固体推进剂易损性试验研究  

Vulnerability Experimental Study on Solid Propellant

作　　者：王建灵[1] 刘海让 杨建[1] 金朋刚[1] Wang Jianling;Liu Hairang;Yang Jian;Jin Penggang(Xi’an Modern Chemistry Research Institute, Xi’an 710065, China;Dangerous & Explosion Department, Xi’an Municipal Public Security Bureau Public Security Sub-bureau,Xi’an 710065, China)

机构地区：[1]西安近代化学研究所,西安710065 [2]西安市公安局治安分局危爆科,西安710065

出　　处：《兵工自动化》2017年第7期60-62,69,共4页Ordnance Industry Automation

摘　　要：固体推进剂易损性评价方法研究是保证高能推进剂安全使用的前提和基础。根据美军标MIL-STD-2105C《非核弹药的危险性评估试验》建立的7种易损性试验方法,对典型固体推进剂进行易损性试验,得到典型固体推进剂在不同刺激下响应特性。结果表明:推进剂对于刺激源具有选择性,相同配方推进剂在不同刺激源下响应特性不同。The vulnerability experimental evaluation method study is the premise and base for safety use of high energypropellant.Establish7vulnerability test methods according to MIL-STD-2105C“non-nuclear hazard evaluation test”,carryout vulnerability experiment for typical solid propellant,and acquire response features of typical solid propellant underdifferent stimuli.The results show that the solid propellants have the selective under different stimuli,the same formulahave the different response characteristics by different stimuli.

关 键 词：固体推进剂 易损性 危险性 感度 

分 类 号：TJ510.6[兵器科学与技术—军事化学与烟火技术]