研究者業績

岡田 達明

オカダ タツアキ  (Tatsuaki Okada)

基本情報

所属
国立研究開発法人宇宙航空研究開発機構 宇宙科学研究所 太陽系科学研究系 准教授
東京大学大学院 理学系研究科化学専攻 准教授
学位
博士(理学)(1996年3月 東京大学)

研究者番号
30321566
J-GLOBAL ID
201501026547105146
researchmap会員ID
B000243484

外部リンク

専門は惑星科学、惑星物理学、惑星物質・物性科学、惑星探査科学。特に熱赤外カメラを用いた史上初の小惑星探査により、惑星探査に「熱撮像」の手法を世界で初めて導入に成功し、さらに「太陽系物性科学」の分野を創設。観測機器の開発による惑星探査でのその場観測とサンプルリターンによる帰還試料分析を主な研究手法とする。

主要な開発機器は、蛍光X線分光計、熱赤外カメラ、多波長熱赤外カメラである。また開発中のものはマルチターン飛行時間型質量分析計等である。地上分析においてはハイパースペクトル顕微鏡による帰還試料の分析の他、将来の資料熱物性分析のための多色熱赤外顕微鏡の開発を推進中である。

◆国内外の惑星探査計画(観測機器担当)

・月探査「Lunar-A」 光学カメラLIC(Co-I)1993-2005 

・火星探査「のぞみ」 HFレーダ高度計PWS/ALT(Co-I)1994-2003、可視カメラMIC(Co-I)1995-2003

・小惑星探査「はやぶさ」 蛍光エックス線分光計XRS担当(PI)1995-2010

・月周回探査「かぐや(SELENE)」 蛍光X線分光計XRS担当(PI)1998-2009

・小惑星探査「はやぶさ2」 中間赤外カメラTIR担当(PI)2010-present.、

・小惑星探査「はやぶさ2」 小型ランダーMASCOT担当(JAXAリエゾン)2010-2019

・小惑星探査「はやぶさ2」 デジタルエレキDE担当(PI)2010-present

・小惑星探査「はやぶさ2」 ハイパースペクトル顕微鏡MicrOmega担当(Co-PI)2019-present

・二重小惑星探査計画Hera 熱赤外カメラTIRI担当(PI)2020-present

・二重小惑星探査計画Hera Hera Investigation Team メンバ(招聘)2020-present

◆帰還サンプルの分析(地上分析)

・JAXAキュレーションセンター(地球外物質研究グループ所属)2009-present

・ハイパースペクトル顕微鏡MicrOmega-CF(Co-PI)

・熱赤外顕微鏡(PI)

◆海外ミッション参画

・SMART-1 D-CIXS(Co-I)2000-2005

・Chandrayaan-1 C1XS(Co-I)2006-2009

・BepiColombo MIXS(Co-I)2003-present、SIXS (Co-I)2003-present

・Hera (-JP) Proejct Manager & TIRI(PI)2020-present、Investigation Team 2020-present

◆WG参画

・ESA MarcoPolo(=Hayabusa-MkII)においてX線分光、熱積外カメラ、着陸機

・月着陸機SELENE-B、SELENE-II

・月着陸SLIM(科学システム検討担当)

・火星探査MELOS(科学システム検討担当(固体惑星)、着陸探査)

・OKEANOS (科学システム検討担当、質量分析計HRMSの開発)

・月縦孔探査Uzume(科学システム検討担当、熱赤外カメラの開発)

 


