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

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title垂直離着陸型ロケットの着陸前逆噴射時における空力特性
Other TitleAerodynamic characteristics of a vertical takeoff and landing rocket during reverse thrust before landing
Author(jpn)野中 聡; 渡邊 浩司; 小川 博之; 稲谷 芳文
Author(eng)Nonaka, Satoshi; Watanabe, Koji; Ogawa, Hiroyuki; Inatani, Yoshifumi
Author Affiliation(jpn)宇宙航空研究開発機構 宇宙科学研究本部; 東京農工大学 工学部; 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)Japan Aerospace Exploration Agency Institute of Space and Astronautical Science; Tokyo University of Agriculture and Technology Faculty of Engineering; 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)
宇宙航空研究開発機構宇宙科学研究本部
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 page136
End page139
Publication date2005-03
Languagejpn
Keywordsreverse thrust; aerodynamic characteristic; vertical takeoff and landing rocket; wind tunnel test; flow visualization; aerodynamic drag; drag measurement; PIV; pressure measurement; 逆噴射; 空力特性; 垂直離着陸型ロケット; 風洞試験; 流れの可視化; 空力抵抗; 抗力測定; PIV; 圧力測定
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会
SHI-NOAA0048089035
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/39666


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