JAXA Repository / AIREX 未来へ続く、宙(そら)への英知

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Other TitleAtmospheric reentry vehicle using deceleration mechanism by a tension shell structure
Author(jpn)堤 裕樹; 若月 一彦; 安部 隆士; 佐藤 俊逸
Author(eng)Tsutsumi, Yuki; Wakatsuki, Kazuhiko; Abe, Takashi; Sato, Shunichi
Author Affiliation(jpn)東海大学 大学院; 東海大学 大学院; 宇宙航空研究開発機構 宇宙科学研究本部; 宇宙航空研究開発機構 宇宙科学研究本部
Author Affiliation(eng)Tokai University Graduate School; Tokai University Graduate School; Japan Aerospace Exploration Agency Institute of Space and Astronautical Science; Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Issue Date2005-03
PublisherInstitute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
Publication title宇宙航行の力学シンポジウム 平成16年度
Symposium on Flight Mechanics and Astrodynamics 2004
Start page144
End page147
Publication date2005-03
Keywordsspacecraft reentry; atmospheric entry; reentry vehicle; tension shell; deceleration; aerodynamic characteristic; aerodynamic heating; hypersonic wind tunnel; wind tunnel test; 宇宙機再突入; 大気圏突入; 再突入機; テンションシェル; 減速; 空力特性; 空力加熱; 極超音速風洞; 風洞試験
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会

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