@inproceedings{oai:jaxa.repo.nii.ac.jp:00007912,
 author = {中上, 禎章 and 丸, 祐介 and 森, 初男 and 稲谷, 芳文 and Nakaue, Yoshiaki and Maru, Yusuke and Mori, Hatsuo and Inatani, Yoshifumi},
 book = {第32回宇宙エネルギーシンポジウム, 32nd ISAS Space Energy Symposium},
 month = {Mar},
 note = {第32回エネルギーシンポジウム (2013年3月1日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県, The Space Energy Symposium (March 1, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, The Integrated Propulsion and Energy System (IPES) is an advanced energy system for space transportation vehicle to operate like an airplane and to reduce cost and turn around time by using as less number of components as possible. In this paper, I will introduce the method to design the propulsion and energy system considered about the integration of functions and components. And I also apply this method to future space missions and discuss how influence the IPES to some evaluate terms such as mass, cost, and turn-around-time for reusable rocket., 形態: カラー図版あり, 形態: PDF, Physical characteristics: Original contains color illustrations, Physical characteristics: PDF, 資料番号: AA0061912006, レポート番号: SES-2012-006},
 publisher = {宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS), Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)},
 title = {宇宙往還機の統合推進エネルギーシステム設計と評価に関する研究},
 year = {2013}
}