首页> 外国专利> Explosive device for use in anti-aircraft/anti-radar missile, has spacing unit actuated by command issued by missile control unit to separate sector movable ends for inclining spark generator envelope with respect to longitudinal axis

Explosive device for use in anti-aircraft/anti-radar missile, has spacing unit actuated by command issued by missile control unit to separate sector movable ends for inclining spark generator envelope with respect to longitudinal axis

机译:用于防空/反雷达导弹的爆炸装置,具有由导弹控制单元发出的指令致动的间隔单元,用于将扇形可移动端分开,以使火花发生器外壳相对于纵轴倾斜

摘要

The device has an explosive load with two sectors surrounded by a spark generator envelope (11), where each sector has ends movable with respect to each other. A spacing unit (14) is actuated by a command issued by a missile control unit to separate the movable ends for inclining the envelope with respect to a longitudinal axis. An ignition device ignites the load that is actuated by another command issued by the control unit.
机译:该装置具有爆炸性负载,其两个扇区被火花发生器外壳(11)围绕,其中每个扇区的两端都可以相对移动。间隔单元(14)由导弹控制单元发出的指令致动,以使可动端分开,以使包膜相对于纵轴倾斜。点火装置点燃由控制单元发出的另一指令所致动的负载。

著录项

  • 公开/公告号FR2853726A1

    专利类型

  • 公开/公告日2004-10-15

    原文格式PDF

  • 申请/专利权人 THOMSON BRANDT ARMEMENTS;

    申请/专利号FR19900005078

  • 发明设计人 FERRON JOEL;WINAVER ANDRE;

    申请日1990-04-20

  • 分类号F42B12/22;F42B12/34;

  • 国家 FR

  • 入库时间 2022-08-21 22:39:10

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