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. Noguchi, M. Kimura, T. Hashimoto, M. Konno, T. Nakamura, M. E. Zolensky, A. Tsuchiyama, T. Matsumoto, J. Matsuno, R. Okazaki, M. Uesugi, Y. Karouji, T. Yada, Y. Ishibashi, K. Shirai, M. Abe, T. Okada
    Meteoritics and Planetary Science 49(7) 1305-1314 2014年7月  査読有り
    We observed cross sectional ultra-thin sections near the surface of 12 particles recovered from the S-type asteroid Itokawa by the Hayabusa spacecraft in 2010, using spherical aberration-corrected STEM and conventional TEM. Although their mineralogy is almost identical to the equilibrated LL chondrites and therefore basically anhydrous, micrometer-to-submicrometer-sized sylvite was identified on the surface of Itokawa particle RA-QD02-0034. Separately, micrometer-sized halite was also identified on the surface of Itokawa particle RA-QD02-0129. Detailed inspection of the sample processing procedures at the JAXA's Planetary Materials Sample Curation Facility and textural observation of the sylvite and halite indicate that they were clearly present on two Itokawa particles before they were removed from Clean Chamber #2 at JAXA. However, there is no direct evidence for their extraterrestrial origin at present. If the sylvite and halite are extraterrestrial, their presence suggests that they may be more abundant on the surface of S-type asteroids than previously thought. © The Meteoritical Society, 2014.
  • Masayuki Uesugi, Ryo Noguchi, Tooru Matsumoto, Junya Matsuno, Takashi Nagano, Akira Tsuchiyama, Shigenori Harada, Kaori Yokoyama, Yoshiaki Yodo, Noboru Takeda, Toru Yada, Shogo Yakame, Yuzuru Karouji, Yukihiro Ishibashi, Masanao Abe, Tatsuaki Okada, Akio Fujimura, Mitsuru Ebihara, Fumio Kitajima, Keisuke Nagao, Tomoki Nakamura, Hiroshi Naraoka, Takaaki Noguchi, Ryuji Okazaki, Hisayoshi Yurimoto
    METEORITICS & PLANETARY SCIENCE 49(7) 1186-1201 2014年7月  査読有り
    We report the investigation of cutting methods for Hayabusa samples. The purpose of our study is to explore the possibility of applying multiple analyses to a single particle effectively. We investigated the cutting performance of a blade dicing saw, laser, focused ion beam (FIB), and physical breaking by microindenter. Cutting performance was examined by estimating the aspect ratio of the cut slit, i.e., depth over width of the slit. We also investigated the possible contamination and sample damage by cutting. The result of the investigation shows that we can cut the samples from <50 mu m to 500 mu m using those methods with aspect ratios from 10 to 20, although they would introduce some contamination or damage to the samples. Our investigations also provide an important basis for the analysis of samples obtained by future sample return missions.
  • Hiroki Hihara, Kaori Iwase, Junpei Sano, Hisashi Otake, Tatsuaki Okada, Ryu Funase, Ryoichi Kashikawa, Isamu Higashino, Tetsuya Masuda
    JOURNAL OF APPLIED REMOTE SENSING 8(1) 084987 2014年4月  査読有り
    A thermal-infrared (TIR) imager system is developed for HAYABUSA2, which is planned to be launched in 2014 and aims at sample-return from a C-class near-Earth asteroid 162173 (1999JU3) considered to contain organic or hydrated materials. The system consists of a TIR imager and digital electronics, which are used not only for the scientific investigation of physical properties of the asteroid surface, but also for the assessment of landing site selection and safe descent operation onto the asteroid surface with in situ measurement. TIR adopts an uncooled bolometer. Image operations such as multiple images summation, dark image subtraction, and the compensation of dead pixels are processed onboard. A processing module is connected to sensor interfaces through SpaceWire in order to provide deterministic processing time. Data compression is also provided to reduce the restriction of transmission time, which provides the equivalent compression ratio as JPEG2000 in 1/30 processing time in average. A high-speed data recorder is connected through SpaceWire in order to record TIR data in parallel with other sensor data. The modularity of SpaceWire enables us to use these as built devices for TIR and inherits the same design as the long-wavelength infrared imager developed for the Venus climate orbiter Akatsuki. (C) 2014 Society of Photo-Optical Instrumentation Engineers (SPIE)
  • Takaaki Noguchi, Makoto Kimura, Takahito Hashimoto, Mitsuru Konno, Tomoki Nakamura, Michael E. Zolensky, Ryuji Okazaki, Masahiko Tanaka, Akira Tsuchiyama, Aiko Nakato, Toshinori Ogami, Hatsumi Ishida, Ryosuke Sagae, Shinichi Tsujimoto, Toru Matsumoto, Junya Matsuno, Akio Fujimura, Masanao Abe, Toru Yada, Toshifumi Mukai, Munetaka Ueno, Tatsuaki Okada, Kei Shirai, Yukihiro Ishibashi
    METEORITICS & PLANETARY SCIENCE 49(2) 188-214 2014年2月  査読有り
    On the basis of observations using Cs-corrected STEM, we identified three types of surface modification probably formed by space weathering on the surfaces of Itokawa particles. They are (1) redeposition rims (2-3nm), (2) composite rims (30-60nm), and (3) composite vesicular rims (60-80nm). These rims are characterized by a combination of three zones. Zone I occupies the outermost part of the surface modification, which contains elements that are not included in the unchanged substrate minerals, suggesting that this zone is composed of sputter deposits and/or impact vapor deposits originating from the surrounding minerals. Redeposition rims are composed only of Zone I and directly attaches to the unchanged minerals (Zone III). Zone I of composite and composite vesicular rims often contains nanophase (Fe,Mg)S. The composite rims and the composite vesicular rims have a two-layered structure: a combination of Zone I and Zone II, below which Zone III exists. Zone II is the partially amorphized zone. Zone II of ferromagnesian silicates contains abundant nanophase Fe. Radiation-induced segregation and in situ reduction are the most plausible mechanisms to form nanophase Fe in Zone II. Their lattice fringes indicate that they contain metallic iron, which probably causes the reddening of the reflectance spectra of Itokawa. Zone II of the composite vesicular rims contains vesicles. The vesicles in Zone II were probably formed by segregation of solar wind He implanted in this zone. The textures strongly suggest that solar wind irradiation damage and implantation are the major causes of surface modification and space weathering on Itokawa.
