论文部分内容阅读
液体火箭发动机采用高压补燃系统,可以最大限度地利用燃料的化学能,是第二代航天技术动力装置的发展方向.本文介绍了可贮存推进剂发动机高压补燃系统的特点和有关的技术问题.
Liquid rocket engine using high-pressure make-up system, can maximize the use of fuel chemical energy, is the second generation aerospace technology power plant development direction.This paper describes the characteristics and technical issues related to the high pressure combustion system can be stored propellant engine .