WEKO3
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Test results of rocket recovery demonstrator vehicle suspended from helicopter
https://jaxa.repo.nii.ac.jp/records/7758
https://jaxa.repo.nii.ac.jp/records/77581ea5afe9-8f07-4dd7-9f2e-33ee8d8ec0e4
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 | Test results of rocket recovery demonstrator vehicle suspended from helicopter | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ロケット回収実施機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ヘリコプター | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | パラグライダー | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 誘導 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 分離 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 重心 | |||||
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 | 制御系 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rocket recovery demonstrator vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | helicopter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | paraglider | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | guidance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | separation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | center of gravity | |||||
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 | control system | |||||
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 | ロケット回収実験機のヘリ吊り下げ時の機体特性と制御結果 | |||||
著者 |
佐野, 成寿
× 佐野, 成寿× 大塚, 浩仁× 森田, 泰弘× 平木, 講儒× Sano, Naruhisa× Otsuka, Hirohito× Morita, Yasuhiro× Hiraki, Koju |
|||||
著者所属 | ||||||
IHIエアロスペース・エンジニアリング | ||||||
著者所属 | ||||||
アイ・エイチ・アイ・エアロスペース | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
九州工業大学 | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Aerospace Engineering Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Aerospace Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
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15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 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers p. 352-355, 発行日 2004-02 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | ロケットをパラグライダで回収する技術の実証のためのロケット回収実験機を説明する。また、2003年2月に実施した、ヘリコプタから吊り下げた状態での機体の制御系の機能や性能を確認した結果を示す。ヘリコプタによる高空からの投下試験は、2004年2月に実施予定である。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This rocket recovery demonstrator vehicle is scheduled to launch in February 2004. This demonstrator vehicle is planned to perform the guidance by the paraglider with small rocket vehicle. This vehicle will be dropped from a helicopter at 2,000 m altitude in February 2004. Some functions and performances of this demonstrator were tested at February 2003. The outline of this flight test in 2004 is shown and the results of the tests under the condition suspended from the helicopter in February 2003 are shown. | |||||
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: AA0046652057 |