兵工自动化2017，Vol.36Issue(7)：60-62,69,4.DOI:10.7690/bgzdh.2017.07.018
固体推进剂易损性试验研究
Vulnerability Experimental Study on Solid Propellant
王建灵 1刘海让 2杨建 1金朋刚1
作者信息
- 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
- 折叠
摘要
Abstract
The vulnerability experimental evaluation method study is the premise and base for safety use of high energy propellant. Establish 7 vulnerability test methods according to MIL-STD-2105C "non-nuclear hazard evaluation test", carry out vulnerability experiment for typical solid propellant, and acquire response features of typical solid propellant under different stimuli. The results show that the solid propellants have the selective under different stimuli, the same formula have the different response characteristics by different stimuli.关键词
固体推进剂/易损性/危险性/感度Key words
solid propellant/vulnerability/hazard/sensitivity分类
军事科技引用本文复制引用
王建灵,刘海让,杨建,金朋刚..固体推进剂易损性试验研究[J].兵工自动化,2017,36(7):60-62,69,4.