  • Tomoki Nakamura, Aiko Nakato, Hatsumi Ishida, Shigeru Wakita, Takaaki Noguchi, Michael E. Zolensky, Masahiko Tanaka, Makoto Kimura, Akira Tshuchiyama, Toshihiro Ogami, Takahito Hashimoto, Mitsuru Konno, Masayuki Uesugi, Toru Yada, Kei Shirai, Akio Fujimura, Ryuji Okazaki, Scott. A. Sandford, Yukihiro Ishibashi, Masanao Abe, Tatsuaki Okada, Munetaka Ueno, Junichiro Kawaguchi
    METEORITICS & PLANETARY SCIENCE 49(2) 215-227 2014年2月  査読有り
    The mineralogy and mineral chemistry of Itokawa dust particles captured during the first and second touchdowns on the MUSES-C Regio were characterized by synchrotron-radiation X-ray diffraction and field-emission electron microprobe analysis. Olivine and low- and high-Ca pyroxene, plagioclase, and merrillite compositions of the first-touchdown particles are similar to those of the second-touchdown particles. The two touchdown sites are separated by approximately 100 meters and therefore the similarity suggests that MUSES-C Regio is covered with dust particles of uniform mineral chemistry of LL chondrites. Quantitative compositional properties of 48 dust particles, including both first- and second-touchdown samples, indicate that dust particles of MUSES-C Regio have experienced prolonged thermal metamorphism, but they are not fully equilibrated in terms of chemical composition. This suggests that MUSES-C particles were heated in a single asteroid at different temperatures. During slow cooling from a peak temperature of approximately 800 degrees C, chemical compositions of plagioclase and K-feldspar seem to have been modified: Ab and Or contents changed during cooling, but An did not. This compositional modification is reproduced by a numerical simulation that modeled the cooling process of a 50 km sized Itokawa parent asteroid. After cooling, some particles have been heavily impacted and heated, which resulted in heterogeneous distributions of Na and K within plagioclase crystals. Impact-induced chemical modification of plagioclase was verified by a comparison to a shock vein in the Kilabo LL6 ordinary chondrite where Na-K distributions of plagioclase have been disturbed.
  • Toru Yada, Akio Fujimura, Masanao Abe, Tomoki Nakamura, Takaaki Noguchi, Ryuji Okazaki, Keisuke Nagao, Yukihiro Ishibashi, Kei Shirai, Michael E. Zolensky, Scott Sandford, Tatsuaki Okada, Masayuki Uesugi, Yuzuru Karouji, Maho Ogawa, Shogo Yakame, Munetaka Ueno, Toshifumi Mukai, Makoto Yoshikawa, Junichiro Kawaguchi
    METEORITICS & PLANETARY SCIENCE 49(2) 135-153 2014年2月  査読有り
    The Planetary Material Sample Curation Facility of JAXA (PMSCF/JAXA) was established in Sagamihara, Kanagawa, Japan, to curate planetary material samples returned from space in conditions of minimum terrestrial contaminants. The performances for the curation of Hayabusa-returned samples had been checked with a series of comprehensive tests and rehearsals. After the Hayabusa spacecraft had accomplished a round-trip flight to asteroid 25143 Itokawa and returned its reentry capsule to the Earth in June 2010, the reentry capsule was brought back to the PMSCF/JAXA and was put to a series of processes to extract recovered samples from Itokawa. The particles recovered from the sample catcher were analyzed by electron microscope, given their ID, grouped into four categories, and preserved in dimples on quartz slide glasses. Some fraction of them has been distributed for initial analyses at NASA, and will be distributed for international announcement of opportunity (AO), but a certain fraction of them will be preserved in vacuum for future analyses.
  • Masahiko Tanaka, Tomoki Nakamura, Takaaki Noguchi, Aiko Nakato, Hatsumi Ishida, Toru Yada, Kei Shirai, Akio Fujimura, Yukihiro Ishibashi, Masanao Abe, Tatsuaki Okada, Munetaka Ueno, Toshifumi Mukai
    METEORITICS & PLANETARY SCIENCE 49(2) 237-244 2014年2月  査読有り
    The crystallization temperatures of Itokawa surface particles recovered by the space probe Hayabusa were estimated by a plagioclase geothermometer using sodic plagioclase triclinicity. The Delta 131- index required for the thermometer, which is the difference in X- ray diffraction peak positions between the 131 and 131 reflections of plagioclase, was obtained by a high- resolution synchrotron Gandolfi camera developed for the third generation synchrotron radiation beamline, BL15XU at SPring- 8. Crystallization temperatures were successfully determined from the Delta 131- indices for four particles. The observed plagioclase crystallization temperatures were in a range from 655 to 660 degrees C. The temperatures indicate crystallization temperatures of plagioclases in the process of prograde metamorphism before the peak metamorphic stage.
  • Katsushi Furutani, Ryota Inukai, Takayoshi Takano, Tatsuaki Okada, Kazuto Saiki, Hiroyuki Ohue
    Proceedings - ASPE 2014 Annual Meeting 508-511 2014年  査読有り
  • Katsushi Furutani, Eiji Ikeda, Tatsuaki Okada, Kazuto Saiki, Hiroyuki Ohue
    ADVANCES IN MATERIALS AND PROCESSING TECHNOLOGIES XV 773-774 392-+ 2014年  査読有り
    This paper describes design of a prototype of a wire-sawing machine and some machining demonstrations. Slicing the rock samples is preferable to observe their interior for in-situ analysis in lunar and planetary explorations. The requirements for the wire-sawing machine were clarified as follows: using a long saw wire to extend the duty cycle, and winding and unwinding the saw wire with two reels. After building a prototype of the wire-sawing machine, the cutting performance in vacuum was compared with that in air. The cutting depth in vacuum leveled off and was smaller than that in air.
