摘要
本文将液体火箭发动机的动力循环过程分为开式循环和闭式循环,并通过分析的办法,建立了发动机动力循环的效率公式.在这些公式的基础上,分析了影响液体火箭发动机循环效率的因素.本文所得的结果,对液体火箭发动机设计计算有一定的参考价值.
In this paper the power cycles of liquid propellant rocket engines are divided into open cycle and close cycle and analyzed.Through the analysis, formulae for the power cycle efficiency of liquid propellant rocket engines are set up.Based on those formulae, the factors effecting cycle efficiency of the rocket engines are also analyzed.The conclusions in this paper are for refference in the design calculation of the liquid propellant rocket engines.
出处
《推进技术》
EI
CAS
CSCD
北大核心
1989年第3期15-19,共5页
Journal of Propulsion Technology
关键词
液体推进剂
火箭发动机
热力学循环
能量转换
Liquid propellant rocket engine, Thermodynamic cycle, Energy conversion efficiency, System analysis
