@inproceedings{oai:jaxa.repo.nii.ac.jp:00016465,
 author = {森本, 明 and 土屋, 武司 and 田口, 秀之 and Morimoto, Akira and Tsuchiya, Takeshi and Taguchi, Hideyuki},
 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, This paper describes conceptual studies on hypersonic experimental vehicle systems. In this research, we focus on studying the hypersonic experimental systems that provides test environment for precooled turbojet. The experiment aims to acquire engine operational data during the flight at speeds over Mach 4. We conducted flight dynamics simulations at different initial conditions and optimized the trajectories., 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: AA0065073018},
 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 = {最適設計手法による極超音速飛行実験機システム構想の検討},
 year = {2011}
}