@inproceedings{oai:jaxa.repo.nii.ac.jp:00038607,
 author = {植田, 修一 and 加藤, 周徳 and 長谷川, 進 and 平岩, 徹夫 and Ueda, Shuuichi and Kato, Kanenori and Hasegawa, Susumu and Hiraiwa, Tetsuo},
 book = {第57回宇宙科学技術連合講演会講演集, Proceedings of 57th Space Sciences and Technology Conference},
 month = {Oct},
 note = {第57回宇宙科学技術連合講演会（2013年10月9日-11日. 米子コンベンションセンター（BiG SHiP）), 米子市, 鳥取県, Feasibility study on future transportation vehicle (termed as reference system) is undergoing at Japan AerospaceExploration Agency, setting the target on reusable, manned launch vehicles. Two-staged vehicle to low earth orbit is thefinal target of the current study, with hydrocarbon fuel (namely ethanol) in scope for easy and low-cost operation, andfiner system packaging due to high density. To compensate the Isp loss associated with usage of hydrocarbon fuel,airbreathing technology is fitted to the booster stage of the vehicle, i.e., application of a RBCC (Rocket Based CombinedCycle) engine. This engine is to embed rocket engines within a ramjet-duct, with various operation modes according toflight speed. Research activity has been conducted at JAXA to establish design methodology of this engine system withan emphasis on aerodynamic design with hydrogen as its fuel. Status of the research activity is herein reported., 資料番号: AC1400023000, レポート番号: JSASS-2013-4276},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences(JSASS)},
 title = {ロケット複合エンジンシステムにかかる技術研究状況について},
 year = {2013}
}