The University of Tokyo
The University of Tokyo
The University of Tokyo
The University of Tokyo
The University of Tokyo
The University of Tokyo
Japan Atomic Energy Agency (JAEA)
Japan Atomic Energy Agency (JAEA)
Japan Atomic Energy Agency (JAEA)
Japan Atomic Energy Agency (JAEA)
出版者
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)
出版者（英）
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
雑誌名
平成24年度宇宙輸送シンポジウム: 講演集録
雑誌名(英)
Proceedings of Space Transportation Symposium: FY2012
Space Transportation FY2012 (January 17-18, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan
抄録（英）
Microwave rocket is one of BEP (Beamed Energy Propulsion) systems. It is expected as a future low cost transportation system for large-scale infrastructure constructions like SSPS (Space Solar Power System). Microwave rocket can realize high payload ratio because it can use the atmospheric air as a propellant during its flight in atmosphere. However, a launch experiment with a kg class thruster was not conducted in the past study. The reason for this is impulse decrement due to refilling problem and low power density due to long distance beam transmission. In this study, these problems are resolved and the launch experiment with a kg class thruster is conducted.
内容記述
形態: カラー図版あり
形態: PDF
内容記述（英）
Translation title: Launch experiment results of kg class microwave rocket
Physical characteristics: Original contains color illustrations
Physical characteristics: PDF
kg級マイクロ波ロケットの打上げ実証実験報告
61856117.pdf
(552.09KB)
