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作 者:姜夕博[1] 饶国宁[1] 徐森[1] 姚淼[1] 马安鹏[1] 彭金华[1]
出 处:《爆炸与冲击》2014年第1期99-105,共7页Explosion and Shock Waves
摘 要:为了研究退役单基药的冲击起爆特性,参照GJB772A-97中卡片式隔板法实验方法,分别开展了退役单基药的连续爆速实验、冲击波感度实验及锰铜压力计实验,观测了其冲击起爆的爆轰建立过程,得到了临界隔板值以及临界起爆压力。在连续爆速实验中,隔板厚度为50mm时,观察到了退役单基药反应冲击波不断增长的过程,并在90mm处转变为爆轰;在冲击波感度以及锰铜压力计实验中,测得其临界隔板厚度为50~52mm,临界起爆压力为1.35~1.49GPa。对退役单基药的冲击起爆过程进行了数值模拟,结合三种实验的实验结果,标定了其点火增长模型反应速率方程参数。The continuous detonation velocity test, the shock wave sensitivity test and the critical initi- ation pressure test were developed, respectively, with reference to the GJB772A-97 card gap test. Based on the above tests, the detonation establishment process in the expired single-base propellant was investigated, and the critical gap thickness and the critical initiation pressure were obtained. In the continuous detonation velocity test, the building-up process of the reactive shock wave was ob- served at the PMMA gap thickness of 50 mm and it developed into a normal detonation at the PMMA gap thickness of 90 mm. The critical gap thickness was 50--52 mm obtained from the shock wave sen- sitivity test. And the critical initiation pressure was 1.35--1.49 GPa obtained from the critical initia- tion pressure test. According to the above tests, the numerical simulations were conducted to calibrate the parameters of the reactive rate equation in the ignition-and-growth model for the expired single- base propellant.
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