日本航空宇宙学会論文集
Online ISSN : 2432-3691
Print ISSN : 1344-6460
ISSN-L : 1344-6460
研究ノート
大電力・高デューティ比作動によるマイクロ波ロケットの推力向上
小松 怜史山口 敏和小田 靖久齋藤 翔平福成 雅史小紫 公也梶原 健高橋 幸司坂本 慶司
著者情報
ジャーナル フリー

2012 年 60 巻 6 号 p. 235-237

詳細
抄録

Microwave Rocket is considered to be a future mass transportation system to space. Thrust is generated by high-pressure air isometrically heated by millimeter wave irradiation from the ground. High-power and high-frequency operation has been achieved mainly because of the improvement of a millimeter wave generator, gyrotron. Thrust was measured in a high-duty-cycle condition with a high-power millimeter wave. As a result, 30 N of time-averaged thrust was recorded at 91 kW of time-averaged power, which corresponds to 330 N/MW of thrust-to-power ratio.

著者関連情報
© 2012 The Japan Society for Aeronautical and Space Sciences
前の記事
feedback
Top