@inproceedings{oai:jaxa.repo.nii.ac.jp:00038600,
 author = {木村, 俊哉 and 佐藤, 正喜 and 吉田, 誠 and 石本, 真二 and Kimura, Toshiya and Sato, Masaki and Yoshida, Makoto and Ishimoto, Shinji},
 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, As one of future space transportation systems, a fully reusable TSTO system to LEO has been studied in JAXA. Severalpossible combinations for vehicles and engines of this TSTO system have been under consideration, As a propulsionsystem, an ordinary rocket engine, an aerospike nozzle engine, and a RBCC (Rocket Based Combined Cycle) engine aremain candidates. In this paper, we report the present status of our system study for the first and second stages of the TSTOsystem using an ordinary rocket engine. The concept of TDM (Total design management) is applied in the design of theengines in order to make the study efficient and to avoid unnecessary works when the system requirements to the enginewill be changed., 資料番号: AC1400016000, レポート番号: JSASS-2013-4274},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences(JSASS)},
 title = {再使用型TSTO 軌道往還輸送システムのロケット推進系システム検討},
 year = {2013}
}