  • S. Tachibana, M. Abe, M. Arakawa, M. Fujimoto, Y. Iijima, M. Ishiguro, K. Kitazato, N. Kobayashi, N. Namiki, T. Okada, R. Okazaki, H. Sawada, S. Sugita, Y. Takano, S. Tanaka, S. Watanabe, M. Yoshikawa, H. Kuninaka
    Geochemical Journal 48(6) 571-581 2014年  査読有り
    Copyright © 2014 by The Geochemical Society of Japan. Hayabusa2 is an asteroid exploration mission to return surface samples of a near-Earth C-type asteroid (162173) 1999 JU3. Because asteroids are the evolved remnants of planetesimals that were the building blocks of planets, detailed observation by a spacecraft and analysis of the returned samples will provide direct evidence regarding planet formation and the dynamic evolution of the solar system. Moreover, C-type asteroids are expected to preserve the most pristine materials in the solar system, a mixture of minerals, ice, and organic matter that interact with each other. Space missions are the only way to obtain such pristine materials with geologic context and without terrestrial contamination. Hayabusa2 will launch off in 2014, arrive at 1999 JU3 in mid-2018, and fully investigate and sample the asteroid at three different locations during its 18-month stay. The concept and design of the Hayabusa2 sampler are basically the same as that on-board Hayabusa, and impact sampling with a 5-g Ta bullet will be made at three locations of the asteroid. The sample container has three separate chambers inside to store samples obtained at different locations separately. The spacecraft will return to Earth with samples in December 2020. Returned samples will be investigated by state-of-the-art analytical techniques in 2020 to understand the evolutionary history of the solar system from 4.56 Gyr ago to the present by combining results from laboratory examinations of the returned samples with remote-sensing datasets and comparing all results of observations of meteorites, interplanetary dust particles, and future returned samples.
  • Hisashi Otake, Tatsuaki Okada, Ryu Funase, Hiroki Hihara, Junpei Sano, Kaori Iwase, Satoko Kawakami, Jun Takada, Tetsuya Masuda
    INFRARED REMOTE SENSING AND INSTRUMENTATION XXII 9219 2014年  査読有り
    Onboard signal processing system for infrared sensors has been developed for HAYABUSA2 for the exploration of C class near-Earth asteroid 162173 (1999JU3), which is planned to be launched in 2014. 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.Since the processing cycle of these sensors are independent, data processing, formatting and recording are processed in parallel. In order to provide the functions within the resource limitation of deep space mission, automatic packet routing function is realized in one chip router with SpaceWire standard. Thanks to the SpaceWire upper layer protocol (remote memory access protocol: RMAP), the variable length file system operation function can be delegated to the data recorder from the CPU module of the digital electronics of the sensor system. In consequence the infrared spectrometer data from NIRS3 is recorded in parallel with the infrared image sensors. High speed image compression algorithm is also developed for both lossless and lossy image compression in order to eliminate additional hardware resource while maintaining the JPEG2000 equivalent image quality.
  • 唐牛譲, 石橋之宏, 上椙真之, 矢田達, 中藤亜衣子, 熊谷和也, 岡田達明, 安部正真
    地球化学 48(4) 211-220 2014年  査読有り
    The Extraterrestrial Sample Curation Center of JAXA curates the Hayabusa-returned samples in conditions of minimum terrestrial contaminants, because these samples are very tiny. We evaluated the cleanliness of the handling instruments, the cleanroom environments and the sample storage chamber to improve the cleanliness of particles, organic molecules and metallic elements to a level not to affect the analyses of the Hayabusa-returned samples. In the environment of the clean chamber No. 2 where the samples have been stored, the organic molecule abundance was lower than the detection limit, furthermore, metallic elemental concentrations were the lowest among other evaluated place. A multi-stage ultrasonic cleaning by organic solvents and the ultrapure water have been applied to instruments made of stainless steel and/or aluminum alloy, and additionally, acid-alkali liquids cleaning have been performed for those made of quartz glasses. For the cleanliness of quartz glasses after the cleaning, the organic molecules abundances were blank level, and the metallic element concentrations were 1~100×109atom/cm2/24 h. It was confirmed by optical microscope that no particle of size more than 10 μm was observed on quartz glasses after the cleaning.
  • Masayuki Uesugi, Yuzuru Karouji, Toru Yada, Yukihiro Ishibashi, Tatsuaki Okada, Masanao Abe
    METEORITICS & PLANETARY SCIENCE 48 A351-A351 2013年7月  査読有り
  • Yuzuru Karouji, Masayuki Uesugi, Toru Yada, Yukihiro Ishibashi, Tatsuaki Okada, Masanao Abe
    METEORITICS & PLANETARY SCIENCE 48 A387-A387 2013年7月  査読有り
  • H. Naraoka, H. Mita, K. Hamase, M. Mita, H. Yabuta, K. Saito, K. Fukushima, F. Kitajima, S. A. Sandford, T. Nakamura, T. Noguchi, R. Okazaki, K. Nagao, M. Ebihara, H. Yurimoto, A. Tsuchiyama, M. Abe, K. Shirai, M. Ueno, T. Yada, Y. Ishibashi, T. Okada, A. Fujimura, T. Mukai, M. Yoshikawa, J. Kawaguchi
    Geochemical Journal 46(1) 61-72 2012年  査読有り
    Microparticles recovered from the Asteroid 25143 Itokawa surface by the Hayabusa mission have been examined for the occurrence of soluble organic compounds. After five individual particles (∼50 to 100 μm in diameter) were rinsed with organic solvents on a diamond plate, two extracts were hydrolyzed with hydrochloric acid for amino acid analysis (AAA), and three extracts were combined for time of flight-secondary ion mass spectrometry (ToF-SIMS) to look for other organic compounds, including polycyclic aromatic hydrocarbons. The organic compounds detected by both methods have the same concentrations as those in blank levels, indicating that indigenous organic compounds are not found in this study. Based on the sensitivities of AAA and ToF-SIMS with the reference sample analyses, the concentrations of indigenous organics in the samples are below part-per-million (ppm), if present. Copyright © 2012 by The Geochemical Society of Japan.
  • Katsushi Furutani, Tatsuaki Okada
    Proceedings of Inernational Symposium on Artificial Intelligence, Robotics and Automation in Space 18 1-8 2012年  査読有り
  • K. Furutani, E. Kagami, M. Ohtake, C. Honda, M. Ohtsuki, T. Kubota, T. Okada
    Proceedings of the 12th International Conference of the European Society for Precision Engineering and Nanotechnology, EUSPEN 2012 2 481-484 2012年  査読有り
    For in-situ analysis in future lunar, planetary or asteroid explorations, a rock surface should be smoothed. In this paper, a surface shaver with a piezoelectric actuator is proposed and its machining performance is investigated. Shaving teeth are mounted at the ends of a lever mechanism. The surface roughness of basalt was small with an increase of the pressing force. However, the removal amount was smaller with an increase of the pressing force further.
