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Interceptor projectile and method of use

机译:拦截弹和使用方法

摘要

An interceptor projectile includes a deployable net that deploys during flight and wraps around an incoming projectile, such as a rocket propelled grenade (RPG). The net is initially in a tubular body of the interceptor projectile. Weights are attached to ends of the net with metal cables. A propellant is used to deploy the net from the tubular body and to deploy the weights at acute angles to the longitudinal axis of the interceptor projectile. The weights move radially out from the interceptor projectile, expanding the net outward, and wrapping the net around an incoming projectile. The engagement of the net with the incoming projectile disables the incoming projectile, sending the incoming projectile off course.
机译:拦截弹丸包括可展开的网,该网在飞行过程中展开并包裹进来的弹丸,例如火箭榴弹(RPG)。该网最初位于拦截弹的管状体内。配重用金属电缆固定在网的末端。推进剂用于从管状主体中展开网,并使重物与拦截弹的纵轴成锐角。配重沿径向从拦截弹中移出,向外扩展网,然后将网包裹在进入的弹体周围。网与进入的射弹的啮合使进入的射弹失效,从而使进入的射弹偏离航向。

著录项

  • 公开/公告号US8387540B2

    专利类型

  • 公开/公告日2013-03-05

    原文格式PDF

  • 申请/专利权人 PAUL A. MEREMS;

    申请/专利号US20080189302

  • 发明设计人 PAUL A. MEREMS;

    申请日2008-08-11

  • 分类号F42B15/00;F41H11/04;

  • 国家 US

  • 入库时间 2022-08-21 16:43:00

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