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Countermeasure apparatus for deploying interceptor elements from a spin stabilized rocket

机译:用于从自旋稳定火箭上部署拦截器元件的对策设备

摘要

There is provided a countermeasure defense system against hostile missiles directed against tanks and other military vehicles in battle zone that reduces the hazard to friendly military personnel in the zone that is produced at lower cost and whose mission is less complicated to implement by employing non-explosive intercepting ("NEI") elements 14 deployed by the spin stabilized rocket 10. The NEI are carried in a payload section 17 and contained by a slidable sleeve assembly 16 which is retracted by a drive mechanism 21 after a predetermined time delay programmed into the trigger release assembly 46 at the time of launch. The drive mechanism includes a drive rod 26 that is releasably held by a release mechanism 46 that actuates the compressed coiled spring unit 30 that urges the sleeve assembly 16 to move forward with the sleeve member 22 exposing the contents of the payload section to the centrifugal force of the spin stabilized rocket propelling the NEI elements out from the rocket at constant angular velocity creating an intercepter cloud of elements.
机译:提供了一种针对战场上的坦克和其他军车的敌对导弹的对策防御系统,该系统减少了对该地区友好的军事人员的危害,该区域的生产成本较低,并且通过采用非爆炸性武器实现的任务较简单由自旋稳定火箭10部署的拦截(NEI)元件14。NEI携带在有效载荷部分17中,并包含在可滑动的套筒组件16中,该套筒组件在经过预定时间延迟后被驱动机构21缩进扳机中在发射时释放组件46。该驱动机构包括驱动杆26,该驱动杆26由释放机构46可释放地保持,该释放机构致动压缩的螺旋弹簧单元30,该压缩的螺旋弹簧单元促使套筒组件16与套筒构件22一起向前移动,从而将有效载荷部分的内容物暴露于离心力。自旋稳定火箭的一部分以恒定角速度将NEI元素从火箭中推出,从而形成了元素拦截器云。

著录项

  • 公开/公告号IL121220D0

    专利类型

  • 公开/公告日1998-01-04

    原文格式PDF

  • 申请/专利权人 TRW INC.;

    申请/专利号IL19970121220

  • 发明设计人

    申请日1997-07-02

  • 分类号6F42BA;

  • 国家 IL

  • 入库时间 2022-08-22 02:57:39

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