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超抵高度衛星SLATSの熱制御と高層大気
https://jaxa.repo.nii.ac.jp/records/38645
https://jaxa.repo.nii.ac.jp/records/38645e0df0c76-5647-474a-936e-60a12439bdbd
名前 / ファイル | ライセンス | アクション |
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AC1500004000.pdf (658.3 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-04-09 | |||||
タイトル | ||||||
タイトル | 超抵高度衛星SLATSの熱制御と高層大気 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Super low altitude satellite | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | SLATS | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Thermal control | |||||
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 | Upper atomosphere and Thermal control of the Super Low Altitude Test Satellite | |||||
著者 |
川崎, 春夫
× 川崎, 春夫× 高畑, 博樹× 此上, 一也× 佐藤, 洋平× 今村, 俊介× Kawasaki, Haruo× Kohata, Hiroki× Konoue, Kazuya× Satoh, Yohei× Imamura, Shunsuke |
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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 | ||||||
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) | ||||||
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 | "The Super Low Altitude Test Satellite (SLATS) is an engineering test satellite currently under development in JAXA in an attempt to open a new frontier of space utilization on extremely low earth orbits. The altitude of SLATS orbit is around 200km altitude. In this altitude, rarefied aerodynamics and high-density atomic oxygen effect on the thermal design of SLATS. The thermal control of SLATS was introduced in this paper. And, the equilibrium temperature on the bumper of SLATS was estimated with upper atmosphere data." | |||||
権利 | ||||||
権利情報 | ©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: AC1500004000 | |||||
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-2013-4120 |