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はやぶさ2 Marco Polo の軌道計画について
https://jaxa.repo.nii.ac.jp/records/7386
https://jaxa.repo.nii.ac.jp/records/73863b2720ad-b362-413c-a530-270d8aed4891
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | はやぶさ2 Marco Polo の軌道計画について | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Trajectory Designs of HAYABUSA 2 and MARCO POLO Near Earth Objects Sample Return Missions | |||||
著者 |
川口, 淳一郎
× 川口, 淳一郎× 森本, 睦子× 川勝, 康弘× 松岡, 正敏× 矢野, 創× 吉川, 真× Kawaguchi, Junichiro× Morimoto, Mutsuko Y.× Kawakatsu, Yasuhiro× Matsuoka, Masatoshi× Yano, Hajime× Yoshikawa, Makoto |
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著者所属 | ||||||
宇宙航空研究開発機構月惑星探査推進グループ : 宇宙航空研究開発機構宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構月惑星探査推進グループ | ||||||
著者所属 | ||||||
宇宙航空研究開発機構月惑星探査推進グループ : 宇宙航空研究開発機構宇宙科学研究本部 | ||||||
著者所属 | ||||||
NEC航空宇宙システム | ||||||
著者所属 | ||||||
宇宙航空研究開発機構月惑星探査推進グループ : 宇宙航空研究開発機構宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構月惑星探査推進グループ : 宇宙航空研究開発機構宇宙科学研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC) : Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC) | ||||||
著者所属(英) | ||||||
en | ||||||
JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC) : Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Aerospace Systems | ||||||
著者所属(英) | ||||||
en | ||||||
JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC) : Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC) : Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
アストロダイナミクスシンポジウム講演後刷り集 en : Proceedings of 18th workshop on JAXA Astrodynamics and flight mechanics 巻 2008, 発行日 2009-03 |
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会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Symposium on Flight Mechanics and Astrodynamics 2008 (July 28-29, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 「はやぶさ」は、近地球型小惑星イトカワ(S 型)を探査し現在帰還の途についている。プログラム探査として続く「はやぶさ2」では「はやぶさ」同型機によるC型近地球型小惑星探査、「マルコポーロ(はやぶさMk2)」では世界初の枯渇彗星核サンプルリターンを目指す。両機ともイオンエンジンを搭載している。ここでは、EDVEGA を用いた軌道計画を示す。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | JAXA is currently studying the Hayabusa-follow-on missions to more primitive bodies. Hayabusa-2 is a replica to the Hayabusa spacecraft and will be ready for quick flight in less than four years. It will go to a C-type asteroid, while Hayabusa visited an S-type asteroid, Itokawa. And Marco Polo (Hayabusa mk-II) is much larger spacecraft that may go to an extinct comet, Wilson-Harrington. Both the spacecraft are propelled by the ion engines and the trajectory analysis results through an optimization process. The paper presents how those missions scenarios are built utilizing the EDVEGA strategy. | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11567475 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064733012 |