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A theoretical and experimental study of the electromagnetic environment surrounding a magnetic induction launcher

机译:电磁感应发射器周围电磁环境的理论和实验研究

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摘要

Electromagnetic (EM) field measurements were conducted near a prototype system that launches metal plates via EM induction. These plates are intended to augment a vehicle's passive armor by intercepting incoming kinetic energy (KE) projectiles some distance away from the vehicle. The subscale EM induction launcher consists of two 4.5-turn, 15 cm square spiral coils machined from 1.27 cm thick copper-beryllium plate. This type of system is designed to launch a 15 cm square aluminum plate in an edge-on orientation as was done for an earlier design (see W. Coburn, C. Le, and H. Martin, US Army Research Laboratory Report ARL-MR-206, April 1995), both the short-term magnetic fields associated with the launch process and the long-term electric fields associated with the flying plate were measured. A theoretical model designed to simulate the magnetic fields surrounding the launcher has been developed and its results compare favorably with measured data.
机译:电磁(EM)场测量是在原型系统附近进行的,该系统通过EM感应发射金属板。这些板块通过拦截与车辆相距一定距离的传入动能(KE)弹丸来增强车辆的被动装甲。超小型电磁感应发射器由两个4.5匝,15厘米见方的螺旋形线圈组成,该线圈由1.27厘米厚的铜铍板加工而成。这种类型的系统设计为可以像以前的设计那样沿边缘定向发射15厘米见方的铝板(请参阅W. Coburn,C。Le和H. Martin,美国陆军研究实验室报告ARL-MR -206,1995年4月),测量了与发射过程相关的短期磁场和与飞行板相关的长期电场。已经开发出一种用于模拟发射器周围磁场的理论模型,其结果与实测数据相比具有优势。

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