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Feasibility study for a small Mars exploration rotorcraft
https://jaxa.repo.nii.ac.jp/records/7656
https://jaxa.repo.nii.ac.jp/records/7656d0679eec-f1e6-4499-b033-479aa5cda273
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Feasibility study for a small Mars exploration rotorcraft | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 予備調査 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 実験研究 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 回転翼航空機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 火星探査 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ロービング機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 火星大気 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 飛行条件 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | feasibility study | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | experimental investigation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rotary wing aircraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Mars exploration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | roving vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Mars atmosphere | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flight condition | |||||
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 | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル | ||||||
その他のタイトル | 火星探査のためのロータクラフト機の検討 | |||||
著者 |
都築, 範明
× 都築, 範明× 佐藤, 俊逸× 安部, 隆士× Tsuzuki, Noriaki× Sato, Shunichi× Abe, Takashi |
|||||
著者所属 | ||||||
東京大学 大学院工学系研究科 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS) | |||||
書誌情報 |
平成16年度アストロダイナミクスシンポジウム:講演後刷り集 en : ISAS proceedings of 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers p. 127-133, 発行日 2005-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 火星地表探査においてローバと組になって探査を行うロータークラフト機の可能性についての検討を行う。このようなロータークラフト機の併用により、ローバの活動性を向上させることが可能である。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | An aerial vehicle operating under the command of a rover has a potential to extend the coverage for Mars exploration. Especially, a rotorcraft equipped with an imaging camera can gather geographic information around the rover and enables making of a smart strategy for the exploration. The development of such a rotorcraft, however, must solve some difficulty due to the thin Mars atmosphere. This is because the aerodynamic characteristics of the rotor depend mainly on the Reynolds number (Re) that decreases due to the thin atmosphere. In this paper, the aerodynamic characteristics of rotors were experimentally investigated to access a capability of the hover performance of the rotor in a very low Reynolds number regime (Re = 10(exp 3) to 10(exp 4), Ultra-low Reynolds number) that is expected in the thin Mars atmosphere. Based on the experimental investigation, the feasibility of such a rotorcraft was demonstrated. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0918-8053 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0047897023 |