委員歴

 3

受賞

 24

論文

 227
  • T. Morota, S. Sugita, Y. Cho, M. Kanamaru, E. Tatsumi, N. Sakatani, R. Honda, N. Hirata, H. Kikuchi, M. Yamada, Y. Yokota, S. Kameda, M. Matsuoka, H. Sawada, C. Honda, T. Kouyama, K. Ogawa, H. Suzuki, K. Yoshioka, M. Hayakawa, N. Hirata, M. Hirabayashi, H. Miyamoto, T. Michikami, T. Hiroi, R. Hemmi, O. S. Barnouin, C. M. Ernst, K. Kitazato, T. Nakamura, L. Riu, H. Senshu, H. Kobayashi, S. Sasaki, G. Komatsu, N. Tanabe, Y. Fujii, T. Irie, M. Suemitsu, N. Takaki, C. Sugimoto, K. Yumoto, M. Ishida, H. Kato, K. Moroi, D. Domingue, P. Michel, C. Pilorget, T. Iwata, M. Abe, M. Ohtake, Y. Nakauchi, K. Tsumura, H. Yabuta, Y. Ishihara, R. Noguchi, K. Matsumoto, A. Miura, N. Namiki, S. Tachibana, M. Arakawa, H. Ikeda, K. Wada, T. Mizuno, C. Hirose, S. Hosoda, O. Mori, T. Shimada, S. Soldini, R. Tsukizaki, H. Yano, M. Ozaki, H. Takeuchi, Y. Yamamoto, T. Okada, Y. Shimaki, K. Shirai, Y. Iijima, H. Noda, S. Kikuchi, T. Yamaguchi, N. Ogawa, G. Ono, Y. Mimasu, K. Yoshikawa, T. Takahashi, Y. Takei, A. Fujii, S. Nakazawa, F. Terui, S. Tanaka, M. Yoshikawa, T. Saiki, S. Watanabe, Y. Tsuda
    Science 368(6491) 654-659 2020年5月8日  査読有り
    © 2020 American Association for the Advancement of Science. All rights reserved. The near-Earth asteroid (162173) Ryugu is thought to be a primitive carbonaceous object that contains hydrated minerals and organic molecules. We report sample collection from Ryugu’s surface by the Hayabusa2 spacecraft on 21 February 2019. Touchdown images and global observations of surface colors are used to investigate the stratigraphy of the surface around the sample location and across Ryugu. Latitudinal color variations suggest the reddening of exposed surface material by solar heating and/or space weathering. Immediately after touchdown, Hayabusa2’s thrusters disturbed dark, fine grains that originate from the redder materials. The stratigraphic relationship between identified craters and the redder material indicates that surface reddening occurred over a short period of time. We suggest that Ryugu previously experienced an orbital excursion near the Sun.
  • M. Arakawa, T. Saiki, K. Wada, K. Ogawa, T. Kadono, K. Shirai, H. Sawada, K. Ishibashi, R. Honda, N. Sakatani, Y. Iijima, C. Okamoto, H. Yano, Y. Takagi, M. Hayakawa, P. Michel, M. Jutzi, Y. Shimaki, S. Kimura, Y. Mimasu, T. Toda, H. Imamura, S. Nakazawa, H. Hayakawa, S. Sugita, T. Morota, S. Kameda, E. Tatsumi, Y. Cho, K. Yoshioka, Y. Yokota, M. Matsuoka, M. Yamada, T. Kouyama, C. Honda, Y. Tsuda, S. Watanabe, M. Yoshikawa, S. Tanaka, F. Terui, S. Kikuchi, T. Yamaguchi, N. Ogawa, G. Ono, K. Yoshikawa, T. Takahashi, Y. Takei, A. Fujii, H. Takeuchi, Y. Yamamoto, T. Okada, C. Hirose, S. Hosoda, O. Mori, T. Shimada, S. Soldini, R. Tsukizaki, T. Iwata, M. Ozaki, M. Abe, N. Namiki, K. Kitazato, S. Tachibana, H. Ikeda, N. Hirata, N. Hirata, R. Noguchi, A. Miura
    Science 368(6486) 2020年4月  査読有り
    © 2020 American Association for the Advancement of Science. All rights reserved. The Hayabusa2 spacecraft investigated the small asteroid Ryugu, which has a rubble-pile structure. We describe an impact experiment on Ryugu using Hayabusa2's Small Carry-on Impactor. The impact produced an artificial crater with a diameter >10 meters, which has a semicircular shape, an elevated rim, and a central pit. Images of the impact and resulting ejecta were recorded by the Deployable CAMera 3 for >8 minutes, showing the growth of an ejecta curtain (the outer edge of the ejecta) and deposition of ejecta onto the surface. The ejecta curtain was asymmetric and heterogeneous and it never fully detached from the surface. The crater formed in the gravity-dominated regime; in other words, crater growth was limited by gravity not surface strength. We discuss implications for Ryugu's surface age.
  • Tatsuaki Okada, Tetsuya Fukuhara, Satoshi Tanaka, Makoto Taguchi, Takehiko Arai, Hiroki Senshu, Naoya Sakatani, Yuri Shimaki, Hirohide Demura, Yoshiko Ogawa, Kentaro Suko, Tomohiko Sekiguchi, Toru Kouyama, Jun Takita, Tsuneo Matsunaga, Takeshi Imamura, Takehiko Wada, Sunao Hasegawa, Jörn Helbert, Thomas G. Müller, Axel Hagermann, Jens Biele, Matthias Grott, Maximilian Hamm, Marco Delbo, Naru Hirata, Naoyuki Hirata, Yukio Yamamoto, Seiji Sugita, Noriyuki Namiki, Kohei Kitazato, Masahiko Arakawa, Shogo Tachibana, Hitoshi Ikeda, Masateru Ishiguro, Koji Wada, Chikatoshi Honda, Rie Honda, Yoshiaki Ishihara, Koji Matsumoto, Moe Matsuoka, Tatsuhiro Michikami, Akira Miura, Tomokatsu Morota, Hirotomo Noda, Rina Noguchi, Kazunori Ogawa, Kei Shirai, Eri Tatsumi, Hikaru Yabuta, Yasuhiro Yokota, Manabu Yamada, Masanao Abe, Masahiko Hayakawa, Takahiro Iwata, Masanobu Ozaki, Hajime Yano, Satoshi Hosoda, Osamu Mori, Hirotaka Sawada, Takanobu Shimada, Hiroshi Takeuchi, Ryudo Tsukizaki, Atsushi Fujii, Chikako Hirose, Shota Kikuchi, Yuya Mimasu, Naoko Ogawa, Go Ono, Tadateru Takahashi, Yuto Takei, Tomohiro Yamaguchi, Kent Yoshikawa, Fuyuto Terui, Takanao Saiki, Satoru Nakazawa, Makoto Yoshikawa, Seiichiro Watanabe, Yuichi Tsuda
    Nature 579(7800) 518-522 2020年3月26日  査読有り筆頭著者責任著者
    © 2020, The Author(s), under exclusive licence to Springer Nature Limited. Carbonaceous (C-type) asteroids1 are relics of the early Solar System that have preserved primitive materials since their formation approximately 4.6 billion years ago. They are probably analogues of carbonaceous chondrites2,3 and are essential for understanding planetary formation processes. However, their physical properties remain poorly known because carbonaceous chondrite meteoroids tend not to survive entry to Earth’s atmosphere. Here we report on global one-rotation thermographic images of the C-type asteroid 162173 Ryugu, taken by the thermal infrared imager (TIR)4 onboard the spacecraft Hayabusa25, indicating that the asteroid’s boulders and their surroundings have similar temperatures, with a derived thermal inertia of about 300 J m−2 s−0.5 K−1 (300 tiu). Contrary to predictions that the surface consists of regolith and dense boulders, this low thermal inertia suggests that the boulders are more porous than typical carbonaceous chondrites6 and that their surroundings are covered with porous fragments more than 10 centimetres in diameter. Close-up thermal images confirm the presence of such porous fragments and the flat diurnal temperature profiles suggest a strong surface roughness effect7,8. We also observed in the close-up thermal images boulders that are colder during the day, with thermal inertia exceeding 600 tiu, corresponding to dense boulders similar to typical carbonaceous chondrites6. These results constrain the formation history of Ryugu: the asteroid must be a rubble pile formed from impact fragments of a parent body with microporosity9 of approximately 30 to 50 per cent that experienced a low degree of consolidation. The dense boulders might have originated from the consolidated innermost region or they may have an exogenic origin. This high-porosity asteroid may link cosmic fluffy dust to dense celestial bodies10.
  • Koji Matsumoto, Hirotomo Noda, Yoshiaki Ishihara, Hiroki Senshu, Keiko Yamamoto, Naru Hirata, Naoyuki Hirata, Noriyuki Namiki, Toshimichi Otsubo, Arika Higuchi, Sei ichiro Watanabe, Hitoshi Ikeda, Takahide Mizuno, Ryuhei Yamada, Hiroshi Araki, Shinsuke Abe, Fumi Yoshida, Sho Sasaki, Shoko Oshigami, Seiitsu Tsuruta, Kazuyoshi Asari, Makoto Shizugami, Yukio Yamamoto, Naoko Ogawa, Shota Kikuchi, Takanao Saiki, Yuichi Tsuda, Makoto Yoshikawa, Satoshi Tanaka, Fuyuto Terui, Satoru Nakazawa, Tomohiro Yamaguchi, Yuto Takei, Hiroshi Takeuchi, Tatsuaki Okada, Manabu Yamada, Yuri Shimaki, Kei Shirai, Kazunori Ogawa, Yu ichi Iijima
    Icarus 338 2020年3月1日  査読有り
    © 2019 Elsevier Inc. Precise information of spacecraft position with respect to target body is of importance in terms of scientific interpretation of remote sensing data. In case of Hayabusa2, a sample return mission from asteroid Ryugu, such information is also necessary for landing site selection activity. We propose a quick method to improve the spacecraft trajectory when laser altimeter range measurements and a shape model are provided together with crude initial trajectory, spacecraft attitude information, and asteroid spin information. We compared topographic features contained in the altimeter data with those expressed by the reference shape model, and estimated long-period trajectory correction so that discrepancy between the two topographic profiles was minimized. The improved spacecraft positions are consistent with those determined by image-based stereophotoclinometry method within a few tens of meters. With such improved trajectory, the altimeter ranges can be converted to Ryugu's topographic profiles that are appropriate for geophysical interpretation. We present a geophysical application that invokes possibility of impact-induced formation of the Ryugu's western bulge.
  • Tatsuaki Okada
    Applied Sciences (Switzerland) 10(6) 2158-2158 2020年3月1日  査読有り招待有り筆頭著者責任著者
    © 2020 by authors. The Near-Earth Asteroid 162173 Ryugu is a C-type asteroid which preserves information about the ancient Solar System and is considered enriched in volatiles such as water and organics associated with the building blocks of life, and it is a potentially hazardous object that might impact Earth. Hayabusa2 is the asteroid explorer organized by the Japan Aerospace Exploration Agency to rendezvous with the asteroid and collect surface materials to return them to Earth. Thermography has been carried out from Hayabusa2 during the asteroid proximity phase, to unveil the thermophysical properties of the primitive Solar System small body, which offered a new insight for understanding the origin and evolution of the Solar System, and demonstrated the technology for future applications in space missions. Global, local, and close-up thermal images taken from various distances from the asteroid strongly contributed to the mission success, including suitable landing site selection, safe assessment during descents into the thermal environments and hazardous boulder abundance, and the detection of deployable devices against the sunlit asteroid surface. Potential applications of thermography in future planetary missions are introduced.
  • Naoyuki Hirata, Tomokatsu Morota, Yuichiro Cho, Masanori Kanamaru, Sei ichiro Watanabe, Seiji Sugita, Naru Hirata, Yukio Yamamoto, Rina Noguchi, Yuri Shimaki, Eri Tatsumi, Kazuo Yoshioka, Hirotaka Sawada, Yasuhiro Yokota, Naoya Sakatani, Masahiko Hayakawa, Moe Matsuoka, Rie Honda, Shingo Kameda, Manabu Yamada, Toru Kouyama, Hidehiko Suzuki, Chikatoshi Honda, Kazunori Ogawa, Yuichi Tsuda, Makoto Yoshikawa, Takanao Saiki, Satoshi Tanaka, Fuyuto Terui, Satoru Nakazawa, Shota Kikuchi, Tomohiro Yamaguchi, Naoko Ogawa, Go Ono, Yuya Mimasu, Kent Yoshikawa, Tadateru Takahashi, Yuto Takei, Atsushi Fujii, Hiroshi Takeuchi, Tatsuaki Okada, Kei Shirai, Yu ichi Iijima
    Icarus 338(1) 113-527 2020年3月1日  査読有り
    © 2019 Elsevier Inc. Asteroid 162173 Ryugu has numerous craters. The initial measurement of impact craters on Ryugu, by Sugita et al. (2019), is based on Hayabusa2 ONC images obtained during the first month after the arrival of Hayabusa2 in June 2018. Utilizing new images taken until February 2019, we constructed a global impact crater catalogue of Ryugu, which includes all craters larger than 20 m in diameter on the surface of Ryugu. As a result, we identified 77 craters on the surface of Ryugu. Ryugu shows variation in crater density which cannot be explained by the randomness of cratering; there are more craters at lower latitudes and fewer at higher latitudes, and fewer craters in the western bulge (160°E – 290°E) than in the region around the meridian (300°E – 30°E). This variation implies a complicated geologic history for Ryugu. It seems that the variation in crater density indicates that the equatorial ridge located in the western hemisphere is relatively young, while that located in the eastern hemisphere is a fossil structure formed during the short rotational period in the distant past.
