发明名称 Guided munition unit with in-flight switchable multiple fuze modes
摘要 <p>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.</p>
申请公布号 IL189692(A) 申请公布日期 2014.07.31
申请号 IL20080189692 申请日期 2008.02.21
申请人 RAFAEL ADVANCED DEFENSE SYSTEMS LTD.;OHAD NURIEL;YARIV BRILL;SHLOMO AVIGDOR 发明人 OHAD NURIEL;YARIV BRILL;SHLOMO AVIGDOR
分类号 F42C 主分类号 F42C
代理机构 代理人
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