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Estimation of the number of asteroids in the Main Belt for a space probe with a clockwise orbit to approach
https://jaxa.repo.nii.ac.jp/records/20642
https://jaxa.repo.nii.ac.jp/records/20642d2a12bb4-ed24-4315-97e3-bd63d7618af3
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 | Estimation of the number of asteroids in the Main Belt for a space probe with a clockwise orbit to approach | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙探査機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 主要ベルト | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 時計回り軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 太陽系 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 重力定数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 火星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 木星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 絶対等級 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | space probe | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | main belt | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | clockwise orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | gravitational constant | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Mars | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Jupiter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | absolute magnitude | |||||
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 | 時計回り軌道からの接近による宇宙プローブに対する主要ベルト小惑星の数の推定 | |||||
著者 |
栃本, 昌孝
× 栃本, 昌孝× 松本, 道弘× 川口, 淳一郎× Tochimoto, Masataka× Matsumoto, Michihiro× Kawaguchi, Junichiro |
|||||
著者所属 | ||||||
慶應義塾大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京都立科学技術大学 工学部 航空宇宙システム工学科 | ||||||
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 | ||||||
Keio University Graduate School of Science and Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan Institute of Technology Department of Aerospace Engineering, Faculty of Engineering | ||||||
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37回月・惑星シンポジウム en : Proceedings of the 37th ISAS Lunar and Planetary Symposium p. 252-254, 発行日 2004-02 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Asteroids in the Main Belt are said to have evidences of how the Solar System was formed. But it is not easy to investigate them, because they are too small to be examined sufficiently. One way to solve this problem is to send a space probe. In this present study, orbital elements of a space probe were optimized to meet as many asteroids as possible in two cases. In one case, asteroids whose semi-major axes are close to 2.35 AU were targeted. In the other case, all asteroids were concluded in the calculation where the original evaluation function was introduced. What is more, a quantitative way to throw the space probe into a clockwise orbit was gotten. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0047898064 |