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ハイブリッドロケット内部弾道特性評価技術の発展経緯と課題
https://jaxa.repo.nii.ac.jp/records/16481
https://jaxa.repo.nii.ac.jp/records/16481f294c71b-e560-460a-923d-2792b0a34a33
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内部弾道特性評価技術の発展経緯と課題 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Hybrid Rocket | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Internal Ballistics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Numerical Simulation | |||||
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 | Progress of development and challenges of evaluation technology on internal ballistic characteristics of hybrid rocket | |||||
著者 |
船見, 祐揮
× 船見, 祐揮× 嶋田, 徹× Funami, Yuki× Shimada, Toru |
|||||
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宇宙科学研究所 (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
School of Engineering, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
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 | Estimation of chamber pressure is necessary for the design of a hybrid rocket. Comprehension of combustion instability and regression rate behaviour is required in order to estimate chamber pressure. Characteristics of combustion instability and regression rate behaviour are called "internal ballistics". In this study, literature research of AIAA paper about hybrid rocket's internal ballistics is done to recognize technical problems of the evaluation of internal ballistics characteristic. | |||||
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: AA0065073034 |