@inproceedings{oai:jaxa.repo.nii.ac.jp:00016450,
 author = {平岩, 徹夫 and 富岡, 定毅 and 植田, 修一 and 齋藤, 俊仁 and 伊藤, 勝宏 and 谷, 香一郎 and Hiraiwa, Tetsuo and Tomioka, Sadatake and Ueda, Shuichi and Saito, Toshihito and Ito, Katsuhiro 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." The operation condition of the embedded rocket engine changes drastically in accordance with the engine operation mode. Status of research activity as well as its perspective including flight-tests for technology evaluation as milestone, is introduced 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: AA0065073003},
 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 = {JAXA におけるRBCC研究開発の現状と計画},
 year = {2011}
}