  • 古谷克司, 福永翔乃, 岡田達明, 佐伯和人, 大上寛之
    精密工学会誌(Web) 86(8) 2020年  査読有り
  • 岡田達明, 岡田達明, 福原哲哉, 田中智, 坂谷尚哉, 嶌生有理, 荒井武彦, 千秋博紀, 出村裕英, 神山徹, 関口朋彦
    日本惑星科学会誌 遊・星・人 29(2) 80-87 2020年  査読有り筆頭著者責任著者
    <p>小惑星探査機「はやぶさ2」に搭載された中間赤外カメラTIRによって,C型小惑星Ryuguに対して全球の高解像度サーモグラフィ(熱撮像)が史上初めて実施された.表層温度と日変化から導出される熱慣性から,Ryuguの表面を覆う岩塊や岩片の大部分が,典型的な炭素質コンドライト隕石と比較して非常に高空隙な物質で構成されていることが分かった.この高空隙な性質は,表面重力の小さい始原的小惑星に共通であると考えられる.太陽系初期の微惑星も同様に高空隙で低強度の物質で構成されていたと考えられ,惑星形成時の力学進化過程の考察に影響を与える可能性を提起する重要な発見である.</p>
  • Hiroki Hihara, Junpei Sano, Jun Takada, Tetsuya Masuda, Tatsuaki Okada, Naoko Ogawa, Hisashi Ootake, Yuichi Tsuda
    Proceedings of SPIE - The International Society for Optical Engineering 11502 2020年  査読有り招待有り
    © 2020 SPIE HAYABUSA2 asteroid probe has completed its mission successfully in the vicinity of asteroid Ryugu on November 13, 2019. It is on its way to the Earth now. Digital Electronics and Optical Navigation Camera (DE-ONC) was developed for scientific observation and real-time image recognition for optical navigation. The development process and its high-speed wire rate signal processing architecture of onboard electronics are explained in this lecture. Highly efficient lossless and lossy image compression algorithm were developed to send observed images through within the limited capacity of communication channels between the asteroid Ryugu and the Earth for scientific purposes. Onboard sensitivity and distortion correction functions for image sensors were also developed to improve compression ratio of images. High level synthesis technology was employed to implement the image recognition functions for optical navigation functions into limited numbers of space grade field programmable gate arrays (FPGAs) and to achieve wire rate signal processing speed. It must also satisfy high reliability and safety requirements of HAYABUSA2 missions. Functional distribution mode, standby redundancy mode and hot redundancy mode were realized with the same device configuration. Model based design was performed to satisfy these requirements. The onboard image processing unit of DE-ONC adopts a unified language processing system and a distributed memory model with reference to a parallel inference machine developed for the Fifth Generation Computer Systems aiming at artificial intelligence technology development. Its image processing module integrates a radiation hardened micro-controller unit (MCU) and FPGAs with the unified language processing system and the distributed object model.
  • Katsushi Furutani, Haruki Okamura, Tatsuaki Okada, Kazuto Saiki, Hiroyuki Ohue
    Proceedings - 35th ASPE Annual Meeting 210-213 2020年  査読有り
  • Jens Biele, Ekkehard Kührt, Hiroki Senshu, Naoya Sakatani, Kazunori Ogawa, Maximilian Hamm, Matthias Grott, Tatsuaki Okada, Takehiko Arai
    Progress in Earth and Planetary Science 6(1) 48-48 2019年12月1日  査読有り
    © 2019, The Author(s). We have investigated the influence of thin thermally opaque dust layers on the thermal emission of rocks and regolith and determined the thermal response of these dust-covered surfaces to diurnal insolation cycles. Results are computed for Hayabusa2’s target asteroid (162173) Ryugu, which was observed by thermal infrared instruments on the orbiter and in situ. We show that even a very thin (10.100 μm) fine-grained porous dust layer with thermal inertia of 25 J m−2 K−1 s−1/2 can have a significant influence on surface temperatures and alter the apparent thermal inertia of the underlying material derived under the simplified assumption of a homogenous half space by more than 20%. The masking of the underlying material is complete at about 1 diurnal skin depth, corresponding to ~ 10 mm on Ryugu. Between 0.1 and 1 diurnal skin depths, we find a thermal lag smaller than what would be predicted for a surface consisting of dust only. If a dust cover were present on Ryugu, this should be clearly visible in the data returned by the orbiter’s thermal infrared imager (TIR) and the MASCOT lander’s radiometer (MARA), which observed a single boulder at the landing site. However, this appears not to be the case, and dust seems to play a minor role in the thermal emission from the asteroid. [Figure not available: see fulltext.].
  • M. Grott, J. Knollenberg, M. Hamm, K. Ogawa, R. Jaumann, K. A. Otto, M. Delbo, P. Michel, J. Biele, W. Neumann, M. Knapmeyer, E. Kührt, H. Senshu, T. Okada, J. Helbert, A. Maturilli, N. Müller, A. Hagermann, N. Sakatani, S. Tanaka, T. Arai, S. Mottola, S. Tachibana, I. Pelivan, L. Drube, J. B. Vincent, H. Yano, C. Pilorget, K. D. Matz, N. Schmitz, A. Koncz, S. E. Schröder, F. Trauthan, M. Schlotterer, C. Krause, T. M. Ho, A. Moussi-Soffys
    Nature Astronomy 3(11) 971-976 2019年11月1日  査読有り
    © 2019, The Author(s), under exclusive licence to Springer Nature Limited. C-type asteroids are among the most pristine objects in the Solar System, but little is known about their interior structure and surface properties. Telescopic thermal infrared observations have so far been interpreted in terms of a regolith-covered surface with low thermal conductivity and particle sizes in the centimetre range. This includes observations of C-type asteroid (162173) Ryugu1–3. However, on arrival of the Hayabusa2 spacecraft at Ryugu, a regolith cover of sand- to pebble-sized particles was found to be absent4,5 (R.J. et al., manuscript in preparation). Rather, the surface is largely covered by cobbles and boulders, seemingly incompatible with the remote-sensing infrared observations. Here we report on in situ thermal infrared observations of a boulder on the C-type asteroid Ryugu. We found that the boulder’s thermal inertia was much lower than anticipated based on laboratory measurements of meteorites, and that a surface covered by such low-conductivity boulders would be consistent with remote-sensing observations. Our results furthermore indicate high boulder porosities as well as a low tensile strength in the few hundred kilopascal range. The predicted low tensile strength confirms the suspected observational bias6 in our meteorite collections, as such asteroidal material would be too frail to survive atmospheric entry7.
  • R. Jaumann, N. Schmitz, T. M. Ho, S. E. Schröder, K. A. Otto, K. Stephan, S. Elgner, K. Krohn, F. Preusker, F. Scholten, J. Biele, S. Ulamec, C. Krause, S. Sugita, K. D. Matz, T. Roatsch, R. Parekh, S. Mottola, M. Grott, P. Michel, F. Trauthan, A. Koncz, H. Michaelis, C. Lange, J. T. Grundmann, M. Maibaum, K. Sasaki, F. Wolff, J. Reill, A. Moussi-Soffys, L. Lorda, W. Neumann, J. B. Vincent, R. Wagner, J. P. Bibring, S. Kameda, H. Yano, S. Watanabe, M. Yoshikawa, Y. Tsuda, T. Okada, T. Yoshimitsu, Y. Mimasu, T. Saiki, H. Yabuta, H. Rauer, R. Honda, T. Morota, Y. Yokota, T. Kouyama
    Science 365(6455) 817-820 2019年8月23日  査読有り
    © 2017 The Authors. The near-Earth asteroid (162173) Ryugu is a 900-m-diameter dark object expected to contain primordial material from the solar nebula. The Mobile Asteroid Surface Scout (MASCOT) landed on Ryugu’s surface on 3 October 2018. We present images from the MASCOT camera (MASCam) taken during the descent and while on the surface. The surface is covered by decimeter- to meter-sized rocks, with no deposits of fine-grained material. Rocks appear either bright, with smooth faces and sharp edges, or dark, with a cauliflower-like, crumbly surface. Close-up images of a rock of the latter type reveal a dark matrix with small, bright, spectrally different inclusions, implying that it did not experience extensive aqueous alteration. The inclusions appear similar to those in carbonaceous chondrite meteorites.
  • T. Okada
    Proceedings of QIRT Asia 2019 S9-01 2019年7月  査読有り招待有り筆頭著者責任著者
  • Tra Mi Ho, Ralf Jaumann, Jean Pierre Bibring, Matthias Grott, Karl Heinz Glassmeier, Aurelie Moussi, Ulrich Auster, Jens Biele, Barbara Cozzoni, Clement Dudal, Cinzia Fantinati, Jan Thimo Grundmann, David Hercik, Kagan Kayal, Joerg Knollenberg, Christian Krause, Oliver Küchemann, Caroline Lange, Michael Lange, Laurence Lorda, Michael Maibaum, Yuya Mimasu, Celine Cenac-Morthe, Cedric Pilorget, Tatsuaki Okada, Josef Reill, Takano Saiki, Kaname Sasaki, Nicole Schmitz, Nortbert Toth, Yuichi Tsuda, Stephan Ulamec, Friederike Wolff, Tetsuo Yoshimitsu
    Proceedings of the International Astronautical Congress, IAC 2019-October 2019年  査読有り
    Copyright © 2019 by the International Astronautical Federation (IAF). All rights reserved. On October 3rd, 2018, the MASCOT lander has been deployed successfully by the Hayabusa2 spacecraft from an altitude of 41m onto the C-type near-Earth asteroid (162173) Ryugu. After a free-fall of approx. 6 minutes MASCOT has experienced its first contact with the asteroid. The lander underwent a bouncing phase of ~ 11 minutes before it finally came to rest at its first settlement point where it entered into its on-surface operational mode. The lander was able to perform science measurements with its payload suite at 3 locations on Ruygu. After about 17 hrs of operations, the MASCOT mission terminated with the last communication contact. The lander was jointly developed by the German Aerospace Centre (DLR) and the Centre National d'Etudes Spatiales (CNES). The payload suite of four scientific instruments is provided by DLR Berlin (MASCam wide-angle camera with colour illumination and MARA thermal IR radiometer), IAS Paris (MicrOmega hyperspectral IR soil microscope) and TU Braunschweig (MASMag magnetometer). The paper will outline the path of the lander on the asteroid and present a summary of the scientific observations. These first results are related to the progress of the Hayabusa2 mission and its MINERVA-II rovers on the background of a recap of the landing site selection process.
  • Katsushi Furutani, Ryota Inukai, Tatsuaki Okada, Kazuto Saiki, Hiroyuki Ohue
    Proceedings - 34th ASPE Annual Meeting 431-434 2019年  査読有り
  • S. Watanabe, M. Hirabayashi, N. Hirata, N. Hirata, R. Noguchi, Y. Shimaki, H. Ikeda, E. Tatsumi, M. Yoshikawa, S. Kikuchi, H. Yabuta, T. Nakamura, S. Tachibana, Y. Ishihara, T. Morota, K. Kitazato, N. Sakatani, K. Matsumoto, K. Wada, H. Senshu, C. Honda, T. Michikami, H. Takeuchi, T. Kouyama, R. Honda, S. Kameda, T. Fuse, H. Miyamoto, G. Komatsu, S. Sugita, T. Okada, N. Namiki, M. Arakawa, M. Ishiguro, M. Abe, R. Gaskell, E. Palmer, O. S. Barnouin, P. Michel, A. S. French, J. W. McMahon, D. J. Scheeres, P. A. Abell, Y. Yamamoto, S. Tanaka, K. Shirai, M. Matsuoka, M. Yamada, Y. Yokota, H. Suzuki, K. Yoshioka, Y. Cho, S. Tanaka, N. Nishikawa, T. Sugiyama, H. Kikuchi, R. Hemmi, T. Yamaguchi, N. Ogawa, G. Ono, Y. Mimasu, K. Yoshikawa, T. Takahashi, Y. Takei, A. Fujii, C. Hirose, T. Iwata, M. Hayakawa, S. Hosoda, O. Mori, H. Sawada, T. Shimada, S. Soldini, H. Yano, R. Tsukizaki, M. Ozaki, Y. Iijima, K. Ogawa, M. Fujimoto, T. M. Ho, A. Moussi, R. Jaumann, J. P. Bibring, C. Krause, F. Terui, T. Saiki, S. Nakazawa, Y. Tsuda
    Science 364(6437) 268-272 2019年  査読有り
