@inproceedings{oai:jaxa.repo.nii.ac.jp:00004378,
 author = {福成, 雅史 and 山口, 敏和 and 葛山, 浩 and 小紫, 公也 and 荒川, 義博 and Fukunari, Masafumi and Yamaguchi, Toshikazu and Katsurayama, Hiroshi and Komurasaki, Kimiya and Arakawa, Yoshihiro},
 book = {宇宙航空研究開発機構特別資料: 第43回流体力学講演会: 航空宇宙数値シミュレーション技術シンポジウム2011論文集, JAXA Special Publication: Proceedings of 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011},
 month = {Mar},
 note = {第43回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2011 (2011年7月7日-8日. 早稲田大学国際会議場) 東京, 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 (July 7-8,  2011. Waseda University, International Conference Center), Tokyo Japan, An air-breathing beamed energy propulsion rocket, "Microwave Rocket" has been proposed as a low cost launch system. The rocket is driven by a microwave beam radiated from the ground. Atmospheric air is used as a propellant in the pulsed engine. In order to improve its thrust performance, an air-breathing mechanism using reed values is under development. Ambient air is taken into the thruster through the reed valves. The air flow rate through the reed valves was computed and an air-breathing performance was evaluated in term of Partial Filling Rate, PFR. As a result, a 10 to 15-fold increase in thrust is predicted compared with the case without reed valves., 資料番号: AA0065207006, レポート番号: JAXA-SP-11-015},
 pages = {33--36},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {パルスデトネーション型マイクロ波ロケットのリード弁をもちいた吸気機構の解析},
 volume = {JAXA-SP-11-015},
 year = {2012}
}