  • Katsushi Furutani, Eiji Ikeda, Tatsuaki Okada, Kazuto Saiki, Hiroyuki Ohue
    Proceedings of 15th International Conference on Advances in Materials and Processing Technologies 11151 1-6 2012年  査読有り
  • S. Z. Weider, B. J. Kellett, B. M. Swinyard, I. A. Crawford, K. H. Joy, M. Grande, C. J. Howe, J. Huovelin, S. Narendranath, L. Alha, M. Anand, P. S. Athiray, N. Bhandari, J. A. Carter, A. C. Cook, L. C. Duston, V. A. Fernandes, O. Gasnault, J. N. Goswami, J. P.D. Gow, A. D. Holland, D. Koschny, D. J. Lawrence, B. J. Maddison, S. Maurice, D. J. McKay, T. Okada, C. Pieters, D. A. Rothery, S. S. Russell, A. Shrivastava, D. R. Smith, M. Wieczorek
    Planetary and Space Science 60(1) 217-228 2012年1月  査読有り
    We present X-ray fluorescence observations of the lunar surface, made by the Chandrayaan-1 X-ray Spectrometer during two solar flare events early in the mission (12th December 2008 and 10th January 2009). Modelling of the X-ray spectra with an abundance algorithm allows quantitative estimates of the MgO/SiO 2 and Al 2O 3/SiO 2 ratios to be made for the two regions, which are in mainly basaltic areas of the lunar nearside. One of these ground tracks includes the Apollo 14 landing site on the Fra Mauro Formation. Within the 1σ errors provided, the results are inside the range of basaltic samples from the Apollo and Luna collections. The Apollo 14 soil composition is in agreement with the results from the January flare at the 1σ uncertainty level. Discrepancies are observed between our results and compositions derived for the same areas by the Lunar Prospector gamma-ray spectrometer; some possible reasons for this are discussed. © 2011 Elsevier Ltd. All rights reserved.
  • 岡田達明
    ぶんせき (10) 554-557 2012年  査読有り筆頭著者責任著者
  • 並木則行, 小松吾郎, 臼井寛裕, 杉田精司, 宮本英昭, 久保田孝, 石上玄也, 出村裕英, 岡田達明, 三浦弥生, 長勇一郎, 後藤和久, 千秋博紀, 和田浩二, 石橋高, 荒井朋子, 小林正規, 大野宗祐
    地質学雑誌 118(10) 606-617 2012年  査読有り
    将来火星着陸探査計画として,われわれは探査車(ローバ)による地質調査を提案している.米国,ロシア(旧ソ連),欧州による軌道上からの,あるいは複数の着陸点での観測から,火星は非常に多様性に富む天体であり,複雑な物理・化学過程が表層の地質に影響を与え続けてきたことが明らかとなっている.ローバを使った化学組成分析や同位体測定では火星隕石の収集とは異なり,地質現象の時間的変遷を追うことが出来るので,複雑性を解明することに役立つ.観察対象は堆積岩と火山岩に大別され,それぞれ異なる科学目標を有する.堆積岩調査は米欧の火星探査の流れに沿う方向であり,国際協調による科学成果の向上が期待できる.一方,火山岩調査は日本の独自性の高い選択である.現段階ではいずれの方向を選択すべきか決まっていないが,堆積岩調査にせよ火山岩調査にせよ,大型プロジェクトとして広範な地球科学者の評価と支持を得ることが必要である.
  • T. Noguchi, T. Nakamura, M. Kimura, M. E. Zolensky, M. Tanaka, T. Hashimoto, M. Konno, A. Nakato, T. Ogami, A. Fujimura, M. Abe, T. Yada, T. Mukai, M. Ueno, T. Okada, K. Shirai, Y. Ishibashi, R. Okazaki
    Science 333(6046) 1121-1125 2011年8月26日  査読有り
    The reflectance spectra of the most abundant meteorites, ordinary chondrites, are different from those of the abundant S-type (mnemonic for siliceous) asteroids. This discrepancy has been thought to be due to space weathering, which is an alteration of the surfaces of airless bodies exposed to the space environment. Here we report evidence of space weathering on particles returned from the S-type asteroid 25143 Itokawa by the Hayabusa spacecraft. Surface modification was found in 5 out of 10 particles, which varies depending on mineral species. Sulfur-bearing Fe-rich nanoparticles exist in a thin (5 to 15 nanometers) surface layer on olivine, low-Ca pyroxene, and plagioclase, which is suggestive of vapor deposition. Sulfur-free Fe-rich nanoparticles exist deeper inside (<60 nanometers) ferromagnesian silicates. Their texture suggests formation by metamictization and in situ reduction of Fe 2+.
  • Jun Kimura, Taichi Kawamura, Hisataka Morito, Tomokatsu Morota, Chikatoshi Honda, Kiyoshi Kuramoto, Tatsuaki Okada
    ICARUS 214(2) 596-605 2011年8月  査読有り最終著者
    Iapetus, one of the saturnian moons, has an extreme albedo contrast between the leading and trailing hemispheres. The origin of this albedo dichotomy has led to several hypotheses, however it remains controversial. To clarify the origin of the dichotomy, the key approach is to investigate the detailed distribution of the dark material. Recent studies of impact craters and surface temperature from Cassini spacecraft data implied that sublimation of H(2)O ice can occur on Iapetus' surface. This ice sublimation can change the albedo distribution on the moon with time.In this study, we evaluate the effect of ice sublimation and simulate the temporal change of surface albedo. We assume the dark material and the bright ice on the surface to be uniformly mixed with a certain volume fraction, and the initial albedo distribution to incorporate the dark material deposits on the surface. That is, the albedo at the apex is lowest and concentrically increases in a sinusoidal pattern. This situation simulates that dark materials existed around the Iapetus' orbit billions of years ago, and the synchronously rotating Iapetus swept the material and then deposited it on its surface. The evolution of the surface albedo during 4.0 Gyr is simulated by estimating the surface temperature from the insolation energy on Iapetus including the effect of Saturn's eccentricity and Iapetus' obliquity precession, and evaluating the sublimation rate of H(2)O ice from the Iapetus' surface.As a result, we found that the distribution of the surface albedo changed dramatically after 4.0 Gyr of evolution. The sublimation has three important effects on the resultant surface albedo. First, the albedo in the leading hemisphere has significantly decreased to approach the minimum value. Second, the albedo distribution has been elongated along the equator. Third, the edge of the low albedo region has become clear. Considering the effect of ice sublimation, the current albedo distribution can be reconstructed from the sinusoidal albedo distribution, suggesting the apex-antapex cratering asymmetry as a candidate for the origin of the albedo dichotomy. From the model analysis, we obtained an important aspect that the depth of the turn-over layer where the darkening process proceeded for 4 Gyr should be an order of 10 cm, which is consistent with evaluation from the Cassini radar observations. (C) 2011 Elsevier Inc. All rights reserved.
