極超音速ターボジェットエンジンの研究開発

Material type: 文書・図像類

Author: 佐藤, 哲也ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2004-10-29

Material Format: Digital

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Note (General)：: Development studies on a hypersonic turbo jet engine have been conducted to be employed to the reusable space transportation. As this mid-term target,...

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Material Type: 文書・図像類
Title: 極超音速ターボジェットエンジンの研究開発
Author/Editor: 佐藤, 哲也
田口, 秀之
下平, 一雄
小林, 弘明
岡井, 敬一
岩瀬, 識
二村, 尚夫
森本, 哲也
小島, 孝之
藤田, 和央
Sato, Tetsuya
Taguchi, Hideyuki
Shimodaira, Kazuo
Kobayashi, Hiroaki
Okai, Keiichi
Iwase, Shiki
Futamura, Hisao
Morimoto, Tetsuya
Kojima, Takayuki
Fujita, Kazuhisa
Author Heading: 佐藤, 哲也
田口, 秀之
下平, 一雄
小林, 弘明
岡井, 敬一
岩瀬, 識
二村, 尚夫
森本, 哲也
小島, 孝之
藤田, 和央
Sato, Tetsuya
Taguchi, Hideyuki
Shimodaira, Kazuo
Kobayashi, Hiroaki
Okai, Keiichi
Iwase, Shiki
Futamura, Hisao
Morimoto, Tetsuya
Kojima, Takayuki
Fujita, Kazuhisa
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2004-10-29
Publication Date (W3CDTF): 2004-10-29
Alternative Title: Development study on the hypersonic turbojet engine
Periodical title: 宇宙航空研究開発機構研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:輸送系 = JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Space Transportation System
No. or year of volume/issue: JAXA-RM-04-009
Volume: JAXA-RM-04-009
Pages: 21-26
ISSN (Periodical Title): ISSN : 1349-1121
Text Language Code: jpn
Subject Heading: スペースプレーン
TSTO
極超音速
ターボジェットエンジン
再使用宇宙機
宇宙輸送システム
複合材料
風洞試験
spaceplane
hypersonic speed
turbojet engine
reusable spacecraft
space transportation system
composite material
wind tunnel test
Target Audience: 一般
Note (General): Development studies on a hypersonic turbo jet engine have been conducted to be employed to the reusable space transportation. As this mid-term target, it is proposed that a subscale prototype engine will be produced and demonstrated under sea-level-static and supersonic conditions (Mach 6) for getting fundamental key technologies and valuable experiences. Engine system optimization analyses for an actual TSTO space plane by the precise components data on the performance and weight as well as the dynamic characteristics along the accelerating trajectory is also investigated. In this year, fundamental key results were obtained by a trade-off study to decide the prototype engine cycle, a study of the defrosting system on the precooler (a cryogenic heat exchanger), wind tunnel tests of air inlets and nozzles and an application study of the composite materials.
資料番号: AA0047944005
レポート番号: JAXA-RM-04-009
Access Restrictions: 限定公開
Periodical Title (NCID): AA11983593
https://ci.nii.ac.jp/ncid/AA11983593
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