摘要
本文从燃烧室压力、系统工作循环方式以及最大推力三个方面叙述了世界各国液体火箭发动机的技术水平。简单介绍了世界各国液体火箭发动机技术发展的趋势及中国的最新进展,分析了中国液体火箭发动机技术发展的可能前景。
This paper presents the development of the liquid propellant rocket engine technology from the viewpoint of combustion chamber pressure, thrust level and power cycle. The progress of rocket engine development in China is reviewed. Finally, the future development of liquid propellant rocket engine in China and other countries is discussed.
出处
《导弹与航天运载技术》
1993年第6期15-25,共11页
Missiles and Space Vehicles
关键词
火箭发动机
液体推进剂
运载火箭
Rocket engine
Liquid propellant rocket engine
Launch vehicle
