摘要
介绍液体火箭发动机采用大比推力对提高导弹经济性的作用。论述推进剂性质、燃烧室压力、氧化剂剩余系数对液体火资机动机比推力的影响及选用范围。
This paper describes the function of adopting large specific thrust for liquid rocket engine in improving the missile economy, and discusses the effection and selection of propellant feature combustion chamber pressure and residual oxidant coefficient specific thrust of liquid rocket engine.
出处
《洪都科技》
1995年第2期24-29,共6页
Hongdu Science and Technology
关键词
海防导弹
火箭发动机
比推力
液体推进剂
Coastal-defence missile Liquid rocket engine Specific thrust
