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アイテム
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非化学推進による地球周回軌道間移行ミッションの性能評価
https://jaxa.repo.nii.ac.jp/records/17504
https://jaxa.repo.nii.ac.jp/records/17504c8b93b5c-a3d8-4596-bbd0-39c5f9eff106
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 | 非化学推進による地球周回軌道間移行ミッションの性能評価 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 化学推進 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 電気推進 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 太陽熱推進 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道変換機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 大型宇宙構造物 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星姿勢制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 比推力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | GEO | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | GTO | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | chemical propulsion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | electric propulsion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar thermal propulsion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbit transfer vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | large space structure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite attitude control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | specific impulse | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | GEO | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | GTO | |||||
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 | Performance evaluation of Earth orbit transfer missions by non-chemical propulsion | |||||
著者 |
中野, 正勝
× 中野, 正勝× 藤田, 和久× Viliam, Kmetik× 木皿, 且人× 新野, 正之× Nakano, Masakatsu× Fujita, Kazuhisa× Viliam, Kmetik× Kisara, Katsuto× Niino, Masayuki |
|||||
著者所属 | ||||||
科学技術振興事業団 | ||||||
著者所属 | ||||||
科学技術振興事業団 | ||||||
著者所属 | ||||||
航空宇宙技術振興財団 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Science and Technology Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Science and Technology Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Technology Foundation | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
出版者 | ||||||
出版者 | 宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | The Institute of Space and Astronautical Science (ISAS) | |||||
書誌情報 |
宇宙輸送シンポジウム 平成13年度 en : Proceedings of Space Transportation Symposium FY2001 p. 304-307, 発行日 2002-04 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper compares the mission performances of advanced propulsion systems such as electric, solar thermal and laser propulsion systems for GTO-GEO orbit-raising applications. The performance of payload fractions to mission durations was evaluated under the constraints of the Earth shadow and the Van-Allen radiation belts. It was shown that the electric propulsion system can deliver much payload fractions in mission durations over several months, and the solar thermal and laser propulsion systems can deliver much payload fractions in comparison with the chemical propulsion with less radiation damage. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0033392076 |