首页> 外国专利> Cruise missile and pilot parachute separating method for military transport plane, involves igniting cartouches to separate missile from extension platform and/or airdrop-pylon, when missile hangs vertically down to parachute in stable way

Cruise missile and pilot parachute separating method for military transport plane, involves igniting cartouches to separate missile from extension platform and/or airdrop-pylon, when missile hangs vertically down to parachute in stable way

机译:用于军事运输机的巡航导弹和飞行员降落伞的分离方法,涉及当导弹以稳定的方式垂直向下垂降到降落伞时,通过点火触碰将导弹与扩展平台和/或空投塔架分离。

摘要

The method involves presetting angle of rudder-machines of a cruise missile. Cartouches of pylons of an extension platform and/or airdrop-pylon are ignited to separate the missile from the platform and/or airdrop-pylon, when the missile hangs vertically down to a pilot parachute in a stable manner. The sequence for launching the missile-power drive is activated when a nosedive-maneuver of the missile is activated.
机译:该方法涉及预置巡航导弹的舵机角度。当导弹以稳定的方式垂直悬挂在降落伞上时,点燃扩展平台和/或空投塔的挂架,以将导弹与平台和/或空投塔分开。当启动导弹的俯冲操纵时,启动发射导弹动力驱动装置的程序。

著录项

  • 公开/公告号DE102004042989A1

    专利类型

  • 公开/公告日2006-03-09

    原文格式PDF

  • 申请/专利权人 GRABMEIER MICHAEL;

    申请/专利号DE20041042989

  • 发明设计人 GRABMEIER MICHAEL;

    申请日2004-09-06

  • 分类号B64D7/08;

  • 国家 DE

  • 入库时间 2022-08-21 21:20:43

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