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

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title火星探査用小型回転翼機の実現可能性とその回転翼ホバー性能
Other TitleFeasibility of a compact rotary wing aircraft for surveying Mars and hovering performance of the rotary wings
Author(jpn)都築 範明; 佐藤 俊逸; 安部 隆士
Author(eng)Tsuzuki, Noriaki; Sato, Shunichi; Abe, Takashi
Author Affiliation(jpn)東京大学 大学院工学系研究科; 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)University of Tokyo School 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 page140
End page143
Publication date2005-03
Languagejpn
Keywordsrotary wing aircraft; rotary wing; Mars; feasibility; hovering; aerodynamic characteristic; Reynolds number; wing tip Mach number; space exploration; 回転翼機; 回転翼; 火星; 実現可能性; ホバリング; 空力特性; Reynolds数; 翼端マッハ数; 宇宙探査
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会
SHI-NOAA0048089036
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/32241


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