@inproceedings{oai:jaxa.repo.nii.ac.jp:00016597,
 author = {今村, 俊介 and 田口, 秀之 and 小島, 孝之 and 上野, 篤史 and 小林, 弘明 and 藤井, 啓介 and 廣谷, 智成 and 神吉, 誠志 and 土屋, 武司 and Imamura, Shunsuke and Taguchi, Hideyuki and Kojima, Takayuki and Ueno, Atsushi and Kobayashi, Hiroaki and Fujii, Keisuke and Hirotani, Tomonari and Kamiyoshi, Seiji and Tsuchiya, Takeshi},
 book = {宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium},
 month = {Jan},
 note = {平成21年度宇宙輸送シンポジウム(2010年1月14日-15日, 宇宙航空研究開発機構宇宙科学研究本部), Space Transportation Symposium (January 14-15, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)),  Sagamihara, Kanagawa Japan, JAXA are researching the HST(HyperSonic Transport aircraft) that is the goal of the hypersonic aircraft technology development. The purpose of this year's study are 1) Improvement of MDO(Multidisciplinary Design Optimization) precision.The MDO consists of aerodynamics and structure, thermal, propulsion, and so on. 2) Trade-off study about the figure of aircraft and cruising velocity, flight distance and so on. This paper shows the result of 1) Improvement of MDO precision., 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: AA0064741027},
 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 = {極超音速旅客機(HST)システム検討状況報告},
 volume = {平成21年度},
 year = {2010}
}