@inproceedings{oai:jaxa.repo.nii.ac.jp:00016468,
 author = {溝端, 一秀 and 湊, 亮二郎 and 吹場, 活佳 and 東野, 和幸 and 棚次, 亘弘 and Mizobata, Kazuhide and Minato, Ryojiro and Fukiba, Katsuyoshi and Higashino, Kazuyuki and Tanatsugu, Nobuhiro},
 book = {平成22年度宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium: FY2010},
 month = {},
 note = {平成22年度宇宙輸送シンポジウム(2011年1月20-21日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県, Space Transportation FY2010 (January 20-21, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan, With the aims of creating and validating innovative fundamental technologies for high-speed atmospheric flights, a small scale supersonic experimental vehicle is designed as a flying test bed. Several aerodynamic configurations were proposed and analyzed by wind-tunnel tests. A twin-engine configuration was selected as the baseline. Its flight capability was predicted by mass point analysis on the basis of aerodynamic characterization and performance estimation of the turbojet engine to be installed. In addition, a prototype vehicle with the equivalent configuration and dimension is designed and fabricated for verification of subsonic flight characteristics. Its first flight test was carried out in August 2010 and good flight capability was demonstrated., 形態: カラー図版あり, 形態: CD-ROM1枚, Physical characteristics: Original contains color illustrations, Note: One CD-ROM, 資料番号: AA0065073021},
 publisher = {宇宙航空研究開発機構宇宙科学研究所, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)},
 title = {フライングテストベッドとしての小型超音速飛行実験機の設計およびプロトタイプの試作と試験飛行},
 year = {2011}
}