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飛行実験をめざした極超音速ターボジェットエンジンの開発状況
https://jaxa.repo.nii.ac.jp/records/6007
https://jaxa.repo.nii.ac.jp/records/60071f0b7a75-0ce0-4430-84b9-9297dcc97eb8
名前 / ファイル | ライセンス | アクション |
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49500023.pdf (1.1 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 飛行実験をめざした極超音速ターボジェットエンジンの開発状況 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速ターボジェットエンジン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速航空機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | エンジン設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 飛行試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 飛行環境試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 性能試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空気予冷却器 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱交換器 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧縮機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 液体水素 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic turbojet engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic aircraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | engine design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flight test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flight environment test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | performance test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | air precooler | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heat exchanger | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | compressor | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | liquid hydrogen | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Development status of hypersonic turbojet engine for flight experiments | |||||
著者 |
佐藤, 哲也
× 佐藤, 哲也× Sato, Tetsuya |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Aerospace Technology | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 平成18年度 宇宙航空研究開発機構 総合技術研究本部 宇宙科学研究本部 研究成果報告書 en : JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency 巻 JAXA-SP-06-006, p. 107-110, 発行日 2006-11-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The Japan Space Exploration Agency (JAXA) is developing a hypersonic turbojet engine to realize Mach 5 or 6 cruise vehicles and reusable LEO transportation systems. Design and fabrication of a subscale turbojet engine of 1 kN thrust with an air precooking system have been continued. In 2005, we conducted performance verification test of a newly developed air-precooler, compressor, and a liquid hydrogen supply system for the subscale engine. Test results are briefly reported in this paper. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0049500023 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-06-006 |