WEKO3
アイテム
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HTV搭載型回収カプセルの検討
https://jaxa.repo.nii.ac.jp/records/6249
https://jaxa.repo.nii.ac.jp/records/6249794800db-962f-4e81-8a84-5a78988fbe1a
名前 / ファイル | ライセンス | アクション |
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49056018.pdf (1.4 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | HTV搭載型回収カプセルの検討 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙ステーション補給機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ISS | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スペースシャトル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 回収カプセル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機信頼性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 鈍頭体 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙輸送システム | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | H-2 transfer vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ISS | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | space shuttle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reentry capsule | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft reliability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | blunt body | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | space transportation system | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Concept study of HTV loading re-entry capsule | |||||
著者 |
藤井, 謙司
× 藤井, 謙司× 野田, 篤司× 平岩, 徹夫× 山中, 浩二× Fujii, Kenji× Noda, Atsushi× Hiraiwa, Tetsuo× Yamanaka, Koji |
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著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 事業推進部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙基幹システム本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Program Management and Integration Dept., Inst. of Space Tech. and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Office of Space Flight and Operations | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:宇宙輸送系基盤技術 en : JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Space Transportation Systems 巻 JAXA-SP-05-010, p. 89-92, 発行日 2006-01-20 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Retirement of the space shuttle in 2010 was already decided and there will be some difficulties in transportation from ISS (the International Space Station) from 2010 until the next generation new transportation system CEV (Crew Exploration Vehicle) will be operative. JAXA started concept studies of re-entry systems that will be loaded in HTV (H-2 Transfer Vehicle) and will be ejected after its deorbit. A minimum but affordable capsule with the capability of carrying 50 kg payload was selected from various kinds of concept. System study was conducted and it showed that the capsule is feasible but has some technical problems to be solved. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0049056018 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-05-010 |