@inproceedings{oai:jaxa.repo.nii.ac.jp:00036753,
 author = {下田, 孝幸 and 松崎, 貴至 and Shimoda, Takayuki and Matsuzaki, Takashi},
 book = {航空宇宙技術研究所特別資料, Special Publication of National Aerospace Laboratory},
 month = {Jan},
 note = {航空宇宙技術研究所 8 Jun. 1995 東京 日本, National Aerospace Laboratory 8 Jun. 1995 Tokyo Japan, HOPE(H-2ロケット打上型有翼回収機)開発に先立って3つの実験を行った。1994年2月4日にH-2のTF#1の機会にOREX(軌道再突入実験)を行い、再突入時の空気熱力学および空気力学の基礎データを取得しOREXの主目的のひとつの結果を報告した。空力熱力学については、飛行実験前に風洞実験値とFay&Riddell法から導いた推定値との比較を評価した。実験後、以前に確認したFay&Riddell法を使い飛行軌道から誘導した加熱率を推定した。そして熱解析モデルを使い澱み点の温度を計算し、飛行データの値と比較した。空気力学に関しては、推定値と飛行圧力データとを比較した。, Three experiments are performed preceding to the development of HOPE (H-2 Orbiting Plane). OREX (Orbital Reentry Experiment) was performed taking the opportunity of H-2 TF (Test Flight) No. 1 on Feb. 4, 1994. A result of one of the main purpose of OREX, acquisition of fundamental data of aerothermo- and aerodynamics during reentry is reported. As to aerothermodynamics, comparison between wind tunnel test data and values estimated from Fay & Riddell method was evaluated before a flight experiment. After the experiment, heating rate induced from flight orbit using Fay & Riddell method validated before was evaluated. And a temperature at the stagnation point was calculated using thermal-analysis model, then the value was compared with flight data. As to aerodynamics, flight pressure data was compared with estimated value., 資料番号: AA0000110003, レポート番号: NAL SP-29},
 pages = {17--26},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {The result of an analysis of aerothermo and aerodynamics of OREX},
 volume = {29},
 year = {1996}
}