@inproceedings{oai:jaxa.repo.nii.ac.jp:00038615,
 author = {杵淵, 紀世志 and 齊藤, 靖博 and 西平, 慎太郎 and 更江, 渉 and 杉森, 大造 and 沖田, 耕一 and 谷, 直樹 and 梅村, 悠 and 小林, 弘明 and 姫野, 武洋 and 石川, 佳太郎 and 青山, 太一 and Kinefuchi, Kiyoshi and Saitoh, Yasuhiro and Nishihira, Shintaro and Sarae, Wataru and Sugimori, Daizo and Okita, Koichi and Tani, Naoki and Umemura, Yutaka and Kobayashi, Hiroaki and Himeno, Takehiro and Ishikawa, Keitaro and Aoyama, Taichi},
 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, Upper stages of H-IIA and H-IIB use LOX/LH2 as a propellant and achieve high performance and reliability. Utilizingthe experiences of cryogenic propellant management, the upper stage of H-IIA is now being upgraded for more efficientmass transfer. The propulsion system development is one of the most critical issues for the H-IIA Upgrade, and willsucceed CPS, Cryogenic Propulsion Stage, which is an element of the international exploration architecture for thein-space orbital transfer. Currently, CPS was scaled up to DUUS, Dual Use Upper Stage, and JAXA is now conducting acollaborative study with NASA. It is necessary to improve understanding of cryogenic propellant management to developDUUS, hence, JAXA focuses on not only vehicle development but also basic researches with universities and industries., 資料番号: AC1400031000, レポート番号: JSASS-2013-4163},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences(JSASS)},
 title = {基幹ロケット上段推進系の発展と国際有人探査への貢献　－極低温軌道間輸送機の研究開発－},
 year = {2013}
}