubota, T. Hashimoto, A. Fujiwara, J. Kawaguchi, T. Kominato, M. Matsuoka, K. Shirakawa, T. Ohnishi, S. Abe, T. Mukai, R. Gaskell, D. Scheeres
    Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006, 3 1515-1521, Dec 1, 2006  Peer-reviewed
    Hayabusa was moving near Asteroid Itokawa for about three months in 2005. Using tracking and navigation data such as range, Boppler, distance from the asteroid, and optical images taken by navigation cameras, we estimated the mass of Itokawa for several orbital phases. The results are consistent in their error ranges. The estimated mass of Itokawa is 3.51 ± 0.105 (1010 kg), from which the density of Itokawa is derived as 1.9 ± 0.13 (g/cm3). This is one of the important characteristics to understand the nature of Itokawa. We are also trying to investigate the accuracy of the ephemeris of this asteroid. Copyright © 2006 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
  • Takashi Kubota, Masatsugu Otsuki, Tatsuaki Hashimoto, Nobutaka Bando, Hajime Yano, Masashi Uo, Ken'ichi Shirakawa, Jun'ichiro Kawaguchi
    Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006, 2 1403-1414, Dec 1, 2006  Peer-reviewed
    Hayabusa spacecraft performed the final descents and touchdowns twice in November 2005. In final descent phase, terrain alignment maneuvers were accomplished to control both altitude and attitude with respect to the surface by using four beams Laser Range Finder onboard. Then Hayabusa spacecraft made dynamic touchdowns the surface of the asteroid by the sampler system to collect samples automatically. This paper presents the terrain alignment maneuver and touchdown scheme. This paper also describes the novel sample horn system and touchdown dynamics. Touchdown tests on the ground are presented. Then the flight results on touchdown dynamics are shown and discussed. Copyright © 2006 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
  • 矢野 創
    関西経協, 60(8) 20-25, Aug, 2006  InvitedLead author
  • Michael Zolensky, Phil Bland, John Bradley, Adrian Brearley, Sean Brennan, John Bridges, Donald Brownlee, Arma Buttervorth, Zurong Dai, Denton Ebel, Matt Genge, Matthieu Gounelle, Giles Graham, Jeff Grossman, Lawrence Grossman, Ralph Harvey, Hope Ishii, Anton Kearsley, Lindsay Keller, Alexander Krot, Falko Langenhorst, Antonio Lanzirotti, Hugues Leroux, Graciela Matrajt, Keiko Messenger, Takashi Mikouchi, Tomoki Nakamura, Kazumasa Ohsumi, Kyoko Okudaira, Murielle Perronnet, Frans Rietmeijer, Steven Simon, Thomas Stephan, Rhonda Stroud, Mitra Taheri, Kazu Tomeoka, Alice Toppani, Peter Tsou, Akira Tsuchiyama, Michael Velbel, Iris Weber, Mike Weisberg, Andrew Westphal, Hajime Yano, Thomas Zega
    METEORITICS & PLANETARY SCIENCE, 41(8) A167-A167, Aug, 2006  Peer-reviewed

Misc.

 489

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