@inproceedings{oai:jaxa.repo.nii.ac.jp:00016746,
 author = {白石, 裕也 and 山口, 敏和 and 小紫, 公也 and 小田, 靖久 and 梶原, 健 and 高橋, 幸司 and 春日井, 敦 and 坂本, 慶司 and Shiraishi, Yuya and Yamaguchi, Toshikazu and Komurasaki, Kimiya and Oda, Yasuhisa and Kajiwara, Ken and Takahashi, Koji and Kasugai, Atsushi and Sakamoto, Keishi},
 book = {宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium},
 month = {},
 note = {平成20年度宇宙輸送シンポジウム(2009年1月19日-20日, 宇宙航空研究開発機構宇宙科学研究本部), An experiment on Microwave Rocket under microwave repetitive pulse conditions has been conducted. In this research, 170 GHz high power gyrotron was used as a microwave source. Measured thrust by pressure gauge and load cell has a dependency on partial filling rate. And it discussed also about natural air-breathing in the thruster and flight mode. Therefore, thrust can become to be optimized., 資料番号: AA0064292053},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)},
 title = {前方吸気を想定した部分充填率によるマイクロ波ロケットの推力最適化},
 volume = {平成20年度},
 year = {2009}
}