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観測ロケットを利用した極超音速飛行試験: 2軌道検討
https://jaxa.repo.nii.ac.jp/records/16164
https://jaxa.repo.nii.ac.jp/records/16164b9f5e2ad-84e8-47d9-859e-9f2c0187ad7f
名前 / ファイル | ライセンス | アクション |
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61856028.pdf (736.5 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 観測ロケットを利用した極超音速飛行試験: 2軌道検討 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Trajectory Optimization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Suborbital Reentry Vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Hypersonic Flight Experiment | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Trajectory Design of Experimental Hypersonic Vehicles Launched by Sounding Rockets | |||||
著者 |
藤川, 貴弘
× 藤川, 貴弘× 土屋, 武司× 田口, 秀之× Fujikawa, Takahiro× Tsuchiya, Takeshi× Taguchi, Hideyuki |
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著者所属 | ||||||
東京大学大学院工学系研究科 | ||||||
著者所属 | ||||||
東京大学工学部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発本部(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of Engineering, The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
School of Engineering, The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | |||||
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24年度宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium: FY2012 p. 1-4, 発行日 2013-01 |
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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24年度宇宙輸送シンポジウム (2013年1月17日-1月18日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 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 FY2012 (January 17-18, 2013. 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 | The trajectory research is conducted on experimental hypersonic vehicles launched by S-520 sounding rockets. Direct trajectory optimization techniques are applied to obtain the trajectory which maximizes the duration of the requested experimental conditions, i.e., a Mach number no less than 4 and dynamic pressure between 45 and 55 kPa. It is demonstrated that the experimental conditions can be achieved for more than 1 minute if the initial mass and launch angle of the sounding rocket are designed properly. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: PDF | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: PDF | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0061856028 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: STCP-2012-028 |