@inproceedings{oai:jaxa.repo.nii.ac.jp:00016467,
 author = {富岡, 定毅 and 平岩, 徹夫 and 齋藤, 俊仁 and 植田, 修一 and 谷, 香一郎 and Tomioka, Sadatake and Hiraiwa, Tetsuo and Saito, Toshihito and Ueda, Shuichi and Tani, Koichiro},
 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, Research efforts on a rocket-based combined cycle engine are undergoing at JAXA Kakuda Space Center. The engine concept is to embed rocket engines within an air-breathing engine flow pass (i.e., a conversing-diverging duct). The engine operation is characterized due to vehicle speed, i.e., take-off to supersonic speed in "ejector-jet mode," supersonic to hypersonic in "ramjet mode," and hypersonic up to Mach 11 in "scramjet-mode." Flight tests are necessary to verify the ground test results, and also to verify control technique in accelerating environment. A flight test perspective is described in this presentation., 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: AA0065073020},
 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 = {極超音速エンジン向けFTB におけるRBCC 作動モード切替実証試験の検討},
 year = {2011}
}