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Target Selection and Architecture Design for a Manned Near Earth Object Mission
https://jaxa.repo.nii.ac.jp/records/7284
https://jaxa.repo.nii.ac.jp/records/7284c8faf377-8f7e-4f09-b93f-fd301cf7278e
Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Target Selection and Architecture Design for a Manned Near Earth Object Mission | |||||
言語 | ||||||
言語 | eng | |||||
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 | |||||
著者 |
松本, 道弘
× 松本, 道弘× 川口, 淳一郎× Boden, Ralf× Matsumoto, Michihiro× Kawaguchi, Junichiro |
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著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構月・惑星探査プログラムグループ (JAXA)(JSPEC) : 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Technical University Munich (TUM) | ||||||
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) : 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所 (JAXA)(ISAS) | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | |||||
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 : The 20th Workshop on JAXA Astrodynamics and Flight Mechanics 巻 20, p. 221-231, 発行日 2011-03 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第20回アストロダイナミクスシンポジウム (2010年7月26-27日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県 | |||||
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 | The 20th Workshop on JAXA Astrodynamics and Flight Mechanics 2010 (July 26-27, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper, a first concept for a manned NEA mission is developed, including estimations of required efforts and mass of the spacecraft as well as a target selection. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A first estimation of the in-LEO masses required to successfully conduct a manned NEO mission can be calculated by examining the Delta v requirements for the trajectories to the currently known NEO population. Using this data, a list of possible mission targets and opportunities, as well as example missions, based on different objectives and properties are presented. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
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: AA0065115037 |