发明名称 Guided weapon with in-flight-switchable multiple fuze modes
摘要 A method for operating a guided munition with a switchable fuze arrangement includes launching the guided munition towards a target. During flight of the guided munition, images are provided to a remote operator, who supplies a switching input. Responsive to said switching input, the fuze arrangement is switched to either of at least two of the following states: a delayed detonation state in which detonation of the explosive charge is delayed by a time delay after impact of the guided munition, an impact detonation state in which detonation of the explosive charge occurs on impact of the guided munition, a proximity detonation state in which detonation of the explosive charge is triggered by a proximity sensing arrangement, and a disabled state in which the guided munition functions as a guided kinetic shell without detonation of the explosive charge.
申请公布号 US8689692(B2) 申请公布日期 2014.04.08
申请号 US20090918327 申请日期 2009.02.12
申请人 BRILL YARIV;NURIEL OHAD HANAN;RAFAEL ADVANCED DEFENSE SYSTEMS LTD. 发明人 BRILL YARIV;NURIEL OHAD HANAN
分类号 F42C9/14 主分类号 F42C9/14
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