Study on Failure Mechanism of Solid Propellant by the Drop

摘要：

We studied the failure mechanism of a double based propellant and a composite modified double base propellant by the overload machine of the drop hammer impact test. When the overload impact is more than 23000 g, we studied that the adiabatic compression blast of the air which between the gap of the charge and the mold is the inherent failure mechanism of the detonation.

作者: WANG Jiangning XIE Bo ZHENG Wei YUAN Zhifeng YAO Baoxue

作者单位: Xian Modern Chemistry Research Institute, East Zhangba Road, Xian 710065, China

会议类型: 国际会议

会议名称: 2011 International Autumn Seminar on Propellants,Explosives and Pyrotechnics(2011国际推进剂、炸药、烟火技术秋季研讨会)

会议地点: 南京

会议语种:英文

页码: 1002-1004

在线出版日期: 2011-09-20（万方平台首次上网日期，不代表论文的发表时间）