摘要
介绍了一种固体发动机推力大小随机调节实现的方案──涡流阀方案,导出了涡流间调节性能的相似准则方程;对涡流闹调节固体发动机静态特性和影响调节性能的各种主要因素进行了分析;指出了提高调节性能的途径,计算了模型发动机的推力调节。
In this paper a thrust random maculation of solid rocket motor which is called vortex valve modulation is introduced. The similarity criterion equations of vortex valve modulation performances are obtained, and static characteristics of SRM modulated by vortex valve are also analyzed. The major factors which effect modulation performances and the way how to improve maculation performances for SRM are shown. The thrust maculation performance calculation for a model SRM is conducted. The results are of great reference value to design of vortex valve modulation.
出处
《推进技术》
EI
CAS
CSCD
北大核心
1995年第5期34-39,共6页
Journal of Propulsion Technology
关键词
固体推进剂
火箭发动机
推力控制
调制器
喷管
Solid propellant rocket engine, Thrust control, Modulator, Performance analysis