火箭装药贮存寿命失效临界点的研究

推进技术 ›› 1996, Vol. 17 ›› Issue (3): 68-71.

火箭装药贮存寿命失效临界点的研究

赵伯华,高鸣

海军驻西安长峰机电研究所军代表室;海军驻西安长峰机电研究所军代表室

发布日期:2021-08-15
基金资助:
部级预研基金

STUDY ON CRITICAL SERVICE LIFE FOR ROCKET GRAIN

Navy Representative Office in Xi’an Chang Feng Electro-Mechanical Iust.Xi’an,710061;Navy Representative Office in Xi’an Chang Feng Electro-Mechanical Iust.Xi’an,710061

Published:2021-08-15

摘要/Abstract

摘要： 目前药柱贮存寿命失效临界点一般都是假设确定的。采用药柱空穴率非接触诊断技术和热加速老化累积损伤法，实测得ＣＭＤＢ固体推进剂的贮存寿命失效临界点，预测了其使用寿命。

关键词: 固体推进剂;热老化;贮存寿命;失效判据;累积损伤

Abstract: The critical service life for rocket grain was presumed at present.In this paper,with the aid of discontiguous diagnostic technology and method of accumulated damage using accelerated aging or heat air-oven the critical service life was determined and the service life for CMDB solid pram Pedant was predicted’The results in this paper are of practical significance for service life prediction of solid rocket grain.

Key words: Solid propellant;Heat aging;Storage life;Faiture criteria;Cumulative damage

赵伯华,高鸣. 火箭装药贮存寿命失效临界点的研究[J]. 推进技术, 1996, 17(3): 68-71.