固体发动机推力随机调节的涡流阀方案研究

推进技术 ›› 1995, Vol. 16 ›› Issue (5): 34-39.

固体发动机推力随机调节的涡流阀方案研究

张为华,程谋森,刘分元

国防科技大学航天技术系;国防科技大学航天技术系;国防科技大学航天技术系

发布日期:2021-08-15

A STUDY ON VORTEX VALVE FOR THRUST RANDOM MODULATION OF SRM

Dept. of Aerospace Technology. NaTional Univ. of Defence Technology, Changsha,410073;Dept. of Aerospace Technology. NaTional Univ. of Defence Technology, Changsha,410073;Dept. of Aerospace Technology. NaTional Univ. of Defence Technology, Changsha,410073

Published:2021-08-15

摘要/Abstract

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。

关键词: 固体推进剂火箭发动机;推力控制;调制器;性能分析

Abstract: 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.

Key words: Solid propellant rocket engine;Thrust control;Modulator;Performance analysis

张为华,程谋森,刘分元. 固体发动机推力随机调节的涡流阀方案研究[J]. 推进技术, 1995, 16(5): 34-39.