防务技术2024,Vol.42Issue(12) :125-135.DOI:10.1016/j.dt.2024.06.012

Design,fabrication and performance test of an integrated exploding foil initiator system

Zehao Wang Pengfei Xue Qingxuan Zeng Mingyu Li
防务技术2024,Vol.42Issue(12) :125-135.DOI:10.1016/j.dt.2024.06.012

Design,fabrication and performance test of an integrated exploding foil initiator system

Zehao Wang 1Pengfei Xue 2Qingxuan Zeng 2Mingyu Li2
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作者信息

  • 1. State Key Laboratory of Explosion Science and Technology,Beijing Institute of Technology,Beijing,100081,China;Institute of Chemical Materials,China Academy of Engineering Physics,Mianyang,621900,China
  • 2. State Key Laboratory of Explosion Science and Technology,Beijing Institute of Technology,Beijing,100081,China
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Abstract

The integration method of exploding foil initiator system(EFIs)used to be researched to broaden its application range in military and aerospace in the last few decades.In order to lower the firing voltage below 1 kV,an integrated EFIs with enhanced energy efficiency was designed.Corresponding exploding foil initiator chips were fabricated in batch via micro electromechanical systems technology by inte-grating a unified foil,a flyer layer and a barrel on a glass substrate successively,meanwhile its package of the whole system was proposed at a volume of 2.194 cm3.The structural parameters were determined by predicted performance including flyer velocity,impact behavior and conduction property via the pro-posed theoretical models and the static electric field simulation.As expect,this integrated EFIs exhibited excellent functions,which could accelerate the flyer to a terminal velocity over 4 km/s and preeminently initiate HNS-IV pellet at a circuit of 0.24 μF/0.9 kV.Furthermore,the theoretical design,fabrication and performance test have been all included to validate the feasibility of this integrated EFIs that was beneficial for its commercial development in the future.

Key words

Exploding foil initiator system/Integration/Planar trigger switch/Micro electromechanical systems/Flyer velocity/Shock initiation

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出版年

2024
防务技术
中国兵工学会

防务技术

CSTPCD
影响因子:0.358
ISSN:2214-9147
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