@inproceedings{oai:jaxa.repo.nii.ac.jp:00038608,
 author = {富岡, 定毅 and 小寺, 正敏 and 加藤, 周徳 and 谷, 香一郎 and Tomioka, Sadatake and Kodera, Masatoshi and Kato, Kanenori and Tani, Kouichio},
 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 conTguration to lowearth orbit is the final target of the current study, while point-to-point high-speed transportation using the same vehicles isalso under consideration for near-term application. For long-range point-to-point transportation, system study on a RBCC(Rocket Based Combined Cycle) engine powered vehicle is undergoing, because a very high specific impulse is necessaryto make dry-weight to take-off weight ratio reasonable. This vehicle will be used for first stage (termed as booster) of theTSTO-RLV. Performance prediction on the RBCC engine was conducted to find that higher Isp including airframe dragthan that of rocket engines in vacuum was attained. System take-off weight analysis was conducted with simplifiedmethod by re-sizing the booster-stage vehicle while the orbiter-stage vehicle size / weight was fixed., 資料番号: AC1400024000, レポート番号: JSASS-2013-4275},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences(JSASS)},
 title = {TSTO ブースター段用空気吸込みエンジンシステム検討},
 year = {2013}
}