@inproceedings{oai:jaxa.repo.nii.ac.jp:00038774,
 author = {谷, 香一郎 and 森戸, 俊樹 and 植田, 修一 and 富岡, 定毅 and 齋藤, 俊仁 and 加藤, 周徳 and 小寺, 正敏 and 高㟢, 浩一 and Tani, Kouichiro and Morito, Toshiki and Ueda, Shuichi and Tomioka, Sadatake and Saito, Toshihito and Kato, Kanenori and Kodera, Masatoshi and Takasaki, Koichi},
 book = {第59回宇宙科学技術連合講演会講演集, Proceedings of 59th Space Sciences and Technology Conference},
 month = {Oct},
 note = {第59回宇宙科学技術連合講演会（2015年10月7日-9日. かごしま県民交流センター), 鹿児島市, 鹿児島県, A future space transportation requires a drastically economical system, such as a reusable vehicle and reusable vehicle needs a engine with much high specific impulse to support its heat-protected, heavy structure. A rocket-based combined cycle engine is one of the promising candidates to realized a high efficiency and has been studied for a decade in JAXA. As its operation cycles had been proved by series of experiments and analysis, JAXA has started planning a demonstration of the engine. Prior planning, a short term goal of the RBCC-powered vehicles was set and the technologies required for the vehicles were depicted. Three plans of the flight demonstrator were proposed and their capabilities for validation of each technology were examined. With supplemental ground tests in the wind tunnel, it was concluded that most of the technologies can be verified by the demonstrators though there are still many issues to be solved to realize such flight experiments., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AC1600032000, レポート番号: JSASS-2015-4449},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {RBCCエンジン実証手法の検討},
 year = {2015}
}