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the projectile may be shot without reduction and without detonation

机译:弹丸可能会被射击而不会减少且不会爆炸

摘要

A projectile to be fired from a tubular or rail-shaped launcher has a warhead integral with a rearwardly extending tube of smaller diameter which contains a propulsive charge inserted between the warhead and a sabot carrying a frangible inertial mass. The rear end of the tube has a constricted opening which, upon detonation of the charge, retains the rearwardly moving sabot while giving passage to the disintegrating mass as the projectile is propelled forwardly. The propulsion gases evolving within the tube are temporarily retained by one or more heat-destructible plugs in the sabot and/or in the tube which melt, burn or char to allow the delayed escape of the gases whereby an in-flight thrust is imparted to the projectile.
机译:从管状或轨​​道形发射器发射的弹丸具有一个弹头,该弹头与较小直径的向后延伸的管成一体,该管包含插入弹头和携带易碎惯性质量的木bot之间的推进装药。管子的后端有一个狭窄的开口,在装药爆炸时,它保持向后移动的木bot,同时当弹丸向前推进时,使分解的物质通过。在管内逸出的推进气体被一个或多个可热破坏的塞子暂时保留在木/和/或管子中,该塞子熔化,燃烧或烧焦,以允许气体延迟逸出,从而将飞行中的推力施加到弹丸。

著录项

  • 公开/公告号BE893645A

    专利类型

  • 公开/公告日1982-10-18

    原文格式PDF

  • 申请/专利权人 RHEINMETALL G.M.B.H.;

    申请/专利号BE19826047676

  • 发明设计人 M. MOLL;W. GROSSWENDT;W. BECKER;

    申请日1982-06-24

  • 分类号F42B;

  • 国家 BE

  • 入库时间 2022-08-22 13:56:06

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