    © 2019 American Association for the Advancement of Science. All rights reserved. The Hayabusa2 spacecraft arrived at the near-Earth carbonaceous asteroid 162173 Ryugu in 2018.We present Hayabusa2 observations of Ryugu's shape, mass, and geomorphology. Ryugu has an oblate "spinning top" shape, with a prominent circular equatorial ridge. Its bulk density, 1.19 ± 0.02 grams per cubic centimeter, indicates a high-porosity (>50%) interior. Large surface boulders suggest a rubble-pile structure. Surface slope analysis shows Ryugu's shape may have been produced from having once spun at twice the current rate. Coupled with the observed global material homogeneity, this suggests that Ryugu was reshaped by centrifugally induced deformation during a period of rapid rotation. From these remote-sensing investigations, we identified a suitable sample collection site on the equatorial ridge.
  • S. Sugita, R. Honda, T. Morota, S. Kameda, H. Sawada, E. Tatsumi, M. Yamada, C. Honda, Y. Yokota, T. Kouyama, N. Sakatani, K. Ogawa, H. Suzuki, T. Okada, N. Namiki, S. Tanaka, Y. Iijima, K. Yoshioka, M. Hayakawa, Y. Cho, M. Matsuoka, N. Hirata, N. Hirata, H. Miyamoto, D. Domingue, M. Hirabayashi, T. Nakamura, T. Hiroi, T. Michikami, P. Michel, R. L. Ballouz, O. S. Barnouin, C. M. Ernst, S. E. Schröder, H. Kikuchi, R. Hemmi, G. Komatsu, T. Fukuhara, M. Taguchi, T. Arai, H. Senshu, H. Demura, Y. Ogawa, Y. Shimaki, T. Sekiguchi, T. G. Müller, A. Hagermann, T. Mizuno, H. Noda, K. Matsumoto, R. Yamada, Y. Ishihara, H. Ikeda, H. Araki, K. Yamamoto, S. Abe, F. Yoshida, A. Higuchi, S. Sasaki, S. Oshigami, S. Tsuruta, K. Asari, S. Tazawa, M. Shizugami, J. Kimura, T. Otsubo, H. Yabuta, S. Hasegawa, M. Ishiguro, S. Tachibana, E. Palmer, R. Gaskell, L. Le Corre, R. Jaumann, K. Otto, N. Schmitz, P. A. Abell, M. A. Barucci, M. E. Zolensky, F. Vilas, F. Thuillet, C. Sugimoto, N. Takaki, Y. Suzuki, H. Kamiyoshihara, M. Okada, K. Nagata, M. Fujimoto, M. Yoshikawa, Y. Yamamoto, K. Shirai, R. Noguchi, N. Ogawa, F. Terui, S. Kikuchi, T. Yamaguchi, Y. Oki, Y. Takao, H. Takeuchi, G. Ono
    Science 364(6437) 252-252 2019年  査読有り
    © 2019 American Association for the Advancement of Science. All rights reserved. The near-Earth carbonaceous asteroid 162173 Ryugu is thought to have been produced from a parent body that contained water ice and organic molecules. The Hayabusa2 spacecraft has obtained global multicolor images of Ryugu. Geomorphological features present include a circum-equatorial ridge, east-west dichotomy, high boulder abundances across the entire surface, and impact craters. Age estimates from the craters indicate a resurfacing age of ≤ 106 years for the top 1-meter layer. Ryugu is among the darkest known bodies in the Solar System. The high abundance and spectral properties of boulders are consistent with moderately dehydrated materials, analogous to thermally metamorphosed meteorites found on Earth. The general uniformity in color across Ryugu's surface supports partial dehydration due to internal heating of the asteroid's parent body.
  • K. Kitazato, R. E. Milliken, T. Iwata, M. Abe, M. Ohtake, S. Matsuura, T. Arai, Y. Nakauchi, T. Nakamura, M. Matsuoka, H. Senshu, N. Hirata, T. Hiroi, C. Pilorget, R. Brunetto, F. Poulet, L. Riu, J. P. Bibring, D. Takir, D. L. Domingue, F. Vilas, M. A. Barucci, D. Perna, E. Palomba, A. Galiano, K. Tsumura, T. Osawa, M. Komatsu, A. Nakato, T. Arai, N. Takato, T. Matsunaga, Y. Takagi, K. Matsumoto, T. Kouyama, Y. Yokota, E. Tatsumi, N. Sakatani, Y. Yamamoto, T. Okada, S. Sugita, R. Honda, T. Morota, S. Kameda, H. Sawada, C. Honda, M. Yamada, H. Suzuki, K. Yoshioka, M. Hayakawa, K. Ogawa, Y. Cho, K. Shirai, Y. Shimaki, N. Hirata, A. Yamaguchi, N. Ogawa, F. Terui, T. Yamaguchi, Y. Takei, T. Saiki, S. Nakazawa, S. Tanaka, M. Yoshikawa, S. Watanabe, Y. Tsuda
    Science 364(6437) 272-275 2019年  査読有り
    © 2019 American Association for the Advancement of Science. All rights reserved. The near-Earth asteroid 162173 Ryugu, the target of the Hayabusa2 sample-return mission, is thought to be a primitive carbonaceous object. We report reflectance spectra of Ryugu's surface acquired with the Near-Infrared Spectrometer (NIRS3) on Hayabusa2, to provide direct measurements of the surface composition and geological context for the returned samples. A weak, narrow absorption feature centered at 2.72 micrometers was detected across the entire observed surface, indicating that hydroxyl (OH)-bearing minerals are ubiquitous there. The intensity of the OH feature and low albedo are similar to thermally and/or shock-metamorphosed carbonaceous chondrite meteorites. There are few variations in the OH-band position, which is consistent with Ryugu being a compositionally homogeneous rubble-pile object generated from impact fragments of an undifferentiated aqueously altered parent body.
  • 檜原弘樹, 檜原弘樹, 佐野淳平, 益田哲也, 大嶽久志, 岡田達明, 尾川順子, 津田雄一
    電子情報通信学会技術研究報告 118(456(DC2018 71-84)(Web)) 77-82 2019年  査読有り
  • Koji Wada, Matthias Grott, Patrick Michel, Kevin J. Walsh, Antonella M. Barucci, Jens Biele, Juergen Blum, Carolyn M. Ernst, Jan Thimo Grundmann, Bastian Gundlach, Axel Hagermann, Maximilian Hamm, Martin Jutzi, Myung-Jin Kim, Ekkehard Kuehrt, Lucille Le Corre, Guy Libourel, Roy Lichtenheldt, Alessandro Maturilli, Scott R. Messenger, Tatsuhiro Michikami, Hideaki Miyamoto, Stefano Mottola, Thomas Mueller, Akiko M. Nakamura, Larry R. Nittler, Kazunori Ogawa, Tatsuaki Okada, Ernesto Palomba, Naoya Sakatani, Stefan E. Schroeder, Hiroki Senshu, Driss Takir, Michael E. Zolensky
    PROGRESS IN EARTH AND PLANETARY SCIENCE 5(1) 82-82 2018年12月  査読有り
    Asteroid (162173) Ryugu is the target object of Hayabusa2, an asteroid exploration and sample return mission led by Japan Aerospace Exploration Agency (JAXA). Ground-based observations indicate that Ryugu is a C-type near-Earth asteroid with a diameter of less than 1km, but the knowledge of its detailed properties is very limited prior to Hayabusa2 observation. This paper summarizes our best understanding of the physical and dynamical properties of Ryugu based on ground-based remote sensing and theoretical modeling before the Hayabusa2's arrival at the asteroid. This information is used to construct a design reference model of the asteroid that is used for the formulation of mission operation plans in advance of asteroid arrival. Particular attention is given to the surface properties of Ryugu that are relevant to sample acquisition. This reference model helps readers to appropriately interpret the data that will be directly obtained by Hayabusa2 and promotes scientific studies not only for Ryugu itself and other small bodies but also for the solar system evolution that small bodies shed light on.
  • Tomohiro Yamaguchi, Takanao Saiki, Satoshi Tanaka, Yuto Takei, Tatsuaki Okada, Tadateru Takahashi, Yuichi Tsuda
    Acta Astronautica 151 217-227 2018年10月  査読有り
    This paper presents the robust planning of the Hayabusa2-Ryugu proximity operation and landing site selection process considering unknown asteroid environment and the spacecraft constraints. The proximity operation scenario is described together with the relationship between the selection process and the in-situ observation. The mission constraints are summarized for the possible asteroid environment, including the rotation state, thermal condition and gravity.
  • Tatsuaki Okada, Yoko Kebukawa, Jun Aoki, Jun Matsumoto, Hajime Yano, Takahiro Iwata, Osamu Mori, Jean-Pierre Bibring, Stephan Ulamec, Ralf Jaumann
    Planetary and Space Science 161 99-106 2018年10月  査読有り筆頭著者責任著者
    An engineering mission OKEANOS to explore a Jupiter Trojan asteroid, using a Solar Power Sail is currently under study. After a decade-long cruise, it will rendezvous with the target asteroid, conduct global mapping of the asteroid from the spacecraft, and in situ measurements on the surface, using a lander. Science goals and enabling instruments of the mission are introduced, as the results of the joint study between the scientists and engineers from Japan and Europe.
  • Tatsuaki Okada, Tetsuya Fukuhara, Satoshi Tanaka, Makoto Taguchi, Takehiko Arai, Hiroki Senshu, Hirohide Demura, Yoshiko Ogawa, Toru Kouyama, Naoya Sakatani, Jun Takita, Tomohiko Sekiguchi, Jorn Helbert, Thomas G. Mueller, Axel Hagermann
    Planetary and Space Science 158 46-52 2018年9月  査読有り筆頭著者責任著者
    Thermal Infrared Imager TIR on Hayabusa2 has proven its in-flight performance to detect celestial bodies during the cruise phase, especially by the observations of the Earth and the Moon before and after the Earth swing-by on 3rd of December 2015. The result indicates that the target C-type asteroid 162173 Ryugu will be detected from the distance of 3000 km at the beginning of the approach phase, and that a C-type small moon larger than 1 m will be detected from the home position, 20 km from the asteroid, if it orbits around the asteroid.
  • Osamu MORI, Jun MATSUMOTO, Toshihiro CHUJO, Hideki KATO, Takanao SAIKI, Junichiro KAWAGUCHI, Shigeo KAWASAKI, Tatsuaki OKADA, Takahiro IWATA, Yuki TAKAO
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 16(4) 328-333 2018年  査読有り
  • Katsushi Furutani, Ryota Inukai, Takayoshi Takano, Tatsuaki Okada, Kazuto Saiki, Hiroyuki Ohue
    Proceedings - 33rd ASPE Annual Meeting 273-276 2018年  査読有り
  • Joern Helbert, Anko Boerner, Alessandro Maturilli, Mario D'Amore, Matthias Grott, Jörg Knollenberg, Gabriele E. Arnold, Ernesto Palomba, Tatsuaki Okada, Pierre Vernazza, Andrew Rivkin, Indhu Varatharajan, Ingo Walter, Thomas Säuberlich, Gisbert Peter
    Proceedings of SPIE - The International Society for Optical Engineering 10765 10765-10765 2018年  査読有り
    © 2018 SPIE. TROTIS (TROjan asteroid Thermal Infrared multi-Spectral imager) is a high spatial-resolution thermal imaging system optimized for targets in the outer solar system with heritage from the Miniaturized Asteroid thermal infrared Imager and Radiometer (MAIR) for the AIDA mission as well as Bepi-Colombo mission's MErcury Radiometer and Thermal Infrared Spectrometer (MERTIS). TROTIS will provide unique science observations that will foster our understanding of Trojan asteroids. It will provide compositional information, thermal physical properties as well as help determine accurate shapes. In addition TROTIS can aid optical navigation, as it will be able to detect targets from any phase angle.
  • C. Krause, U. Auster, J. P. Bibring, J. Biele, C. Cenac, B. Cozzoni, C. Dudal, D. Embacher, C. Fantinati, H. H. Fischer, K. H. Glassmeier, D. Granena, M. Grott, J. T. Grundmann, V. Hamm, D. Hercik, T. M. Ho, R. Jaumann, K. Kayal, J. Knollenberg, O. Küchemann, C. Lange, L. Lorda, M. Maibaum, D. May, A. Moussi, T. Okada, J. Reill, T. Saiki, K. Sasaki, M. Schlotterer, N. Schmitz, N. Termtanasombat, Y. Tsuda, S. Ulamec, T. Yoshimitsu, C. Ziach
    15th International Conference on Space Operations, 2018 2018年  査読有り
  • 岡田達明
    WEB+DB Press 96 90-92 2017年10月  査読有り筆頭著者責任著者
  • Tra-Mi Ho, Volodymyr Baturkin, Christian Grimm, Jan Thimo Grundmann, Thimo Grundmann, Catherin Hobbie, Eugen Ksenik, Caroline Lange, Kaname Sasaki, Markus Schlotterer, Maria Talapina, Nawarat Termtanasombat, Elisabet Wejmo, Lars Witte, Michael Wrasmann, Guido Wuebbels, Johannes Roessler, Christian Ziach, Ross Findlay, Jens Biele, Christian Krause, Stephan Ulamec, Michael Lange, Olaf Mierheim, Roy Lichtenheldt, Maximilian Maier, Josef Reill, Hans-Juergen Sedlmayr, Pierre Bousquet, Anthony Bellion, Olivier Bompis, Celine Cenac-Morthe, Muriel Deleuze, Stephane Fredon, Eric Jurado, Elisabet Canalias, Ralf Jaumann, Jean-Pierre Bibring, Karl Heinz Glassmeier, David Hercik, Matthias Grott, Luca Celotti, Federico Cordero, Jeffrey Hendrikse, Tatsuaki Okada
    SPACE SCIENCE REVIEWS 208(1-4) 339-374 2017年7月  査読有り
