再使用推進系の総合研究:(1)信頼性設計手法の検討(2)再使用推進系総合計画

Material type: 文書・図像類

Author: 倉谷, 尚志ほか

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)：: Synthetic studies on the reusable and future propulsion systems are presented in this paper. Especially, focused are the high reliability design metho...

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Material Type: 文書・図像類
Title: 再使用推進系の総合研究:(1)信頼性設計手法の検討(2)再使用推進系総合計画
Author/Editor: 倉谷, 尚志
田口, 秀之
姫野, 武洋
長谷川, 卓也
青木, 宏
Kuratani, Naoshi
Taguchi, Hideyuki
Himeno, Takehiro
Hasegawa, Takuya
Aoki, Hiroshi
Author Heading: 倉谷, 尚志
田口, 秀之
姫野, 武洋
長谷川, 卓也
青木, 宏
Kuratani, Naoshi
Taguchi, Hideyuki
Himeno, Takehiro
Hasegawa, Takuya
Aoki, Hiroshi
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: Synthetic studies on reusable propulsion system: (1) Study on the reliability design method (2) General planning of the reusable propulsion system
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: 9-14
ISSN (Periodical Title): ISSN : 1349-1121
Text Language Code: jpn
Subject Heading: 飛行実証
再使用可能な推進系
胴体タンク
信頼性
液体燃料ロケットエンジン
許容度
タービンポンプ
燃焼器
flight demonstration
reusable propulsion system
fuselage tank
reliability
liquid propellant rocket engine
tolerance
turbine pump
combustion chamber
Target Audience: 一般
Note (General): Synthetic studies on the reusable and future propulsion systems are presented in this paper. Especially, focused are the high reliability design methodology for the liquid rocket engine at conceptual phase, the flight demonstration project SubLEO that is propelled by the existing propulsion system, the propellant management of the liquid propellant behavior in the fuselage tank for the reusable vehicle testing and existing rocket under the accelerated environment and the health monitoring sensor system for the hydrogen leakage from the fuselage tank and so on, that is, from the fundamental topics to the application ones for the propulsion systems in FY2003.
資料番号: AA0047944003
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