  • F. Kitajima, M. Kotsugi, T. Ohkochi, H. Naraoka, Y. Ishibashi, M. Abe, A. Fujimura, R. Okazaki, T. Yada, T. Nakamura, T. Noguchi, K. Nagao, A. Tsuchiyama, H. Yurimoto, M. Ebihara, T. Mukai, S. A. Sandford, T. Okada, K. Shirai, M. Ueno, M. Yoshikawa, J. Kawaguchi
    METEORITICS & PLANETARY SCIENCE 46 A126-A126 2011年7月  査読有り
  • S. Narendranath, P.S. Athiray, P. Sreekumar, B.J. Kellett, L. Alha, C.J. Howe, K.H. Joy, M. Grande, J. Huovelin, I.A. Crawford, U. Unnikrishnan, S. Lalita, S. Subramaniam, S.Z. Weider, L.R. Nittler, O. Gasnault, D. Rothery, V.A. Fernandes, N. Bhandari, J.N. Goswami, M.A. Wieczorek
    Icarus 214(1) 53-66 2011年7月  査読有り
  • Tatsuaki Okada, Manuel Grande, Juergen Oberst, Sho Sasaki
    EARTH PLANETS AND SPACE 63(1) 3-3 2011年  査読有り筆頭著者責任著者
  • Katsushi Furutani, Shoudai Fukunaga, Tatsuaki Okada, Kazuto Saiki, Hiroyuki Ohue
    Proceedings - ASPE 2011 Annual Meeting 52 349-352 2011年  査読有り
  • 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年  査読有り
  • 佐藤 毅彦, 久保田 孝, 宮本 英昭, 岡田 達明, 松岡 彩子, 今村 剛, 尾川 順子, 川口 淳一郎, MELOSワーキンググループ
    遊・星・人 : 日本惑星科学会誌 18(2) 66-68 2009年6月25日  査読有り
    火星複合探査WGは数多くの議論を通じて,MELOS計画の根幹である科学目標とそれに答えるための科学要求をまとめてきた.火星はなぜ赤いのか?この単純でしかし奥深い問題に答えるには,大気圏・表層・固体圏を一つの惑星システムとして捉える複合探査が必要である.MELOSは,まさにそれを目指そうとしている.
  • 杉田 精司, 宮本 英昭, 橘 省吾, 岡田 達明, 出村 裕英, 大森 聡一, 並木 則行, 高橋 幸弘, 三浦 弥生, 長尾 敬介, 三河内 岳, 佐藤 毅彦
    遊・星・人 : 日本惑星科学会誌 18(2) 79-83 2009年6月25日  査読有り
    我々はこれまでの火星複合探査ワーキンググループの中で,MELOSの着陸機によってどのような火星表層探査を行うべきか,またどのような測定によって実現されるのか議論を行ってきた.本稿では,その議論で見えてきた火星着陸探査による表面探査の科学目標と搭載機器候補について解説する.
  • M. Grande, B. J. Maddison, C. J. Howe, B. J. Kellett, P. Sreekumar, J. Huovelin, I. A. Crawford, C. L. Duston, D. Smith, M. Anand, N. Bhandari, A. Cook, V. Fernandes, B. Foing, O. Gasnaut, J. N. Goswami, A. Holland, K. H. Joy, D. Kochney, D. Lawrence, S. Maurice, T. Okada, S. Narendranath, C. Pieters, D. Rothery, S. S. Russell, A. Shrivastava, B. Swinyard, M. Wilding, M. Wieczorek
    Planetary and Space Science 57(7) 717-724 2009年6月  査読有り
    The Chandrayaan-1 X-ray Spectrometer (C1XS) is a compact X-ray spectrometer for the Indian Space Research Organisation (ISRO) Chandrayaan-1 lunar mission. It exploits heritage from the D-CIXS instrument on ESA's SMART-1 mission. As a result of detailed developments to all aspects of the design, its performance as measured in the laboratory greatly surpasses that of D-CIXS. In comparison with SMART-1, Chandrayaan-1 is a science-oriented rather than a technology mission, leading to far more favourable conditions for science measurements. C1XS is designed to measure absolute and relative abundances of major rock-forming elements (principally Mg, Al, Si, Ca and Fe) in the lunar crust with spatial resolution ≤25 FWHM km, and to achieve relative elemental abundances of better than 10%. © 2009 Elsevier Ltd.
  • I. A. Crawford, K. H. Joy, B. J. Kellett, M. Grande, M. Anand, N. Bhandari, A. C. Cook, L. d'Uston, V. A. Fernandes, O. Gasnault, J. Goswami, C. J. Howe, J. Huovelin, D. Koschny, D. J. Lawrence, B. J. Maddison, S. Maurice, S. Narendranath, C. Pieters, T. Okada, D. A. Rothery, S. S. Russell, P. Sreekumar, B. Swinyard, M. Wieczorek, M. Wilding
    Planetary and Space Science 57(7) 725-734 2009年6月  査読有り
    The UK-built Chandrayaan-1 X-ray Spectrometer (C1XS) will fly as an ESA instrument on India's Chandrayaan-1 mission to the Moon, launched in October 2008. C1XS builds on experience gained with the earlier D-CIXS instrument on SMART-1, but will be a scientifically much more capable instrument. Here we describe the scientific objectives of this instrument, which include mapping the abundances of the major rock-forming elements (principally Mg, Al, Si, Ti, Ca and Fe) in the lunar crust. These data will aid in determining whether regional compositional differences (e.g., the Mg/Fe ratio) are consistent with models of lunar crustal evolution. C1XS data will also permit geochemical studies of smaller scale features, such as the ejecta blankets and central peaks of large impact craters, and individual lava flows and pyroclastic deposits. These objectives all bear on important, and currently unresolved, questions in lunar science, including the structure and evolution of any primordial magma ocean, as revealed by vertical and lateral geochemical variations in the crust, and the composition of the lunar mantle, which will further constrain theories of the Moon's origin, thermal history and internal structure. © 2008 Elsevier Ltd. All rights reserved.