    On December 3rd, 2014, the Japanese Space Agency (JAXA) launched successfully the Hayabusa2 (HY2) spacecraft to its journey to Near Earth asteroid (162173) Ryugu. Aboard this spacecraft is a compact landing package, MASCOT (Mobile Asteroid surface SCOuT), which was developed by the German Aerospace Centre (DLR) in collaboration with the Centre National d'Etudes Spatiales (CNES). Similar to the famous predecessor mission Hayabusa, Hayabusa2, will also study an asteroid and return samples to Earth. This time, however, the target is a C-type asteroid which is considered to be more primitive than (25143) Itokawa and provide insight into an even earlier stage of our Solar System.Upon arrival at asteroid Ryugu in 2018, MASCOT will be released from the HY2 spacecraft and gently descend by free fall from an altitude of about 100 m to the surface of the asteroid. After a few bounces, the lander will come to rest at the surface and perform its scientific investigations of the surface structure and mineralogical composition, the thermal behaviour and the magnetic properties by operating its four scientific instruments. Those include an IR imaging spectrometer (MicrOmega, IAS Paris), a camera (MASCAM, DLR Berlin), a radiometer (MARA, DLR Berlin) and a magnetometer (MASMAG, TU Braunschweig).In order to allow optimized payload operations the thermal design of MASCOT is required to cope with the contrasting requirements of the 4-year cruise in cold environment versus the hot conditions on the surface of the asteroid. Operations up to 2 asteroid days (similar to 16 hours) based on a primary battery are currently envisaged. A mobility mechanism allows locomotion on the surface. The mechanism is supported by an attitude and motion sensing system and an intelligent autonomy manager, which is implemented in the onboard software that enables MASCOT to operate fully independently when ground intervention is not available.
  • R. Jaumann, N. Schmitz, A. Koncz, H. Michaelis, S. E. Schroeder, S. Mottola, F. Trauthan, H. Hoffmann, T. Roatsch, D. Jobs, J. Kachlicki, B. Pforte, R. Terzer, M. Tschentscher, S. Weisse, U. Mueller, L. Perez-Prieto, B. Broll, A. Kruselburger, T. M. Ho, J. Biele, S. Ulamec, C. Krause, M. Grott, J. P. Bibring, S. Watanabe, S. Sugita, T. Okada, M. Yoshikawa, H. Yabuta
    Space Science Reviews 208(1-4) 375-400 2017年7月1日  査読有り
    © 2016, Springer Science+Business Media Dordrecht. The MASCOT Camera (MasCam) is part of the Mobile Asteroid Surface Scout (MASCOT) lander’s science payload. MASCOT has been launched to asteroid (162173) Ryugu onboard JAXA’s Hayabusa 2 asteroid sample return mission on Dec 3rd, 2014. It is scheduled to arrive at Ryugu in 2018, and return samples to Earth by 2020. MasCam was designed and built by DLR’s Institute of Planetary Research, together with Airbus-DS Germany. The scientific goals of the MasCam investigation are to provide ground truth for the orbiter’s remote sensing observations, provide context for measurements by the other lander instruments (radiometer, spectrometer and magnetometer), the orbiter sampling experiment, and characterize the geological context, compositional variations and physical properties of the surface (e.g. rock and regolith particle size distributions). During daytime, clear filter images will be acquired. During night, illumination of the dark surface is performed by an LED array, equipped with 4 × 36 monochromatic light-emitting diodes (LEDs) working in four spectral bands. Color imaging will allow the identification of spectrally distinct surface units. Continued imaging during the surface mission phase and the acquisition of image series at different sun angles over the course of an asteroid day will contribute to the physical characterization of the surface and also allow the investigation of time-dependent processes and to determine the photometric properties of the regolith. The MasCam observations, combined with the MASCOT hyperspectral microscope (MMEGA) and radiometer (MARA) thermal observations, will cover a wide range of observational scales and serve as a strong tie point between Hayabusa 2’s remote-sensing scales (10 3–10 − 3m) and sample scales (10 − 3–10 − 6m). The descent sequence and the close-up images will reveal the surface features over a broad range of scales, allowing an assessment of the surface’s diversity and close the gap between the orbital observations and those made by the in-situ measurements. The MasCam is mounted inside the lander slightly tilted, such that the center of its 54.8° square field-of-view is directed towards the surface at an angle of 22° with respect to the surface plane. This is to ensure that both the surface close to the lander and the horizon are observable. The camera optics is designed according to the Scheimpflug principle, thus that the entire scene along the camera’s depth of field (150 mm to infinity) is in focus. The camera utilizes a 1024 × 1024 pixel CMOS sensor sensitive in the 400–1000 nm wavelength range, peaking at 600–700 nm. Together with the f-16 optics, this yields a nominal ground resolution of 150 micron/px at 150 mm distance (diffraction limited). The camera flight model has undergone standard radiometric and geometric calibration both at the component and system (lander) level. MasCam relies on the use of wavelet compression to maximize data return within stringent mission downlink limits. All calibration and flight data products will be generated and archived in the Planetary Data System in PDS image format.
  • Takehiko Arai, Tomoki Nakamura, Satoshi Tanaka, Hirohide Demura, Yoshiko Ogawa, Naoya Sakatani, Yamato Horikawa, Hiroki Senshu, Tetsuya Fukuhara, Tatsuaki Okada
    SPACE SCIENCE REVIEWS 208(1-4) 239-254 2017年7月  査読有り責任著者
    The thermal infrared imager (TIR) is a thermal infrared camera onboard the Hayabusa2 spacecraft. TIR will perform thermography of a C-type asteroid, 162173 Ryugu (1999 JU(3)), and estimate its surface physical properties, such as surface thermal emissivity epsilon, surface roughness, and thermal inertia Gamma, through remote in-situ observations in 2018 and 2019. In prelaunch tests of TIR, detector calibrations and evaluations, along with imaging demonstrations, were performed. The present paper introduces the experimental results of a prelaunch test conducted using a large-aperture collimator in conjunction with TIR under atmospheric conditions. A blackbody source, controlled at constant temperature, was measured using TIR in order to construct a calibration curve for obtaining temperatures from observed digital data. As a known thermal emissivity target, a sandblasted black almite plate warmed from the back using a flexible heater was measured by TIR in order to evaluate the accuracy of the calibration curve. As an analog target of a C-type asteroid, carbonaceous chondrites (50 mm x 2 mm in thickness) were also warmed from the back and measured using TIR in order to clarify the imaging performance of TIR. The calibration curve, which was fitted by a specific model of the Planck function, allowed for conversion to the target temperature within an error of 1 degrees C (3 sigma standard deviation) for the temperature range of 30 to 100 degrees C. The observed temperature of the black almite plate was consistent with the temperature measured using K-type thermocouples, within the accuracy of temperature conversion using the calibration curve when the temperature variation exhibited a random error of 0.3 degrees C (1 sigma) for each pixel at a target temperature of 50 degrees C. TIR can resolve the fine surface structure of meteorites, including cracks and pits with the specified field of view of 0.051. (328 x 248 pixels). There were spatial distributions with a temperature variation of 3 degrees C at the setting temperature of 50 degrees C in the thermal images obtained by TIR. If the spatial distribution of the temperature is caused by the variation of the thermal emissivity, including the effects of the surface roughness, the difference of the thermal emissivity Delta epsilon is estimated to be approximately 0.08, as calculated by the Stefan-Boltzmann raw. Otherwise, if the distribution of temperature is caused by the variation of the thermal inertia, the difference of the thermal inertia Delta Gamma is calculated to be approximately 150 J m(-2) s(0.5) K-1, based on a simulation using a 20-layer model of the heat balance equation. The imaging performance of TIR based on the results of the meteorite experiments indicates that TIR can resolve the spatial distribution of thermal emissivity and thermal inertia of the asteroid surface within accuracies of Delta epsilon congruent to 0.02 and Delta Gamma congruent to 20 J m(-2) s(0.5) K-1, respectively. However, the effects of the thermal emissivity and thermal inertia will degenerate in thermal images of TIR. Therefore, TIR will observe the same areas of the asteroid surface numerous times (>10 times, in order to ensure statistical significance), which allows us to determine both the parameters of the surface thermal emissivity and the thermal inertia by least-squares fitting to a thermal model of Ryugu.
  • Christian Ziach, Volodymyr Baturkin, Christian Grimm, Jan Thimo Grundmann, Tra Mi Ho, Caroline Lange, Kaname Sasaki, Nawarat Termtanasombat, Norbert Toth, Elisabet Wejmo, Maximilian Maier, Josef Reill, Hans Jürgen Sedlmayr, Friederike Wolff, Michael Lange, Olaf Mierheim, Jens Biele, Barbara Cozzoni, Cinzia Fantinati, Koen Geurts, Kagan Kayal, Christian Krause, Oliver Küchemann, Michael Maibaum, Stephan Ulamec, Matthias Grott, Ralf Jaumann, Céline Cénac-Morthe, Muriel Deleuze, Clément Dudal, David Granena, Laurence Lorda, Aurélie Moussi, Jean Pierre Bibring, David Hercik, Hans Ulrich Auster, Yuya Mimasu, Tatsuaki Okada, Takanao Saiki, Sathoshi Tanaka, Fuyuto Terui, Yuichi Tsuda, Tomohiro Yamaguchi, Tetsuo Yoshimitsu, Seiichiro Watanabe
    Proceedings of the International Astronautical Congress, IAC 5 2897-2904 2017年  査読有り
    © Copyright 2017 by the International Astronautical Federation (IAF). All rights reserved. Launched in December 2014 the Japanese spacecraft Hayabusa2 (HY2) and its small passenger MASCOT (Mobile Asteroid surface SCOuT) have meanwhile successfully performed more than half of their 4-year-long voyage to reach their target body, asteroid (162173) Ryugu, formerly referred to as 1999 JU3. While Hayabusa2 is aiming to characterize Ryugu on a global scale and to return samples to Earth, MASCOT's mission is to land on the surface, perform in-situ investigations and thus provide ground truth and context information for the overall Hayabusa2 science activities. The lander was jointly developed by the German Aerospace Centre (DLR) and the Centre National d'Etudes Spatiales (CNES). It is equipped with a sensor suite of four scientific instruments: a hyperspectral IR spectrometer (MicrOmega, IAS Paris), a camera (MasCam, DLR Berlin), a radiometer (MARA, DLR Berlin) and a magnetometer (MasMag, TU Braunschweig) to investigate Ryugu's surface structure, composition and physical properties including its thermal behaviour and magnetization. The planned on surface sequence of measurements will be repeated in a different site after MASCOT's relocation on the asteroid surface. Therefore a mobility subsystem was developed to make MASCOT jump due to applied angular momentum of an eccentric rotating mass inside the system. Since the characteristics of Ryugu such as the exact orientation of the rotation axis, the thermal conditions, shape and surface structure will be known only after arrival of Hayabusa2 in July 2018 there will be only a few weeks available to select a landing site and refine the specific MASCOT mission parameters according to the conditions found, before the landing can take place, in October 2018. MASCOT's on-asteroid lifetime is limited by the capacity of its primary battery which is the main driver to make maximum use of the given time. In order to prepare MASCOT's operation within these constraints, both, space and ground systems have to be well prepared and descent and on-asteroid phases need to be rigorously planned and tested. This paper will summarize the already performed and planned in-flight activities such as health checks, calibration activities, data transfer tests, and will report on MASCOTs overall health state. Beyond that, all on-ground activities such as the landing site selection process, the verification of operational timelines, planning and training aspects will be outlined.
