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Auxiliary charge for rocket launcher - has partition forming chamber ahead of launching member for extra acceleration

机译:火箭发射器的辅助装药-在发射器之前具有分隔形成室,以实现额外的加速

摘要

A rocket launching tube (a) open ends, contains a missile which includes a main charge (2) for sustaining its flight after launching and the warhead (1), and behind it is launching member with a discharge nozzle (8) at the rear, a launching charge (7) and an auxiliary charge (6) attached by a connector (9) to a partition (3) connected to the rear of the missile. After completion of firing of the launching charge which causes movement of the launching member along the tube, the auxiliary charge fires, giving extra acceleration of the missile, the connection (9) being severed, and the partition (3) forming a chamber for the auxiliary charge until the missile is launched.
机译:火箭发射管(a)的末端开口,装有一枚导弹,该导弹包括用于在发射后维持其飞行的主炸药(2)和弹头(1),在其后方是后部,后部带有排放喷嘴(8)发射装药(7)和辅助装药(6)通过连接器(9)连接到与导弹后部相连的隔板(3)。发射装药发射完成后,发射装药沿管子运动,辅助装药发射,使导弹额外加速,连接件(9)被切断,隔板(3)形成了一个用于发射的腔室。辅助弹药,直到导弹发射完毕。

著录项

  • 公开/公告号FR2260078B1

    专利类型

  • 公开/公告日1978-07-21

    原文格式PDF

  • 申请/专利权人 LUCHAIRE SA;

    申请/专利号FR19730024723

  • 发明设计人

    申请日1973-07-05

  • 分类号F41F3/00;

  • 国家 FR

  • 入库时间 2022-08-22 21:49:39

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