システム解析の研究:コンセプトスタディプログラムの開発と設計基準の検討および空力技術に関する研究

Material type: 文書・図像類

Author: 鈴木, 広一ほか

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)：: In this research, optimal design, evaluation, and aerodynamic problems for future space transportation systems are conducted. An optimal design progra...

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Material Type: 文書・図像類
Title: システム解析の研究:コンセプトスタディプログラムの開発と設計基準の検討および空力技術に関する研究
Author/Editor: 鈴木, 広一
高嵜, 浩一
南, 吉紀
甲斐, 高志
佐藤, 哲也
小林, 弘明
藤田, 和央
伊藤, 健
黒滝, 卓司
Suzuki, Hirokazu
Takasaki, Koichi
Minami, Yoshinori
Kai, Takashi
Sato, Tetsuya
Kobayashi, Hiroaki
Fujita, Kazuhisa
Ito, Takeshi
Kurotaki, Takuji
Author Heading: 鈴木, 広一
高嵜, 浩一
南, 吉紀
甲斐, 高志
佐藤, 哲也
小林, 弘明
藤田, 和央
伊藤, 健
黒滝, 卓司
Suzuki, Hirokazu
Takasaki, Koichi
Minami, Yoshinori
Kai, Takashi
Sato, Tetsuya
Kobayashi, Hiroaki
Fujita, Kazuhisa
Ito, Takeshi
Kurotaki, Takuji
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: Research on system analysis: Development of concept study program, investigation on design criteria and research on aerodynamic technologies
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: 5-8
ISSN (Periodical Title): ISSN : 1349-1121
Text Language Code: jpn
Subject Heading: システム解析
宇宙輸送システム
空力特性
評価
高エンタルピ風洞
最適設計
設計条件
再使用宇宙機
system analysis
space transportation system
aerodynamic characteristic
evaluation
high enthalpy wind tunnel
optimal design
design criterion
reusable spacecraft
Target Audience: 一般
Note (General): In this research, optimal design, evaluation, and aerodynamic problems for future space transportation systems are conducted. An optimal design program is developed in the research of optimal design and evaluation. The design criteria are also investigated and several types of the concept for the future space transportation systems are designed optically and are evaluated. In the last physical year, a developmental plan of prototype of the design program was established and a part of the prototype was developed. The catalysis and the real gas effect are dealt as aerodynamic problems for the future space transportation systems. In the last physical year, precious data were obtained by the high enthalpy wind tunnel.
資料番号: AA0047944002
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