  • Aurélie Moussi, Laurence Lorda, Céline Cénac-Morthé, David Granena, Clement Dudal, Elisabet Canalias, Thierry Martin, Muriel Deleuze, Jean Pierre Bibring, Vincent Hamm, Cédric Pilorget, Tra Mi Ho, Christian Ziach, Jan Thimo Grundmann, Nawarat Termtanasombat, Christian Krause, Cinzia Fantinati, Michael Maibaum, Barbara Cozzoni, Jens Biele, Yuya Mimasu, Tatsuaki Okada, Takanao Saiki, Sathoshi Tanaka, Fuyuto Terui, Yuichi Tsuda, Tomohiro Yamaguchi, Tetsuo Yoshimitsu, Seiichiro Watanabe
    Proceedings of the International Astronautical Congress, IAC 5 2905-2915 2017年  査読有り
    © Copyright 2017 by the International Astronautical Federation (IAF). All rights reserved. Hayabusa-2 is an asteroid sample return mission operated by the Japanese space agency, JAXA. It was launched in December 2014. The spacecraft has already performed half of its 4-year-long cruise to reach the mission target, a kilometer-sized C-type asteroid, one of the most pristine class of objects in our Solar System, called Ryugu. Its analysis, with a special emphasis on organics and hydrated minerals, will give essential clues for the understanding of the Solar System formation and evolution. The small lander MASCOT (Mobile Asteroid surface SCOuT) carried aboard Hayabusa-2 is intended to land on the surface for in-situ investigations while the probe is aiming to study Ryugu on a global scale and to return samples to Earth. MASCOT was jointly developed by the German Aerospace Centre (DLR) and the Centre National d'Etudes Spatiales (CNES). It is equipped with a sensor suite consisting of four fully-fledged instruments. DLR was responsible for developing the MASCOT lander and its ground segment, and is in charge of planning and conducting lander operations. CNES supplied the near-IR hyperspectral microscope MicrOmega developed at IAS, the antennas and the electrical power system that would be essential contributors to the on-asteroid operation success. Some of these subsystems are partly inherited from the Philae lander aboard the Rosetta mission. CNES is responsible for the MASCOT flight dynamics and is also providing a support for RF link, based on the expertise gained on the past science missions. The characteristics of Ryugu including the shape will be known only after arrival of Hayabusa-2 in July 2018. Moreover, the MASCOT's primary battery is expected to supply power to the lander only for 2 asteroid days to perform science activities on the surface. Thus, the time available will be very short for either task and the different processes and teams involved have to be well prepared and trained. This paper is a complement to the project status presented in the "MASCOT - Preparations for its landing in 2018: a status update from ground and space one year ahead of the landing on Ryugu" [1]. It will summarize the already performed and planned activities to prepare the French expertise center at CNES while focusing on the improvements/adaptations made on the subsystems inherited from Philae.
  • Tomohiro Yamaguchi, Takanao Saiki, Satoshi Tanaka, Yuto Takei, Tatsuaki Okada, Tadateru Takahashi, Yuichi Tsuda
    Proceedings of the International Astronautical Congress, IAC 5 2889-2896 2017年  査読有り
    © Copyright 2017 by the International Astronautical Federation (IAF). All rights reserved. This paper presents the robust planning of the Hayabusa2-Ryugu proximity operation and landing site selection process considering unknown asteroid environment and the spacecraft constraints. The proximity operation scenario is described together with the relationship between the selection process and the in-situ observation. The mission constraints are summarized for the possible asteroid environment, including the rotation state, thermal condition and gravity.
  • Ken Endo, Hirohide Demura, Takayuki Dairaku, Tetsuya Fukuhara, Tatsuaki Okada, Satoshi Tanaka
    2017 IEEE AEROSPACE CONFERENCE 978(1) 5090 2017年  査読有り
    Hayabusa2 is a sample return mission to asteroid 162173 Ryugu, which will arrive in 2018. The Thermal Infrared Imager (TIR) is onboard the spacecraft and will be used to make thermal observations to ensure a safe touch down and sample return, and to study the nature of the asteroid. This study developed a TIR database and data browser. Our developments are called Hayabusa2 Exploration Assistant for TIR (HEAT). HEAT has three uses: visualization, calibration, and analysis. It covers all of the uses based on functions, browsers, the database, and a data processor. This study considers two ways to perform calibrations: regression and direct conversion, which is interpolation with all of the ground test data. The TIR data analysis involves the following. First, TIR images are collected. Then, the local time is obtained for a specified longitudinal zone of the shape model. A TIR image includes surface temperature information. Third, the temporal profile of surface temperature is combined with individual TIR images and the local time. Fourth, the thermal inertia of the local site is estimated from the profile. Fifth, the thermal inertia is mapped. Finally, the thermal model is established by integrating the thermal inertia.
  • Nobuyuki Hasebe, Toru Ohta, Yoshiharu Amano, Masayuki Naito, Hiroki Kusano, Hiroshi Nagaoka, Kohei Yoshida, Takuto Adachi, Timothy J. Fagan, Haruyoshi Kuno, Eido Shibamura, Akira Hitachi, José A. Matias Lopes, Jesus Martínez-Frías, Tomoki Nakamura, Shingo Kameda, Yuichiro Cho, Naoki Shirai, Hideaki Miyamoto, Takafumi Niihara, Takashi Mikouchi, Tatsuaki Okada, Yuzuru Karouji
    Proceedings of International Symposium on Radiation Detectors and Their Uses (ISRD2016) 2016年11月14日  
  • Osamu MORI, Takanao SAIKI, Hideki KATO, Yuichi TSUDA, Yuya MIMASU, Yoji SHIRASAWA, Ralf BODEN, Jun MATSUMOTO, Toshihiro CHUJO, Shota KIKUCHI, Junji KIKUCHI, Yusuke OKI, Kosuke AKATSUKA, Takahiro IWATA, Tatsuaki OKADA, Hajime YANO, Shuji MATSUURA, Ryosuke NAKAMURA, Yoko KEBUKAWA, Jun AOKI, Junichiro KAWAGUCHI
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 14(ists30) Pk_1-Pk_7 2016年7月29日  査読有り
  • Tatsuaki Okada, Tetsuya Fukuhara, Satoshi Tanaka, Makoto Taguchi, Takeshi Imamura, Takehiko Arai, Hiroki Senshu, Yoshiko Ogawa, Hirohide Demura, Kohei Kitazato, Ryosuke Nakamura, Toru Kouyama, Tomohiko Sekiguchi, Sunao Hasegawa, Tsuneo Matsunaga, Takehiko Wada, Jun Takita, Naoya Sakatani, Yamato Horikawa, Ken Endo, Jörn Helbert, Thomas G. Müller, Axel Hagermann
    Space Science Reviews 208(1-4) 255-286 2016年  査読有り筆頭著者責任著者
    The thermal infrared imager TIR onboard Hayabusa2 has been developed to investigate thermo-physical properties of C-type, near-Earth asteroid 162173 Ryugu. TIR is one of the remote science instruments on Hayabusa2 designed to understand the nature of a volatile-rich solar system small body, but it also has significant mission objectives to provide information on surface physical properties and conditions for sampling site selection as well as the assessment of safe landing operations. TIR is based on a two-dimensional un-cooled micro-bolometer array inherited from the Longwave Infrared Camera LIR on Akatsuki (Fukuhara et al., 2011). TIR takes images of thermal infrared emission in 8 to 12 mu m with a field of view of 16 x 12 degrees and a spatial resolution of 0.05 degrees per pixel. TIR covers the temperature range from 150 to 460 K, including the well calibrated range from 230 to 420 K. Temperature accuracy is within 2 K or better for summed images, and the relative accuracy or noise equivalent temperature difference (NETD) at each of pixels is 0.4 K or lower for the well-calibrated temperature range. TIR takes a couple of images with shutter open and closed, the corresponding dark frame, and provides a true thermal image by dark frame subtraction. Data processing involves summation of multiple images, image processing including the StarPixel compression (Hihara et al., 2014), and transfer to the data recorder in the spacecraft digital electronics (DE). We report the scientific and mission objectives of TIR, the requirements and constraints for the instrument specifications, the designed instrumentation and the pre-flight and in-flight performances of TIR, as well as its observation plan during the Hayabusa2 mission.
  • Hiroshi Naraoka, Dan Aoki, Kazuhiko Fukushima, Masayuki Uesugi, Motoo Ito, Fumio Kitajima, Hajime Mita, Hikaru Yabuta, Yoshinori Takano, Toru Yada, Yukihiro Ishibashi, Yuzuru Karouji, Takaaki Okada, Masanao Abe
    Earth, Planets and Space 67(1) 67-67 2015年12月  査読有り
    Three carbonaceous category 3 particles (RA-QD02-0180, RB-QD04-0037-01, and RB-QD04-0047-02) returned in the sample catcher from the Hayabusa spacecraft were analyzed by time of flight-secondary ion mass spectrometry (ToF-SIMS) to establish an analytical procedure for determination of their origins. By the different analytical schemes, the three particles gave distinct elemental and molecular ions, in which the organic carbons commonly appear to be associated with nitrogen, silicon, and/or fluorine. The particles could be debris of silicon rubber and fluorinated compounds and are therefore man-made artifacts rather than natural organic matter.
  • Jisun Park, Brent D. Turrin, Gregory F. Herzog, Fara N. Lindsay, Jeremy S. Delaney, Carl C. Swisher, Masayuki Uesugi, Yuzuru Karouji, Toru Yada, Masanao Abe, Tatsuaki Okada, Yukihiro Ishibashi
    METEORITICS & PLANETARY SCIENCE 50(12) 2087-2098 2015年12月  査読有り
    The Hayabusa mission to asteroid 25143, Itokawa, brought back 2000 small particles, which most closely resemble material found in LL4-6 chondrites. We report an Ar-40/Ar-39 age of 1.3 +/- 0.3 Ga for a sample of Itokawa consisting of three grains with a total mass of similar to 2 mu g. This age is lower than the >4.0 Ga ages measured for 75% of LL chondrites but close to one for Y-790964 and its pairs. The flat Ar-40/Ar-39 release spectrum of the sample suggests complete degassing 1.3 Ga ago. Recent solar heating in Itokawa's current orbit does not appear likely to have reset that age. Solar or impact heating 1.3 Ga ago could have done so. If impact heating was responsible, then the 1.3 Ga age sets an upper bound on the time at which the Itokawa rubble pile was assembled and suggests that rubble pile creation was an ongoing process in the inner solar system for at least the first 3 billion years of solar system history.
  • Fumio Kitajima, Masayuki Uesugi, Yuzuru Karouji, Yukihiro Ishibashi, Toru Yada, Hiroshi Naraoka, Masanao Abe, Akio Fujimura, Motoo Ito, Hikaru Yabuta, Hajime Mita, Yoshinori Takano, Tatsuaki Okada
    Earth, Planets and Space 67(1) 2015年2月11日  査読有り
