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ロケット打ち上げ時の有人宇宙船アボートシステムに関する検討(続報)
https://jaxa.repo.nii.ac.jp/records/38603
https://jaxa.repo.nii.ac.jp/records/386038a6a8ca8-2ac0-4193-8fa9-e6253f4b03ab
名前 / ファイル | ライセンス | アクション |
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AC1400019.pdf (1.2 MB)
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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 | ||||||
タイトル | ロケット打ち上げ時の有人宇宙船アボートシステムに関する検討(続報) | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Launch Abort System; Human Rated; Ascent Phase; Tractor; Pusher; Loss of Crew | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Conceptual Study of Launch Abort System (Followup report) | |||||
著者 |
和田, 英一
× 和田, 英一× 谷, 直樹× 藤本, 圭一郎× 山西, 伸宏× Wada, Eiichi× Tani, Naoki× Fujimoto, Keiichiro× Yamanishi, Nobuhiro |
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著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
出版者 | ||||||
出版者 | 日本航空宇宙学会(JSASS) | |||||
出版者(英) | ||||||
出版者 | The Japan Society for Aeronautical and Space Sciences(JSASS) | |||||
書誌情報 |
第57回宇宙科学技術連合講演会講演集 en : Proceedings of 57th Space Sciences and Technology Conference 発行日 2013-10 |
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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57回宇宙科学技術連合講演会(2013年10月9日-11日. 米子コンベンションセンター(BiG SHiP)), 米子市, 鳥取県 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | JAXA is investigating a system of human spacecraft and its launcher, and we are studying a Launch Abort System inorder to increase the safty level of crews in the system. The aim of the study is to realize a safe system evaluated with theprobability of loss of crew. For the first step, this reports shows an estimated probability of the loss of crew in case thatthe launcher explodes in a maximum dynamic pressure during an ascent phase. | |||||
権利 | ||||||
権利情報 | (C)2013 一般社団法人 日本航空宇宙学会 | |||||
著者版フラグ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AC1400019000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JSASS-2013-4418 |