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回転バルブ式4気筒パルスデトネーションエンジン飛行試験機の研究開発
https://jaxa.repo.nii.ac.jp/records/16198
https://jaxa.repo.nii.ac.jp/records/16198b0ce224c-8dfd-4f2a-bc8d-79c1e9740c20
名前 / ファイル | ライセンス | アクション |
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61856062.pdf (3.1 MB)
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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 | 回転バルブ式4気筒パルスデトネーションエンジン飛行試験機の研究開発 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Detonation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Pulse Detonation Engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Flight Test | |||||
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 | Research and Development of a Rotary-valved Four-cylinder Pulse Detonation Engine flight Test Model | |||||
著者 |
笠原, 次郎
× 笠原, 次郎× 坂本, 龍基× 両角, 智人× 柏崎, 貴司× 藤原, 大× 松岡, 健× 松尾, 亜紀子× 船木, 一幸× Kasahara, Jiro× Sakamoto, Ryuki× Morozumi, Tomohito× Kashiwazaki, Takashi× Fujiwara, Yutaka× Matsuoka, Ken× Matsuo, Akiko× Funaki, Ikko |
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著者所属 | ||||||
筑波大学 | ||||||
著者所属 | ||||||
筑波大学 | ||||||
著者所属 | ||||||
筑波大学 | ||||||
著者所属 | ||||||
筑波大学 | ||||||
著者所属 | ||||||
筑波大学 | ||||||
著者所属 | ||||||
広島大学 | ||||||
著者所属 | ||||||
慶應義塾大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tsukuba | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tsukuba | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tsukuba | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tsukuba | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tsukuba | ||||||
著者所属(英) | ||||||
en | ||||||
Hiroshima University | ||||||
著者所属(英) | ||||||
en | ||||||
Keio University | ||||||
著者所属(英) | ||||||
en | ||||||
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 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 | Thrust-measurement experiment was carried out using a four-cylinder pulse detonation rocket engine (PDRE) with a rotary valve. This PDRE used three types of gases, oxidizer (N2O), fuel (C2H4), and purge gas (He) to generate detonation wave intermittently. We used a rotary valve attached coaxially to a motor for supplying these three gases. We achieved time-averaged thrust of 258.5 N and specific impulse of 138.7 sec in the operation for 1000 msec. | |||||
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: PDF | |||||
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 | Physical characteristics: PDF | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0061856062 | |||||
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-2012-062 |