首页> 外国专利> METHOD AND DEVICE FOR USING WARHEADS RELEASED FROM A LAUNCHING VEHICLE TO COMBAT TARGETS IDENTIFIED ALONG THE FLIGHT PATH OF THE LAUNCHING VEHICLE

METHOD AND DEVICE FOR USING WARHEADS RELEASED FROM A LAUNCHING VEHICLE TO COMBAT TARGETS IDENTIFIED ALONG THE FLIGHT PATH OF THE LAUNCHING VEHICLE

机译:使用从发射车辆释放的战斗头打击发射车辆飞行路线上确定的目标的方法和装置

摘要

PCT No. PCT/SE95/01300 Sec. 371 Date Nov. 6, 1997 Sec. 102(e) Date Nov. 6, 1997 PCT Filed Nov. 16, 1995 PCT Pub. No. WO96/15422 PCT Pub. Date May 23, 1996The present invention relates to a method and device for combating identified targets (F) using warheads (2) from a launching vehicle (1) flying over a target area, by separating from this launching vehicle (1) warheads (2) which act independently after separation, and including those targets which lie close to the flight trajectory of the launching vehicle (1) and those which lie well to the side of same flight trajectory. The invention is based on the use of that part of the kinetic energy of the launching vehicle (1) which the warhead (2) takes over from the same when it is separated in order to give the warhead (2) a looping trajectory or any other programmed flight trajectory, which carries it up to a starting height adapted to its active use, which lies considerably above the actual flight trajectory of the launching vehicle (1), and which, if so required, can carry the warhead (2) back to the geographical position where it was separated from the launching vehicle (1). The action of the warhead (2) can then follow guidelines known per se.
机译:PCT号PCT / SE95 / 01300秒371日期1997年11月6日第102(e),1997年11月6日,PCT,1995年11月16日,PCT公开。 WO96 / 15422 PCT公开号日期:1996年5月23日,本发明涉及一种方法和装置,该方法和装置通过使弹头(2)与飞弹(1)的弹头(2)分离,使用从飞越目标区域的弹头(1)的弹头(2)打击目标),它们在分离后独立发挥作用,包括那些靠近运载火箭(1)的飞行轨迹的目标和那些恰好位于同一飞行轨迹的侧面的目标。本发明基于以下用途:使用运载工具(1)的动能的一部分,当弹头(2)分离时,由弹头(2)接管该动能,以使弹头(2)具有环形轨迹或任何轨迹其他程序化的飞行轨迹,它将其携带到适合其实际使用的起始高度,该高度大大高于运载火箭(1)的实际飞行轨迹,并且如果需要,可以将弹头(2)返回到与运载火箭(1)分开的地理位置。然后,弹头(2)的动作可以遵循本身已知的准则。

著录项

  • 公开/公告号EP0793798B1

    专利类型

  • 公开/公告日2001-10-04

    原文格式PDF

  • 申请/专利权人 SAAB AB;

    申请/专利号EP19950937266

  • 申请日1995-11-16

  • 分类号F42B12/58;F42B10/60;

  • 国家 EP

  • 入库时间 2022-08-22 01:16:59

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