Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
出版者
宇宙航空研究開発機構
出版者（英）
Japan Aerospace Exploration Agency (JAXA)
雑誌名
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
雑誌名(英)
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
巻
JAXA-RM-04-009
ページ
5 - 8
発行年
2004-10-29
抄録（英）
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.
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
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