  • Michel Blanc, Yann Alibert, Nicolas Andre, Sushil Atreya, Reta Beebe, Willy Benz, Scott J. Bolton, Angioletta Coradini, Athena Coustenis, Veronique Dehant, Michele Dougherty, Pierre Drossart, Masaki Fujimoto, Olivier Grasset, Leonid Gurvits, Paul Hartogh, Hauke Hussmann, Yasumasa Kasaba, Margaret Kivelson, Krishan Khurana, Norbert Krupp, Philippe Louarn, Jonathan Lunine, Melissa McGrath, David Mimoun, Olivier Mousis, Juergen Oberst, Tatsuaki Okada, Robert Pappalardo, Olga Prieto-Ballesteros, Daniel Prieur, Pascal Regnier, Maarten Roos-Serote, Sho Sasaki, Gerald Schubert, Christophe Sotin, Tom Spilker, Yukihiro Takahashi, Takeshi Takashima, Federico Tosi, Diego Turrini, Tim Van Hoolst, Lev Zelenyi
    EXPERIMENTAL ASTRONOMY 23(3) 849-892 2009年3月  査読有り
    The exploration of the Jovian System and its fascinating satellite Europa is one of the priorities presented in ESA's "Cosmic Vision" strategic document. The Jovian System indeed displays many facets. It is a small planetary system in its own right, built-up out of the mixture of gas and icy material that was present in the external region of the solar nebula. Through a complex history of accretion, internal differentiation and dynamic interaction, a very unique satellite system formed, in which three of the four Galilean satellites are locked in the so-called Laplace resonance. The energy and angular momentum they exchange among themselves and with Jupiter contribute to various degrees to the internal heating sources of the satellites. Unique among these satellites, Europa is believed to shelter an ocean between its geodynamically active icy crust and its silicate mantle, one where the main conditions for habitability may be fulfilled. For this very reason, Europa is one of the best candidates for the search for life in our Solar System. So, is Europa really habitable, representing a "habitable zone" in the Jupiter system? To answer this specific question, we need a dedicated mission to Europa. But to understand in a more generic way the habitability conditions around giant planets, we need to go beyond Europa itself and address two more general questions at the scale of the Jupiter system: to what extent is its possible habitability related to the initial conditions and formation scenario of the Jovian satellites? To what extent is it due to the way the Jupiter system works? ESA's Cosmic Vision programme offers an ideal and timely framework to address these three key questions. Building on the in-depth reconnaissance of the Jupiter System by Galileo (and the Voyager, Ulysses, Cassini and New Horizons fly-by's) and on the anticipated accomplishments of NASA's JUNO mission, it is now time to design and fly a new mission which will focus on these three major questions. LAPLACE, as we propose to call it, will deploy in the Jovian system a triad of orbiting platforms to perform coordinated observations of its main components: Europa, our priority target, the Jovian satellites, Jupiter's magnetosphere and its atmosphere and interior. LAPLACE will consolidate Europe's role and visibility in the exploration of the Solar System and will foster the development of technologies for the exploration of deep space in Europe. Its multi-platform and multi-target architecture, combined with its broadly multidisciplinary scientific dimension, will provide an outstanding opportunity to build a broad international collaboration with all interested nations and space agencies.
  • Tetsuo Yoshimitsu, Shujiro Sawai, Takahide Mizuno, Seisuke Fukuda, Nobutaka Bando, Shin'ichiro Sakai, Ken Higuchi, Tatsuaki Okada, Takashi Kubota, Daisuke Kobayashi, Ryoichiro Yasumitsu, Makoto Kunugi, Shoji Yoshikawa, Katsumi Furukawa, Tetsuya Matsuo
    60th International Astronautical Congress 2009, IAC 2009 2 1096-1100 2009年  査読有り
    After the success of remotely-sensed global observation by SELENE orbiter, Japan has been focusing on the in-situ exploration of the Moon. To know more about the Moon, numerous missions have to be launched to the Moon for surveying different interesting places. Naturally the cost of single mission must be reduced. Japan has been considering a landing mission for about ten years as a next mission to the Moon. This has a few tons of weight and costs a few million euros including the launch vehicle because it also features the future manned mission. Obviously it is not suitable for scientific in-situ exploration, which must be conducted repeatedly. The authors have been studying a small lander on the Moon or the planets in order to enable the multiple in-situ explorations cheaply. With the technologies developed in our studies, the mission named SLIM (Smart Lander for Investigating Moon) has been proposed to demonstrate an autonomous, accurate and soft landing on the specified place of the Moon. SLIM is also helpful to increase the success probability of the nation-led flagship landing mission when it is conducted as a precursor. This paper describes the proposed SLIM mission.
  • TERAZONO Junya, KITAZAWA Yukihito, KANAMORI Hiroshi, TANAKA Satoshi, OKADA Tatsuaki
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN 7(26) 13-16 2009年  査読有り
    Manned lunar explorations are planned in several countries for future goals of their space exploration. Many scientists and engineers are considering that the lunar human outpost will be established no later than early 2020s. The manned lunar mission should be considered as the real problem. To construct rigid lunar bases, the investigation of shallow structure of the moon is required. Here the authors present current technology and understandings of investigation method of lunar shallow structure, and proposes plausible exploration scenario for forthcoming unmanned landing explorations.
  • T. Okada, K. Shirai, Y. Yamamoto, T. Arai, K. Ogawa
    Trans. JSASS Space Tech. Japan 7(26) 39-42 2009年  査読有り筆頭著者責任著者
  • Manuel Grande, Brian J. Maddison, P. Sreekumar, Johani Huovelin, Barry J. Kellett, Chris J. Howe, Ian A. Crawford, D. R. Smith, the D-CIXS Team
    Current Science 96 514-519 2009年  査読有り
  • K. Ogawa, T. Okada
    Advances in Geosciences: Volume 15: Planetary Science (PS) 15 343-354 2009年1月1日  査読有り最終著者責任著者
    © 2009 World Scientific Publishing Company. All Rights Reserved. A carbon nanotube (CNT) field emitter based miniaturized X-ray tube is being developed for X-ray analyses in future planetary explorations. We designed and manufactured the first prototype model of the small X-ray tube, and evaluated its electric and spectral performance. More than 100 pA of electron current from the CNT emitter was obtained at 8 kV applied voltage between electrodes in the initial performance tests. A quick XRF analysis within 300 s was demonstrated by X-ray irradiation from the prototype model. These results indicate that the CNT-based miniaturized X-ray tube has good prospects for use in future XRF/XRD analyses on the extra-terrestrial planets, such as the Moon.
