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RBCC エンジンのシステム解析の現状について
https://jaxa.repo.nii.ac.jp/records/16454
https://jaxa.repo.nii.ac.jp/records/1645444282251-439b-4c27-862d-d3cbbdf01ef6
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 | RBCC エンジンのシステム解析の現状について | |||||
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 | Hypersonic Air-breathing Engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | System Analysis | |||||
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 | Status of RBCC Engine System Analysis | |||||
著者 |
富岡, 定毅
× 富岡, 定毅× 平岩, 徹夫× 齋藤, 俊仁× 加藤, 周徳× 小寺, 正敏× 長谷川, 進× Tomioka, Sadatake× Hiraiwa, Tetsuo× Saito, Toshihito× Kato, Kanenori× Kodera, Masatoshi× Hasegawa, Susumu |
|||||
著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター (JAXA)(KSPC) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター (JAXA)(KSPC) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター (JAXA)(KSPC) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター (JAXA)(KSPC) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター (JAXA)(KSPC) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所 | |||||
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22年度宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium: FY2010 発行日 2011 |
|||||
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22年度宇宙輸送シンポジウム(2011年1月20-21日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県 | |||||
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 FY2010 (January 20-21, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | System analysis upon a TSTO launch vehicle equipping a Rocket-Based Combined Cycle Engine was conducted, to evaluate the benefits of hypersonic air-breathing technology upon the performance of the launch vehicle. Upon the results of aerodynamic performance prediction, structure analysis as well as the supply system analysis was conducted. Though a high Isp performance of the engine system was predicted, the resulting payload capability of the launch system was found to depend highly on the airframe weight including the engine weight, and ranged from less than 1% to 4% of the take-off weight. The analysis method and primary results are herein reported | |||||
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: AA0065073007 |