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Bibliographic Record
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- Material Type
- 規格・テクニカルリポート類
- Title
- Author/Editor
- 松崎, 貴至井上, 安敏Matsuzaki, TakashiInoue, Yasutoshi
- Author Heading
- Publication, Distribution, etc.
- Publication Date
- 1995-11
- Publication Date (W3CDTF)
- 1995-11
- Alternative Title
- High altitude pressure measurement in the orbital reentry experiment (OREX)
- Periodical title
- 航空宇宙技術研究所報告
- No. or year of volume/issue
- 1281
- Volume
- 1281
- Pages
- 1-15
- ISSN (Periodical Title)
- ISSN : 0389-4010
- Text Language Code
- jpn
- Subject Heading
- Target Audience
- 一般
- Note (General)
- A Japanese first OREX that successfully flew, was launched by the first flight of an H-2 rocket on February 4, 1994, and was inserted into a circular orbit at about 450 km. The OREX could get experimental data during its orbital flight and reentry. The OREX project was conducted in cooperation with the National Aerospace Laboratory and the National Space Development Agency of Japan. Pressure data along the flight trajectory is among the most important and fundamental of the aerodynamic data. NAL took charge of the pressure measurement, as one of various measurement missions, from vacuum at high altitude down to an altitude of about 75 km with a four-decade precision capacitive type pressure transducer. These data can be used to predict the surface pressure and the ambient pressure in similar flights in the future. The data verified the real gas Computational Fluid Dynamics (CFD) codes through comparison with aerodynamic calculation results. This paper outlines the design, fabrication, performance tests, environmental tests, flight operation, flight data and their evaluation of high-altitude pressure measurement systems.資料番号: AA0000108000レポート番号: NAL TR-1281
- Access Restrictions
- インターネット公開
- 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)
- 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