固体推进剂体积模量主曲线试验研究

推进技术 ›› 1995, Vol. 16 ›› Issue (2): 67-72.

固体推进剂体积模量主曲线试验研究

高鸣,赵伯华

海军驻航天工业总公司２１０所军事代表室;北京理工大学飞行器工程系;海军驻航天工业总公司２１０所军事代表室;北京理工大学飞行器工程系

发布日期:2021-08-15

AN EXPERIMENTAL STUDY ON THE MASTER CURVE OF THE BULK MODULUS OF SOLID PROPELLANT

Dept.of Flight Vehicle Engineering, Beijing Inst.of Technology, Beijing,100081;Dept.of Flight Vehicle Engineering, Beijing Inst.of Technology, Beijing,100081

Published:2021-08-15

摘要/Abstract

摘要： 采用非接触测量体积模量系统，测出了复合固体推进剂在不同温度下的体积松驰模量和体积蠕变柔量，并依据时间－温度等效原理迭加拟合求得了体积模量主曲线和温度移动因子的数学表达式，其结果可为发动机药柱结构完整性分析提供依据。

关键词: 固体推进剂;体积弹性模量;蠕变分析

Abstract: The bulk relaxation modulus and bulk creep compliance of solid propellant at different temperatures are measured by a self-designed contactless measurement system, and the corresponding mathematical expressions of the master cure for bulk modulus are also given. The results are of practical significance to motor grains in structural integrity analysis.

Key words: Solid propellant;Bulk modulus;Creep analysis

高鸣,赵伯华. 固体推进剂体积模量主曲线试验研究[J]. 推进技术, 1995, 16(2): 67-72.