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ROCKET FOR GRENADE LAUNCHED BY GRENADE LAUNCHER

机译:榴弹发射器发射的榴弹火箭

摘要

FIELD: war material. SUBSTANCE: invention can be used designed of ammunition for grenade launchers. Proposed rocket contains housing, propelling charge and electric fuses. Propelling charge is arranged in stages divided by partitions, each consisting of combustion chambers divided by partitions and accommodating propelling charges and electric fuses. Combustion chambers are connected by electric circuit, and last combustion chamber serves as locking device. Number of stages is two minimum. Number of combustion chambers is two minimum. Stages are made for sequential connection. EFFECT: increased range and speed of grenades. 4 cl, 2 dwg
机译:领域:战争物资。物质:本发明可用于榴弹发射器的弹药设计。拟议的火箭弹包括机壳,推进装药和电熔丝。推进装药由隔板隔开,每级由隔板隔开的燃烧室组成,并容纳推进装药和电熔丝。燃烧室通过电路连接,最后一个燃烧室用作锁定装置。阶段数最少为两个。燃烧室的数量最少为两个。为顺序连接创建了阶段。效果:增加了榴弹的射程和速度。 4厘升,2公升

著录项

  • 公开/公告号RU2217618C1

    专利类型

  • 公开/公告日2003-11-27

    原文格式PDF

  • 申请/专利权人

    申请/专利号RU20020109521

  • 发明设计人 DENISOV V.A.;

    申请日2002-04-12

  • 分类号F02F1/00;

  • 国家 RU

  • 入库时间 2022-08-21 22:45:19

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