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Mission analysis of asteroid flyby exploration by miniature asteroid interceptors
https://jaxa.repo.nii.ac.jp/records/7588
https://jaxa.repo.nii.ac.jp/records/75885daaf646-8051-4dc3-a5ff-1418b22bf167
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Mission analysis of asteroid flyby exploration by miniature asteroid interceptors | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フライバイミッション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | インタセプタ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 小惑星インタセプタ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 小惑星ミッション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 静止トランスファ軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | GTO | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 地球同期軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道計算 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷移軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 小惑星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スイングバイ技術 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道最適化 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flyby mission | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | interceptor | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | asteroid interceptor | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | asteroid mission | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | geostationary transfer orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | GTO | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Earth synchronous orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbit calculation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | trajectory analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transfer orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | asteroid | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | swingby technique | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | trajectory optimization | |||||
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 | ||||||
その他のタイトル | 小型探査機インタセプタによる小惑星フライバイ探査のミッション解析 | |||||
著者 |
川勝, 康弘
× 川勝, 康弘× 森, 治× 津田, 雄一× 中谷, 幸司× 多羅尾, 康太× 川口, 淳一郎× Kawakatsu, Yasuhiro× Mori, Osamu× Tsuda, Yuichi× Nakaya, Koji× Tarao, Kota× Kawaguchi, Junichiro |
|||||
著者所属 | ||||||
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 宇宙科学研究本部 | ||||||
著者所属 | ||||||
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 宇宙科学研究本部 | ||||||
著者所属 | ||||||
東京大学 大学院 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
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/ISAS) | |||||
書誌情報 |
第15回アストロダイナミクスシンポジウム講演後刷り集 2005 en : Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics p. 141-146, 発行日 2006-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 本発表では、「インタセプタ」という呼称で現在構想中の10kg級の超小型探査機を用いた、小惑星フライバイミッションのミッション解析結果を報告する。今回は(1)静止衛星打上時に小型固体モータを装着したインタセプタを相乗りさせるミッション、(2)小型打上機体により複数のインタセプタを同時に打ち上げるミッション、の2つのミッション形態を想定し、軌道計画、運用シナリオなどを検討した結果を報告する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Reported in this paper is the result of the mission analysis of asteroid flyby missions using miniature asteroid interceptors. Two types of mission concept are considered. The first is a mission concept with an interceptor boosted from GTO (Geostationary Transfer Orbit) by small solid rocket motor (assuming the piggy back launch of geostationary satellite). The second is a mission concept with four interceptors loaded on a mother carrier spacecraft, launched together and released on orbit to target four different asteroids. The results of the trajectory analysis and operation sequence investigation are reported in the paper. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063480023 |