    © 2015 Kitajima et al.; licensee Springer. Three category 3 (organic) particles (RB-QD04-0001, RB-QD04-0047-02, and RA-QD02-0120) and so-called 'white object' found in the sample container have been examined by micro-Raman and infrared (IR) spectroscopy. In addition, several artificial substances that could occur as possible contaminants and chondritic insoluble organic matter (IOM) prepared from the Murchison CM2 chondrite were analyzed. The Raman spectra of the particles show broad G-band and weak D-band. The G-band parameters plot in the disordered region and close to the artifact produced from a Viton glove after laser exposure rather than chondritic IOM. The particles were therefore originally at low maturity level, suggesting that they have not experienced strong heating and are therefore not related to the LL4-6 parent body. The IR spectra are not similar to that of chondritic IOM. Furthermore, the particles cannot be identified as some artificial carbonaceous substances, including the white object, which are the possible contaminants, examined in this investigation. Although it cannot be determined exactly whether the three category 3 particles are extraterrestrial, the limited IR and Raman results in this investigation strongly suggest their terrestrial origin. Although they could not be directly related to the artificial contaminants examined in this investigation, they may yet be reaction products from similar substances that flew on the mission. In particular, RB-QD04-0047-02 shows several infrared spectral absorption bands in common with the 'white object.' This may relate to the degradation of a polyimide/polyamide resin.
  • Fumio Kitajima, Masayuki Uesugi, Yuzuru Karouji, Yukihiro Ishibashi, Toru Yada, Hiroshi Naraoka, Masanao Abe, Akio Fujimura, Motoo Ito, Hikaru Yabuta, Hajime Mita, Yoshinori Takano, Tatsuaki Okada
    EARTH PLANETS AND SPACE 67 2015年2月  査読有り
    Three category 3 (organic) particles (RB-QD04-0001, RB-QD04-0047-02, and RA-QD02-0120) and so-called 'white object' found in the sample container have been examined by micro-Raman and infrared (IR) spectroscopy. In addition, several artificial substances that could occur as possible contaminants and chondritic insoluble organic matter (IOM) prepared from the Murchison CM2 chondrite were analyzed. The Raman spectra of the particles show broad G-band and weak D-band. The G-band parameters plot in the disordered region and close to the artifact produced from a Viton glove after laser exposure rather than chondritic IOM. The particles were therefore originally at low maturity level, suggesting that they have not experienced strong heating and are therefore not related to the LL4-6 parent body. The IR spectra are not similar to that of chondritic IOM. Furthermore, the particles cannot be identified as some artificial carbonaceous substances, including the white object, which are the possible contaminants, examined in this investigation. Although it cannot be determined exactly whether the three category 3 particles are extraterrestrial, the limited IR and Raman results in this investigation strongly suggest their terrestrial origin. Although they could not be directly related to the artificial contaminants examined in this investigation, they may yet be reaction products from similar substances that flew on the mission. In particular, RB-QD04-0047-02 shows several infrared spectral absorption bands in common with the 'white object.' This may relate to the degradation of a polyimide/polyamide resin.
  • H. Miyamoto, J. Haruyama, T. Kobayashi, K. Suzuki, T. Okada, T. Nishibori, A.P. Showman, R. Lorenz, K. Mogi, D. A. Crown, J. A. P. Rodriguez, S. Rokugawa, T. Tokunaga, K. Masumoto
    Geophys. Res. Lett., 32 L21316 2015年  査読有り
  • Hiroki Hihara, Yousuke Takano, Junpei Sano, Kaori Iwase, Satoko Kawakami, Hisashi Otake, Tatsuaki Okada, Ryu Funase, Jun Takada, Tetsuya Masuda
    INFRARED REMOTE SENSING AND INSTRUMENTATION XXIII 9608 2015年  査読有り
    Infrared sensor system is a major concern for inter-planetary missions in order to investigate the nature and the formation processes of planets and asteroids. Since it takes long time for the communication of inter-planetary probes, automatic and autonomous functions are essential for provisioning observation sequence including the setup procedures of peripheral equipment. Robotics technology which has been adopted on HAYABUSA2 asteroid probe provides functions for setting up onboard equipment, sensor signal calibration, and post signal processing. HAYABUSA2 was launched successfully in 2014 for the exploration of C class near-Earth asteroid 162173 (1999JU3). An optical navigation camera with telephoto lens (ONC-T), a thermal-infrared imager (TIR), and a near infrared spectrometer (NIRS3) have been developed for the observation of geology, thermo-physical properties, and organic or hydrated materials on the asteroid. ONC-T and TIR are used for those scientific purposes as well as assessment of landing site selection and safe descent operation onto the asteroid surface for sample acquisition. NIRS3 is used to characterize the mineralogy of the asteroid surface by observing the 3-micron band, where the particular diagnostic absorption features due to hydrated minerals appear.Modifications were required in order to apply robotics technology for the probe due to the difference of operation on satellites from robot operation environment. The major difference is time line consideration, because the standardized robotics operation software development system is based on event driven framework. The consistency between the framework of time line and event driven scheme was established for the automatic and autonomous operation for HAYABUSA2.
  • Ebihara M, Shirai N, Sekimoto S, Nakamura T, Tsuchiyama A, Matsuno J, Matsumoto T, Tanaka M, Abe M, Fujimura A, Ishibashi Y, Karouji Y, Mukai T, Okada T, Uesugi M, Yada T
    Meteoritics and Planetary Science 50(2) 243-254 2015年  査読有り
  • Hikaru Yabuta, Masayuki Uesugi, Hiroshi Naraoka, Motoo Ito, A. L.David Kilcoyne, Scott A. Sandford, Fumio Kitajima, Hajime Mita, Yoshinori Takano, Toru Yada, Yuzuru Karouji, Yukihiro Ishibashi, Tatsuaki Okada, Masanao Abe
    Earth, Planets and Space 66(1) 2014年12月3日  査読有り
    © 2014 Yabuta et al. Analyses with a scanning transmission x-ray microscope (STXM) using x-ray absorption near edge structure (XANES) spectroscopy were applied for the molecular characterization of two kinds of carbonaceous particles of unknown origin, termed category 3, which were collected from the Hayabusa spacecraft sample catcher. Carbon-XANES spectra of the category 3 particles displayed typical spectral patterns of heterogeneous organic macromolecules; peaks corresponding to aromatic/olefinic carbon, heterocyclic nitrogen and/or nitrile, and carboxyl carbon were all detected. Nitrogen-XANES spectra of the particles showed the presence of N-functional groups such as imine, nitrile, aromatic nitrogen, amide, pyrrole, and amine. An oxygen-XANES spectrum of one of the particles showed a ketone group. Differences in carbon- and nitrogen-XANES spectra of the category 3 particles before and after transmission electron microscopic (TEM) observations were observed, which demonstrates that the carbonaceous materials are electron beam sensitive. Calcium-XANES spectroscopy and elemental contrast mapping identified a calcium carbonate grain from one of the category 3 particles. No fluorine-containing molecular species were detected in fluorine-XANES spectra of the particles. The organic macromolecular features of the category 3 particles were distinct from commercial and/or biological 'fresh (non-degraded)' polymers, but the category 3 molecular features could possibly reflect degradation of contaminant polymer materials or polymer materials used on the Hayabusa spacecraft. However, an extraterrestrial origin for these materials cannot currently be ruled out.
  • Masayuki Uesugi, Hiroshi Naraoka, Motoo Ito, Hikaru Yabuta, Fumio Kitajima, Yoshinori Takano, Hajime Mita, Ichiro Ohnishi, Yoko Kebukawa, Toru Yada, Yuzuru Karouji, Yukihiro Ishibashi, Takaaki Okada, Masanao Abe
    Earth, Planets and Space 66(1) 102-102 2014年12月  査読有り
    Preliminary results of the analyses of five carbonaceous materials (particle size of approximately 50 μm) from the Hayabusa spacecraft sample catcher, including their texture, chemistry, and chemical/isotopic compositions, are summarized. The carbonaceous particles underwent sequential analysis using a series of microanalytical instruments located at several research institutes and universities. Collected particles were initially classified into four categories: two categories containing extraterrestrial silicate particles, one category containing metal and quartz particles consistent with contamination from the sample catcher or sample manipulation tools, and a final category containing carbonaceous particles. Analysis of this final category was the main focus of this study. Through examination of the carbonaceous materials, the appropriate analytical processes for sample transportation and handling were optimized to minimize sample damage and terrestrial contamination. Particles were investigated by transmission electron microscopy/scanning transmission electron microscopy, and Ca-carbonate inclusions were found in one particle. In a different particle, a heterogeneous distribution of silicon in a uniform C, N, and O matrix was found. Though further analysis is required for a strict determination of particle origin, the differences in the microstructure and elemental distribution of the carbonaceous particles suggest multiple origins.
  • Noguchi Takaaki, Bridges John C, Hicks Leon J, Gurman Steven J, Kimura Makoto, Hashimoto Takahito, Konno Mitsuru, Bradley John P, Okazaki Ryuji, Uesugi Masayuki, Yada Toru, Karouji Yuzuru, Abe Masanao, Okada Tatsuaki, Mitsunari Takuya, Nakamura Tomoki, Kagi Hiroyuki
    EARTH PLANETS AND SPACE 66(1) 2014年10月  査読有り
  • Motoo Ito, Masayuki Uesugi, Hiroshi Naraoka, Hikaru Yabuta, Fumio Kitajima, Hajime Mita, Yoshinori Takano, Yuzuru Karouji, Toru Yada, Yukihiro Ishibashi, Tatsuaki Okada, Masanao Abe
    Earth, Planets and Space 66(1) 2014年8月13日  査読有り
    © 2014 Ito et al.; licensee Springer. Since isotopic ratios of H, C, and N are sensitive indicators for determining extraterrestrial organics, we have measured these isotopes of Hayabusa category 3 organic samples of RB-QD04-0047-02, RA-QD02-0120, and RB-QD04-0001 with ion imaging using a NanoSIMS ion microprobe. All samples have H, C, and N isotopic compositions that are terrestrial within errors (approximately ±50‰ for H, approximately ±9‰ for C, and approximately ±2‰ for N). None of these samples contain micrometer-sized hot spots with anomalous H, C, and N isotopic compositions, unlike previous isotope data for extraterrestrial organic materials, i.e., insoluble organic matters (IOMs) and nano-globules in chondrites, interplanetary dust particles (IDPs), and cometary dust particles. We, therefore, cannot conclude whether these Hayabusa category 3 samples are terrestrial contaminants or extraterrestrial materials because of the H, C, and N isotopic data. A coordinated study using microanalysis techniques including Fourier transform infrared spectrometry (FT-IR), time-of-flight secondary ion mass spectrometry (ToF-SIMS), NanoSIMS ion microprobe, Raman spectroscopy, X-ray absorption near edge spectroscopy (XANES), and transmission electron microscopy/scanning transmission electron microscopy (TEM/STEM) is required to characterize Hayabusa category 3 samples in more detail for exploring their origin and nature.

