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1. 发明专利

DE69523064D1 未知
公开(公告)号：DE69523064D1
公开(公告)日：2001-11-08
申请号：DE69523064
申请日：1995-11-16
申请人： SAAB AB LINKOEPING
发明人： PERSSON PER-OLOF , PAULSSON LARS , JOHNSSON STIG
IPC分类号： F42B10/60 , F42B12/58
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.

2. 发明专利

DE69523064T2 未知
公开(公告)号：DE69523064T2
公开(公告)日：2002-07-11
申请号：DE69523064
申请日：1995-11-16
申请人： SAAB AB LINKOEPING
发明人： PERSSON PER-OLOF , PAULSSON LARS , JOHNSSON STIG
IPC分类号： F42B10/60 , F42B12/58
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.

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