@techreport{oai:jaxa.repo.nii.ac.jp:00039676,
 author = {伊藤, 忠 and 穂積, 弘一 and 吉沢, 昭 and 河本, 巌 and 石塚, 只夫 and Ito, Tadashi and Hozumi, Koichi and Yoshizawa, Akira and Kawamoto, Iwao and Ishizuka, Tadao},
 month = {Nov},
 note = {航空宇宙技術研究所と宇宙開発事業団との間で、H-2ロケット打上げ型有翼宇宙往還機(HOPE)の研究開発についての共同研究が1987年より実施された。空力特性の研究の一環として想定された往還機形状模型の風洞試験が実施されたが、その全データは航空宇宙技術研究所の数値シミュレータのデータベースシステムに「HOPEデータベース」として収録されている。本報告では62HOPE形状の風洞試験の結果に基づき、さらに性能向上を目指した63HOPE形状の風洞試験概要とそのデータベースの格納について述べる。, The cooperative research work on the development of HOPE (H-2 rocket Orbiting Plane) has been conducted by NAL and NASDA since 1987. As a part of this research work, wind tunnel tests were conducted to obtain the aerodynamic characteristics of several candidate shapes of the orbiter. All data obtained in the tests were recorded as 'the HOPE Wind Tunnel Data Base' in the data base system of the NAL's Numerical Simulator. The contents of the wind tunnel data base for the first year which was named 'the 62HOPE Configuration Wind Tunnel Tests' in the data base system was already reported, providing the information necessary to use the data base system. As additional data was compiled during the first stage (1987-1989) of the research, this report describes the contents of the wind tunnel data base named 'the 63HOPE Configuration Wind Tunnel Tests'., 資料番号: AA0000096000, レポート番号: NAL TM-689},
 title = {HOPE風洞試験データベースについて　その２},
 year = {1995}
}