The experiments and the numerical simulations were carried out to investigate the characteristics in the initiation process of the TATB explosive by flyers.The initiation sequence was designed to initiate the high-density TATB explosive.The all-fiber displacement interferometer system for any reflector was used to measure the flyer velocities for the success and failure of the initiation in the TATB explosive, respectively.So the corresponding threshold flyer velocity was determined primarily.And the DYNA2Dprogram was employed to simulate the detonation process of the TATB explosive initiated by the flyer.The simulated results are consistent with the experiments.
Campos J, Duncombe R, Erkol S, et al. Explosive initiation by micro-slapper[C]//The 33th International Annual Conference of ICT. Karlsruhe: Fraunhofer-Institut fur Chemische Technologie, 2002: 1-10.
[2]
Prinse W C, van't Hof P G, Cheng L K, et al. High-speed velocity measurements on an EFI-system[C]//The 27th International Congress on High-speed Photography and Photonics. Xi'an: International Society for Optics and Photonics, 2007: 62795E-62795E-10.
[3]
He Bi, Long Xin-ping, Feng Chang-gen. Numerical simulation on shock-pulse initiation of submicron TATB[C]//The 25th International Symposium on Ballistics. Beijing, 2010: 749-758.
[4]
Tarver C M, McGuire E M. Reactive flow modeling of the interaction of TATB detonation waves with inert materials[C]//The 12th International Detonation Symposium. San Diego, 2002: 641-649.
[5]
Garcia M L, Tarver C M. Three-dimensional ignition and growth reactive flow modeling of prism failure tests on PBX 9502[C]//The 13th International Detonation Symposium. Norfolk, United States: Department of Energy, 2006.
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