MISC

 534
  • Tatsuaki Okada, Satoshi Tanaka, Yuri Shimaki, Naoya Sakatani, Takehiko Arai, Hiroki Senshu, Hirohide Demura, Toru Kouyama, Tomohiko Sekiguchi, Tetsuya Fukuhara
    Europlanet Science Congress 2020 EPSC2020-12 2024年5月2日  招待有り筆頭著者責任著者
    &amp;lt;p&amp;gt;Thermal imaging, or thermography, has revealed the surface physical state of the C-type near-Earth asteroid 162173 Ryugu (Okada et al., 2020). The asteroid is the target body of JAXA Hayabsua2 asteroid sample return mission, and it has been characterized through remote sensing and surface experiments, and will be deeply and accurately investigated by analysis of returned sample. Thermal observations are among such multi-scale observations, providing a new insight into understanding planetary evolution process.&amp;lt;/p&amp;gt; &amp;lt;p&amp;gt;Thermal infrared imager TIR (Okada et al., 2017; 2020) was used to take one-rotation global thermal images of Ryugu at every 6&amp;amp;#176; step, from the home position (20 km altitude) or from the Mid-Altitude (5 km altitude). There were two big surprises contrary to the predictions before arrival at Ryugu: i) flat diurnal temperature profiles compared to the case of non-rough surface, and ii) non-cold spots identified for most of boulders. The flat diurnal temperature profiles and its maximum temperature in a day indicate that Ryugu must have very rough surfaces made of highly porous materials, derived from the thermal inertia of 300 &amp;amp;#177; 100 J K&amp;lt;sup&amp;gt;-1&amp;lt;/sup&amp;gt;s&amp;lt;sup&amp;gt;-0.5&amp;lt;/sup&amp;gt;m&amp;lt;sup&amp;gt;-2&amp;lt;/sup&amp;gt; (hereafter, tiu). Non-cold boulders indicate that boulders are less consolidated or compacted than typical carbonaceous chondrite meteorites, and shows the same thermophysical properties as the surroundings. TIR was also used to take close-up thermal images during the descent operations, and to have proven that the surface of asteroid is covered with fragments of porous rocks, larger than several centimeters in diameter. The typical size of fragments larger than thermal skin depth (~35 mm) results in similar thermal properties between the boulders and their surroundings. We also consider the surface roughness effect (Shimaki et al., 2020) to obtain the maps of thermal inertia ( 225 &amp;amp;#177; 45 tiu) and the roughness (0.41 &amp;amp;#177; 0.05) at the same time, corresponding to very rough surfaces made of highly-porous materials. This thermal inertia is basically consistent with the value (282 +93/-35 tiu) by in situ measurement using a thermal radiometer MARA on MASCOT lander (Grott et al., 2019). Furthermore, in the close-up thermal images, there were found boulders colder by 20 &amp;amp;#176;C or more, indicating the thermal inertia of typical carbonaceous chondrite meteorites.&amp;lt;/p&amp;gt; &amp;lt;p&amp;gt;Considering these results, we proposed a formation scenario of Ryugu: fluffy cosmic dusts gathered to form porous planetesimals, and then much larger sized but still porous bodies. A low degree of consolidation and alteration has occurred at most of the body, while a higher degree of consolidation or alteration proceeded at the deep interior. Huge meteoritic impacts destroyed and fragmented the bodies, and part of those fragments were re-accreted to form the next generation, rubble-pile bodies (asteroids). Boulders found on Ryugu might have originated from the deep interior of parent bodies, so that most of them are very porous and less consolidated but some of them are relatively dense materials similar to carbonaceous chondrites, which might have originated from the interior. Due to YORP effect, the rotation rate decreased to current one, and the current shape of a spinning top-shape were formed. Analysis of returned sample will make progress in our knowledge of the planetary formation process.&amp;lt;/p&amp;gt;
  • B. E. Clark, A. Sen, X. D. Zou, D. N. DellaGiustina, S. Sugita, N. Sakatani, M. Thompson, D. Trang, E. Tatsumi, M. A. Barucci, M. Barker, H. Campins, T. Morota, C. Lantz, A. R. Hendrix, F. Vilas, L. Keller, V. E. Hamilton, K. Kitazato, S. Sasaki, M. Matsuoka, T. Nakamura, A. Praet, S. M. Ferrone, T. Hiroi, H. H. Kaplan, W. F. Bottke, J. Y. Li, L. Le Corre, J. L. Molaro, R. L. Ballouz, C. W. Hergenrother, B. Rizk, K. N. Burke, C. A. Bennett, D. R. Golish, E. S. Howell, K. Becker, A. J. Ryan, J. P. Emery, S. Fornasier, A. A. Simon, D. C. Reuter, L. F. Lim, G. Poggiali, P. Michel, M. Delbo, O. S. Barnouin, E. R. Jawin, M. Pajola, L. Riu, T. Okada, J. D.P. Deshapriya, J. R. Brucato, R. P. Binzel, D. S. Lauretta
    Icarus 400 2023年8月  
    This paper summarizes the evidence for the optical effects of space weathering, as well as the properties of the surface that control optical changes, on asteroid (101955) Bennu. First, we set the stage by briefly reviewing what was known about space weathering of low-albedo materials from telescopic surveys, laboratory simulations, and sample return analysis. We then look at the evidence for the nature of space weathering on Bennu from recent spacecraft imaging and spectroscopy observations, including the visible to near-infrared and thermal infrared wavelengths, followed by other measurements such as normal albedo measurements from LIDAR scans. We synthesize these different lines of evidence in an effort to describe a general model of space weathering processes and resulting color effects on dark C-complex asteroids, with hypotheses that can be tested by analyzing samples returned by the mission. A working hypothesis that synthesizes findings thus far is that the optical effects of maturation in the space environment depend on the level of hydration of the silicate/phyllosilicate substrate. Subsequent variations in color depend on surface processes and exposure age. On strongly hydrated Bennu, in color imaging data, very young craters are darker and redder than their surroundings (more positive spectral slope in the wavelength range 0.4–0.7μm) as a result of their smaller particle sizes and/or fresh exposures of organics by impacts. Solar wind, dehydration, or migration of fines may cause intermediate-age surfaces to appear bluer than the very young craters. Exposed surfaces evolve toward Bennu's moderately blue global average spectral slope. However, in spectroscopic and LIDAR data, the equator, the oldest surface on Bennu, is darker and redder (wavelength range 0.55–2.0μm) than average and has shallower absorption bands, possibly due to dehydration and/or nanophase and/or microphase opaque production. Bennu is a rubble pile with an active surface, making age relationships, which are critical for determining space weathering signals, difficult to locate and quantify. Hence, the full story ultimately awaits analyses of the Bennu samples that will soon be delivered to Earth.
  • 岡田達明, Hera チーム
    2022 年度プラネタリーディフェンス・シンポジウム 1-4 2023年2月  招待有り
  • 黒川宏之, 嶌生有理, 岡田達明, 佐伯孝尚, 津田雄一, 森治, 坂谷尚哉, 深井稜汰, 青木順, 癸生川陽子, 熊本篤志, 田中智, 川村太一, 浦川聖太郎, 巽瑛理, 高尾勇輝, 菊地翔太, 瀧川晶, 奥住聡, 古家健次, 金丸仁明, 荒川創太
    日本惑星科学会秋季講演会予稿集(Web) 2023 2023年  
  • 佐伯孝尚, 津田雄一, 森治, 高尾勇輝, 菊地翔太, 黒川宏之, 岡田達明, 嶌生有理, 深井稜汰, 坂谷尚哉, 田中智
    日本惑星科学会秋季講演会予稿集(Web) 2023 2023年  

講演・口頭発表等

 523
  • 岡田達明, Hera チーム
    2022 年度プラネタリーディフェンス・シンポジウム 2023年2月  招待有り
  • 岡田達明, 田中智, 嶌生有理, 坂谷尚哉, 荒井武彦, 千秋博紀, 出村裕英, 関口朋彦, 金丸仁明, 石崎拓也, 神山徹, 和田武彦, 竹内央, 山本幸生, 荒川政彦, 中村昭子, 杉田精司, 宮本英昭, 吉川真, 阿部新助, 安部正真, 池永敏憲, 浦川聖太郎, 菊地翔太, 北里宏平, 小松吾郎, 佐々木晶, 巽瑛理, 津田雄一, 野口高明, 三桝裕也, 薮田ひかる, 渡邊誠一郎, 斎藤啓仁, 金野龍史, 李正林, 古川聡一朗, Hera-JP, TIRIチーム
    第23回宇宙科学シンポジウム 2023年1月
  • 坂谷尚哉, 岡田達明, 千秋博紀, 荒井武彦, 出村裕英, 嶌生有理, 関口朋彦, 石崎拓也, 金丸仁明, 神山徹, 田中智
    第23回宇宙科学シンポジウム 2023年1月
  • 嶌生有理, 黒川宏之, 坂谷尚哉, 深井稜汰, 癸生川陽子, 青木順, 巽瑛理, 田中智, 渡邊誠一郎, 岡田達明, 浦川聖太郎, 脇田茂, 薮田ひかる, 兵頭龍樹, 藤谷渉, 牛久保孝行, 奥住聡
    第23回宇宙科学シンポジウム 2023年1月
  • 吉川真, 柳沢俊史, 安部正真, 池永敏憲, 岩城陽大, 岡田達明, 菊地耕一, 黒崎裕久, 黒田信介, 佐伯孝尚, 嶌生有理, 津田雄一, 西山和孝, 三桝裕也, 浦川聖太郎, 奥村真一郎
    第23回宇宙科学シンポジウム 2023年1月

担当経験のある科目(授業)

 2

共同研究・競争的資金等の研究課題

 6

● 専任大学名

 1
  • 専任大学名
    東京大学(University of Tokyo)

● 所属する所内委員会

 1
  • 所内委員会名
    放射線安全委員会