The design and verification of ignition universal measuring device in missile
According to the universal measuring device of igniter in missile flight testing, this paper proposed a designing method of cylindrical explosive container, considering from the aspects of container thickness, reflected overpressure, applied materials, container structure, explosive charge of igniter, and calculating the stress twinkling charge of cylindrical explosion container, and simulating the stress through COSMOSWorks software. In the end, the result is verified, and the working state of igniter is analyzed through the recycled data of missile flight testing. The result shows that the experimental result is keeping with the theoretical analysis, which means the container designing is reasonable, so that it provides the necessary data reference and support for the driving force device of trialed igniter in missile.
igniter cylindrical explosion container instantaneous load driving force device
Jiao Xin-quan Chu Cheng-qun Jia Xing-zhong Wang Ge Zhao Xin
National Key Laboratory for Electronic Measurement Technology North University of ChinaTaiyuan,China National Key Laboratory for Electronic Measurement Technology North University of China Taiyuan,Chin
国际会议
成都
英文
1-4
2010-08-20(万方平台首次上网日期,不代表论文的发表时间)