首页> 外国专利> Self-propelling military projectile - has rocket portion at rear which separates after launching and head which descends vertically onto target

Self-propelling military projectile - has rocket portion at rear which separates after launching and head which descends vertically onto target

机译:自走式军事子弹头-火箭部分在后部,发射后分开,头部垂直下降到目标上

摘要

The rear end of the firework or missile assembly has a tapered secton (2) and fins (3) to give stable flight direction and the projective carries a charge appropriate to its use. At a determined point in its flight this can be fired and separation can take place. The missile carries a propulsive charge (13) and a methode of ensuring that the separated part and its charge, very quickly can fall in a vertical direction. The propulsive charge can be powder or gas. If of powder it is in the form of a block or variable section or it can be of several powders of different combustion speeds. The pyrotechnic charge is held in a case (12).
机译:烟火或导弹组件的后端具有锥形的第二部分(2)和鳍片(3),以提供稳定的飞行方向,并且射弹带有适合其使用的弹药。在其确定的飞行点上,可以将其发射并进行分离。导弹带有推进装药(13)和确保分离的部分及其装药能够非常迅速地沿垂直方向落下的方法。推进剂可以是粉末或气体。如果是粉末,则其为块状或可变截面的形式,或者可以是具有不同燃烧速度的几种粉末。烟火药被保存在箱子(12)中。

著录项

  • 公开/公告号FR2390704B1

    专利类型

  • 公开/公告日1980-02-29

    原文格式PDF

  • 申请/专利权人 RUGGIERI ETS;

    申请/专利号FR19770014767

  • 发明设计人

    申请日1977-05-13

  • 分类号F42B13/36;F42B13/40;

  • 国家 FR

  • 入库时间 2022-08-22 17:23:55

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