  • L. Richter, C. Dietze, M. Hallmann, T. M. Ho, H. Krueger, C. Lange, T. Sproewitz, S. Wagenbach, L. Witte, A. Barucci, J. Bellerose, T. Okada, H. Yano, J. P. Bibring, J. Biele, S. Ulamec, J. Block, H. Boehnhardt, P. Bousquet, D. Koschny, R. Nadalini
    60th International Astronautical Congress 2009, IAC 2009 2 1331-1344 2009年  査読有り
    Marco Polo is being studied in the ESA Cosmic Vision programme as a sample return mission to a near-Earth asteroid (NEO) with participation by JAXA, with launch planned in the 2018-19 timeframe. In reponse to ESA's Declaration of Interest call in 2008, the Institute of Space Systems of the German Aerospace Center (DLR) led a proposal for a separate lander 'MASCOT' (Marco Polo Surface Scout) to be carried on the mission. The proposal was recommended by ESA for a feasibility study which was subsequently carried out from late 2008 to September 2009. In parallel to the Marco Polo flight opportunity, MASCOT was studied for the Hayabusa-2 mission currently studied by JAXA as the immediate successor to the currently flying Hayabusa mission. Launch would be earlier, taking place in 2014. The MASCOT study started with a preliminary assessment of lander type, landing mode, mobility options and their impact on minimum achievable mass and volume. Differentiation was made between legged landers ('landing in a defined orientation'), landing packages ('landing with uncontrolled orientation') and the number of achievable landing sites (single vs. multiple) and thus the degree of mobility. The analysis showed that a legged lander in the mass range of 70 kg-100 kg - with full mobility - , a weeks-long lifetime and ≃14 kg P/L is feasible, given the weak gravity of potential target NEOs. Reducing size and capability, a legged lander of 30-40 kg was then conceived by giving up mobility, reducing lifetime and by cutting the P/L to ≃10 kg. Finally, a mobile package version with an uprighting mechanism ('MASCOT-XS') and 3 kg of P/L was found feasible for a total mass of 10-15 kg. The constraints imposed by both the Marco Polo and Hayabusa-2 missions mandate MASCOT-XS to be the baseline for the MASCOT design.
  • 杉田精司, 宮本英昭, 橘省吾, 岡田達明, 出村裕英, 大森聡一, 並木則行, 高橋幸弘, 三浦弥生, 長尾敬介, 三河内岳, 佐藤毅彦
    日本惑星科学会誌 遊・星・人 18(2) 521-530 2009年  筆頭著者
  • Y. Yamamoto, T. Okada, H. Shiraishi, K. Shirai, T. Arai, K. Ogawa, K. Hosono, M. Arakawa, M. Kato
    Advances in Space Research 42(2) 305-309 2008年7月18日  査読有り責任著者
    The X-ray spectrometer (XRS) on the SELENE (SELenological and ENgineering Explorer) spacecraft, XRS, will observe fluorescent X-rays from the lunar surface. The energy of the fluorescent X-ray depends on the elements of which the lunar soil consists, therefore we can determine elemental composition of the upper most lunar surface. The XRS consists of three components: XRF-A, SOL-B, and SOL-C. XRF-A is the main sensor to observe X-rays from the lunar surface. SOL-B is direct monitor of Solar X-ray using Si-PIN photodiode. SOL-C is another Solar X-ray monitor but observes the X-rays from the standard sample attached on the base plate. This enables us to analyze by a comparative method similar to typical laboratory XRF methods. XRF-A and SOL-C adopt charge coupled device as an X-ray detector which depletion layer is deep enough to detect X-rays. The X-ray spectra were obtained by the flight model of XRS components, and all components has been worked well to analyze fluorescent X-rays. Currently, development of the hardware and software of the XRS has been finished and we are preparing for system integration test for the launch. © 2007 COSPAR.
  • Satoshi Tanaka, Hiroaki Shiraishi, Manabu Kato, Tatsuaki Okada
    ADVANCES IN SPACE RESEARCH 42(2) 394-401 2008年7月  査読有り
    Further study for the planning of the post SELENE mission has been discussed by a dedicated working group. As the extension of the SELENE-B study [Okada, T., Sasaki, S., Sugihara, T., et al. Lander and rover exploration on the lunar surface: a study for SELENE-B mission. Adv. Space Res. 37, 88-92, 2006] which proposed in-situ geological investigations using a robotic rover and a static lander, this report newly proposes a revised configuration which enhances the scientific field of view. The spacecraft of this mission, "SELENE-II", is designed as a full payload of H-II launch vehicle, while the former study was designed as a half payload of the same vehicle. This expansion of capacity enabled us to increase the payload mass of the lander to deploy geophysical instruments and to land on a wider region on the Moon including polar regions. We also gained the opportunity to deploy two penetrators in order to make a wide network for geophysical observations. In the new configuration, this mission can install three stations of a global seismic network, which will be able to refine the deeper structure of the Moon. In this study also, a new type of deployment system, whose mechanical interface is much simpler than that of the LUNA R-A mission, is preliminarily designed.The selection of the landing site is still undergoing discussion, but the lander is required to operate as long as about one year and more for the geophysical observations, especially for seismology. In order to realize this, one possible idea is to land in permanently sunlit regions. Polar regions also have a benefit from the geological point of view; the north polar region is a typical high land area and the south one is a part of or adjacent to the South Pole Aitken (SPA), where the deeper part of the crust or the mantle material are expected to be collected.In addition to the lander scientific instruments designed previously (Okada et al., 2006.) for the geological survey, a broad band seismometer is considered to be deployed prior to other geophysical instruments and we expect it to provide us with information about the bulk layered structure with only one station if free oscillations are successfully detected. Even if the free oscillations cannot be detected, the dispersion of surface waves not affected by scattering of the regolith or megaregolith layer brings information to understand the crustal and upper mantle structures.Several landing missions are planned by NASA, CNSA, ISRO, and ESA by 2010-2015 during which the operational period is possible to be overlapped by the different missions. This must be a great opportunity to make larger network observations in the future. It must be a great opportunity to start international collaboration in various ways for the upcoming lunar exploration era. (c) 2007 COSPAR. Published by Elsevier Ltd. All rights reserved.
