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FTBとしての小型超音速飛行実験機の構想と予備的な亜音速機の試作
https://jaxa.repo.nii.ac.jp/records/16757
https://jaxa.repo.nii.ac.jp/records/1675730c52ad7-4f0d-499a-8c39-bdb06961b26f
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 | FTBとしての小型超音速飛行実験機の構想と予備的な亜音速機の試作 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Aerospace Plane, Supersonic, Flight Verification | |||||
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 | Plan of a amall-scale aupersonic flight experimental vehicle as a flying test bed for verifying fundamental technologies on aerospace planes and construction of its prototype for subsonic flights | |||||
著者 |
溝端, 一秀
× 溝端, 一秀× 湊, 亮二郎× 吹場, 活佳× 東野, 和幸× 棚次, 亘弘× Mizobata, Kazuhide× Minato, Ryojiro× Fukiba, Katsuyoshi× Higashino, Kazuyuki× Tanatsugu, Nobuhiro |
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著者所属 | ||||||
室蘭工業大学 | ||||||
著者所属 | ||||||
室蘭工業大学 | ||||||
著者所属 | ||||||
室蘭工業大学 | ||||||
著者所属 | ||||||
室蘭工業大学 | ||||||
著者所属 | ||||||
室蘭工業大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Muroran Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Muroran Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Muroran Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Muroran Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Muroran Institute of Technology | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium 巻 平成20年度, 発行日 2009 |
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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20年度宇宙輸送シンポジウム(2009年1月19日-20日, 宇宙航空研究開発機構宇宙科学研究本部) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | With the aims of realizing hypersonic aircraft and reusable space transportation systems, researches are being carried out at Muroran Institute of Technology, for creation of innovative fundamental technologies for flying at high speeds in the atmosphere. Such technologies will be validated by flight experiments using a small scale unmanned supersonic plane. Its aerodynamic configuration is designed and analyzed by wind-tunnel tests. A preliminary airframe is being constructed for the initial phase of subsonic flight tests. In addition, test facilities such as a supersonic wind tunnel, a flight simulator, and a high-speed sled track, are being prepared for various ground verification. | |||||
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 | |||||
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: AA0064292064 |