JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
61912006.pdf310.68 kB
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
Other TitleStudy and evaluation of the Integrated Propulsion and Energy System for Reusable Rocket
Author(jpn)中上, 禎章; 丸, 祐介; 森, 初男; 稲谷, 芳文
Author(eng)Nakaue, Yoshiaki; Maru, Yusuke; Mori, Hatsuo; Inatani, Yoshifumi
Author Affiliation(jpn)東京大学大学院工学系研究科航空宇宙工学専攻; 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS); 株式会社IHI; 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)
Author Affiliation(eng)Department of Aeronautics and Astronautics, School of Engineering, The University of Tokyo; Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS); IHI Corporation; Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
Issue Date2013-03
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)
Publication title第32回宇宙エネルギーシンポジウム
32nd ISAS Space Energy Symposium
Publication date2013-03
Languagejpn
eng
AbstractThe 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.
Description会議情報: 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
形態: カラー図版あり
形態: PDF
Meeting Information: The Space Energy Symposium (March 1, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan
Physical characteristics: Original contains color illustrations
Physical characteristics: PDF
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会
SHI-NOAA0061912006
Report NoSES-2012-006
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/17734


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