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CFRP製ハイブリッドロケットモーターの開発・製作
https://jaxa.repo.nii.ac.jp/records/49469
https://jaxa.repo.nii.ac.jp/records/49469de7ad8df-c695-444c-92b3-95e9e476d4d4
名前 / ファイル | ライセンス | アクション |
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SA6000184013.pdf (896.0 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2023-05-23 | |||||
タイトル | ||||||
タイトル | CFRP製ハイブリッドロケットモーターの開発・製作 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | Development and production of CFRP hybrid rocket motors | |||||
著者 |
吉野, 啓太
× 吉野, 啓太× 高野, 敦× 喜多村, 竜太× 正井, 卓馬× 植村, 寧夫× 船見, 祐揮× YOSHINO, Keita× TAKANO, Atsushi× KITAMURA, Ryuta× MASAI, Takuma× UEMURA, Shizuo× FUNAMI, Yuki |
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著者所属 | ||||||
神奈川大学大学院 | ||||||
著者所属 | ||||||
神奈川大学 | ||||||
著者所属 | ||||||
神奈川大学 | ||||||
著者所属 | ||||||
神奈川大学 | ||||||
著者所属 | ||||||
神奈川大学 | ||||||
著者所属 | ||||||
防衛大学校 | ||||||
著者所属(英) | ||||||
en | ||||||
Kanagawa University Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
Kanagawa University | ||||||
著者所属(英) | ||||||
en | ||||||
Kanagawa University | ||||||
著者所属(英) | ||||||
en | ||||||
Kanagawa University | ||||||
著者所属(英) | ||||||
en | ||||||
Kanagawa University | ||||||
著者所属(英) | ||||||
en | ||||||
National Defense Academy | ||||||
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 |
令和4年度宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium FY2022 発行日 2023-01 |
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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 | 令和4年度宇宙輸送シンポジウム(2023年1月12日-13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 Symposium FY2022 (January 12-13, 2023. 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 authors are developing and manufacturing hybrid rockets to launch nano-satellites quickly and inexpensively. The development of a CFRP motor case with threaded fasteners has enabled disassembly, inspection, and reuse of the motor case, thereby reducing cost and weight. Based on previous research, there is a possibility that the motor case will burn out due to the increased thermal load caused by a larger engine. This report describes the development and fabrication of the motor case, reflecting the countermeasures and the results of combustion and launch tests of a prototype model using a metal motor case without CFRP. | |||||
著者版フラグ | ||||||
出版タイプ | AM | |||||
出版タイプResource | http://purl.org/coar/version/c_ab4af688f83e57aa | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA6000184013 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | STCP-2022-013 |