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Some Aspects on Hydrocarbon-fueled RBCC Engines for a TSTO Launch Vehicle
https://jaxa.repo.nii.ac.jp/records/22693
https://jaxa.repo.nii.ac.jp/records/226938108d3a6-c732-436d-8dbf-520dd16be6c9
Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2016-07-29 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Some Aspects on Hydrocarbon-fueled RBCC Engines for a TSTO Launch Vehicle | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | RBCC Engines | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | TSTO Launch Vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | System Analysis | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
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 | |||||
著者 |
富岡, 定毅
× 富岡, 定毅× 小林, 完× 齋藤, 俊仁× 加藤, 周徳× 小寺, 正敏× 谷, 香一郎× Tomioka, Sadatake× Kobayashi, Kan× Saito, Toshihito× Kato, Kanenori× Kodera, Masatoshi× Tani, Kouichiro |
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著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター(JAXA)(KSPC) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター(JAXA)(KSPC) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター(JAXA)(KSPC) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター(JAXA)(KSPC) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター(JAXA)(KSPC) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター(JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
出版者 | ||||||
出版者 | 日本航空宇宙学会 (JSASS) | |||||
出版者(英) | ||||||
出版者 | Japan Society for Aeronautical and Space Sciences (JSASS) | |||||
書誌情報 |
en : Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 巻 14, 号 ists30, p. Po_1_1-Po_1_8, 発行日 2016-05-11 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Engine system analysis upon a Rocket-Based Combined Cycle (RBCC) engine for the booster stage of a TSTO launch vehicle was conducted, to evaluate the effects of hydrocarbon fuel type upon the performance of the engine and the whole launch vehicle. A higher thrust and cooling performance with methane was shown, while some technical challenges were also noted. Combination of the scramjet flow pass and the rocket engines, i.e., rocket engine being embedded into the scramjet flow pass or separately mounted to the airframe, was varied to show that the separated configuration mitigated cooling problem, and resulted in a better performance for mid-speed regime. | |||||
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(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1884-0485 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.2322/tastj.14.Po_1_1 | |||||
関連名称 | info:doi/10.2322/tastj.14.Po_1_1 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1610081000 |