  • Tatsuaki Okada, Manuel Grande, Juergen Oberst, Noriyuki Namiki
    Earth, Planets and Space 60(4) 241 2008年  
  • Tatsuaki Okada, Manuel Grande, Juergen Oberst, Noriyuki Namiki
    EARTH PLANETS AND SPACE 60(4) 241-241 2008年  査読有り筆頭著者責任著者
  • K. Shirai, T. Okada, Y. Yamamoto, T. Arai, K. Ogawa, H. Shiraishi, M. Iwasaki, M. Arakawa, M. Grande, M. Kato
    Earth, Planets and Space 60(4) 277-281 2008年  査読有り
    The x-ray fluorescence spectrometer (XRS) on board Japanese lunar polar orbiter SELENE (Kaguya) Will provide global distribution of major elemental composition on the lunar surface in energy range of characteristic K-α x-ray line emission for Mg, Al, Si, Ca, Ti, and Fe. These measurements will contribute to research of lunar origin and its evolution. The XRS shows a good energy resolution within 200 eV at 5.9 keV relying on charge coupled device (CCD) as photon energy dispersive detector. Total collective area of 100 cm2 for main detector facing the lunar surface is composed of 16 CCD chips. Instrumentation of the XRS and its performance evaluated in laboratory are presented. Copyright © The Society of Geomagnetism and Earth, Planetary and Space Sciences (SGEPSS); The Seismological Society of Japan; The Volcanological Society of Japan; The Geodetic Society of Japan; The Japanese Society for Planetary Sciences; TERRAPUB.
  • Takehiko Arai, Tatsuaki Okada, Yukio Yamamoto, Kazunori Ogawa, Kei Shirai, Manabu Kato
    EARTH PLANETS AND SPACE 60(1) 21-31 2008年  査読有り責任著者
    The Japanese Hayabusa spacecraft successfully carried out in situ observations of S-class asteroid 25143 Itokawa, including the surface major elemental analysis with the X-ray fluorescence spectrometer (XRS-Hayabusa). Our previous results for the X-ray experiments (Okada et al., 2006a) indicated that major elemental ratios of Mg/Si and Al/Si on the surface of Itokawa resemble ordinary LL- or L-chondrites more than any other meteorite analogues. In the NEAR Shoemaker observations of S-class asteroid 433 Eros, the results of X-ray fluorescence observations indicated the depletion of sulfur, probably reflecting impact-induced volatilization, photo-or ion-induced sputtering at the surface, or the loss of FeS-rich materials due to partial melting. Here, we determined the elemental abundance of sulfur (S) on the surface of Itokawa, in addition to that of Mg, Al, and Si, and its regional variation using XRS-Hayabusa observations. In particular, we carefully corrected the fluctuation of solar X-rays, variation of surface geometry, and sensor response function in this analysis, and thus we believe that the results are more accurate than those of our previous report. In this study, the upper and lower limits for Mg/Si, Al/Si, and S/Si overlap those of meteorite analogues for ordinary chondrites or primitive achondrites. In terms of the major elemental composition, Itokawa is best classified as a ordinary chondrite or a primitive achondrite. Our models do not include the mineral mixing effects. With the effects, the abundance of sulfur is expected to be 30% lower than our results. Hence, we conclude that the abundance of sulfur on the surface of Itokawa is almost equal to or even lower than the average abundance in ordinary chondrites. Although the abundances for Mg and Si are globally homogeneous, best-tit or upper limits of mass fraction for Al and S vary in local areas. There is a negative correlation (-0.92) for Al/Si vs. S/Si in ten facets. In particular, the area with the lowest sulfur, accompanied with enriched aluminum, is found in Arcoona, close to a cratered area. Therefore, aluminum enrichment and sulfur depletion features may support events of partial melting on the parent body of Itokawa or aluminum-rich material impacts on the surface of Itokawa. In some areas, Itokawa has a brighter geometric albedo and color variation. Little altered, fresh material may be exposed in these portions of the surface. The sulfur abundance on the surface appears to vary between little and highly altered areas by space weathering. Thus, the sulfur regional variation in our result may reflect the heterogeneity of a surface altered by space weathering.
  • Yoko Maruyama, Kazunori Ogawa, Tatsuaki Okada, Manabu Kato
    EARTH PLANETS AND SPACE 60(4) 293-297 2008年  査読有り責任著者
    We performed laboratory experiments to investigate the effect of particle size in X-ray fluorescence (XRF) with respect to interpreting remote X-ray spectrometry. To simulate microscopic roughness of the uppermost surface of lunar regolith, we used powdery specimens of crashed rocks ranging 25 to 500 mu m in size and flat rock plates for comparison. Our results show that XRF intensities from powdery specimens decrease relative to those from flat plates by up to 50%, especially for larger particle size and at increasing source-to-surface-to-detector angle (phase angle). Corrections should be required for elemental analysis by XRF spectrometry in the SELENE "Kaguya" and other planetary orbiter missions.
  • Kazunori Ogawa, Tatsuaki Okada, Kei Shirai, Manabu Kato
    EARTH PLANETS AND SPACE 60(4) 283-292 2008年  査読有り
    We conducted a numerical estimation of lunar X-ray spectra, which is applicable for lunar X-ray fluorescence observations using an X-ray spectrometer (XRS) onboard the SELENE orbiter, with an improved simulation model. We investigated the integration times of measurements for six elements (Mg, Al, Si, Ca, Ti, and Fe) to achieve signal-to-background ratio of over 10 under various solar conditions. The results of these calculations indicate that expected along-the-track spatial resolutions of a single orbital path for Mg, Al and Si will be < 90 km and 20 km under normal and active Sun conditions, respectively. Ca, Ti and Fe will be also detectable with a spatial resolution of 20 km during the periods active solar flares over M1 class happen to occur.
  • 倉本 圭, 玄田 英典, 荒井 朋子, 岡田 達明, 杉田 精司
    遊・星・人 : 日本惑星科学会誌 16(3) 197-207 2007年9月25日  査読有り
    惑星内部の進化の実証的研究は惑星科学の萌芽的分野であり,「かぐや」をはじめとする月の新たな探査はその前進のための大きな一歩となる.本論文では,これまでの月内部進化についての理解とそれにまっわる謎について,月の熱進化の観点からレビューする.そして今後どのような着眼点で何を調べると月内部進化の理解に有益なのか,考えるためのヒントを提供したい.
  • Kazunori Ogawa, Tatsuaki Okada, Manabu Kato
    EIGHTH IEEE INTERNATIONAL VACUUM ELECTRONICS CONFERENCE 391-+ 2007年  査読有り

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