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ハイブリッドロケットCAMUIを利用したエジェクタロケットの亜音速飛行実験
https://jaxa.repo.nii.ac.jp/records/16616
https://jaxa.repo.nii.ac.jp/records/16616013bea07-3866-466f-8b24-333d1a259f95
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ハイブリッドロケットCAMUIを利用したエジェクタロケットの亜音速飛行実験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | RBCC | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Ejector | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Flight Experiment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Hybrid-rocket | |||||
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(英) | ||||||
その他のタイトル | Flight Experiment of Ejector-Rocket using Hybrid-Rocket CAMUI | |||||
著者 |
植田, 修一
× 植田, 修一× 平岩, 徹夫× 竹腰, 正雄× 谷, 香一郎× 苅田, 丈士× 永田, 晴紀× Ueda, Shuichi× Hiraiwa, Tetsuo× Takegoshi, Masao× Tani, Koichiro× Kanda, Takeshi× Nagata, Harunori |
|||||
著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター | ||||||
著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター | ||||||
著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター | ||||||
著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター | ||||||
著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター | ||||||
著者所属 | ||||||
北海道大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuta Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuta Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuta Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuta Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuta Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Hokkaido University | ||||||
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) | |||||
書誌情報 |
宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium 巻 平成21年度, 発行日 2010-01 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 平成21年度宇宙輸送シンポジウム(2010年1月14日-15日, 宇宙航空研究開発機構宇宙科学研究本部) | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Space Transportation Symposium (January 14-15, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper presents an overview of the subsonic flight experiments for ejector-rocket using CAMUI-type hybrid-rocket. The flight experiment was planned to obtain ejector characteristics under subsonic flight condition, for developing design technology of rocket based combined-cycle engine. An ejector-duct was attached to the engine of the rocket. Two experimental vehicles were launched at 16th March 2009, from the coast of Taiki-town in Hokkaido island of Japan. Flight experiments were successfully conducted and ejector characteristics data at the flight condition were acquired. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: CD-ROM1枚 | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Note: One CD-ROM | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10324301 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064741046 |