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低DeltaVでの地球月遷移軌道計画と電気推進を用いた出発ウインドウの拡大について
https://jaxa.repo.nii.ac.jp/records/7398
https://jaxa.repo.nii.ac.jp/records/73983d7600e8-dad1-4a16-a22a-0502de3eb44c
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 | 低DeltaVでの地球月遷移軌道計画と電気推進を用いた出発ウインドウの拡大について | |||||
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 | The Low Delta-V Transfer Schemes To The Moon And The Window Expansion Via Electric Propulsion | |||||
著者 |
田中, 啓太
× 田中, 啓太× 森本, 睦子× 松本, 道弘× 川口, 淳一郎× Tanaka, Keita× Morimoto, Mutsuko× Matsumoto, Michihiro× Kawaguchi, Junichiro |
|||||
著者所属 | ||||||
東京大学 | ||||||
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 | ||||||
東京大学 | ||||||
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(英) | ||||||
en | ||||||
University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC) | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC) | ||||||
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 |
|||||
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(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Recent Space Exploration sometimes assume an apparent gravity capture around the Moon, using the solar tidal force effect accumulated while flying in the far boundary region of the Earth gravity field. One of the such trajectories we may plan is that S/C which departs from LEO changes the orbit by lunar swing-by and then re-approaches the moon. In this case whether S/C will be captured by the moon or not, however, depends on when S/C departs from LLO, when it swings by the moon and how it approaches the moon. Therefore, such spontaneous capture is hardly applicable to the flexible and practical transportation systems to the moon. This paper focuses on the trajectory from lunar swing-by to the re-approach the moon, and presents how the lunar swing-by conditions is relaxed taking the advantage of the artificial acceleration, electric propulsion means. | |||||
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: AA0064733024 |