@inproceedings{oai:jaxa.repo.nii.ac.jp:00016757,
 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 = {宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium},
 month = {},
 note = {平成20年度宇宙輸送シンポジウム(2009年1月19日-20日, 宇宙航空研究開発機構宇宙科学研究本部), With the aims of realizing hypersonic aircraft and reusable space transportation systems, researches are being carried out at Muroran Institute of Technology, for creation of innovative fundamental technologies for flying at high speeds in the atmosphere. Such technologies will be validated by flight experiments using a small scale unmanned supersonic plane. Its aerodynamic configuration is designed and analyzed by wind-tunnel tests. A preliminary airframe is being constructed for the initial phase of subsonic flight tests. In addition, test facilities such as a supersonic wind tunnel, a flight simulator, and a high-speed sled track, are being prepared for various ground verification., 形態: カラー図版あり, 資料番号: AA0064292064},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)},
 title = {FTBとしての小型超音速飛行実験機の構想と予備的な亜音速機の試作},
 volume = {平成20年度},
 year = {2009}
}