FIELD: formation of instructions for activation of proximity fuze. SUBSTANCE: technical result of invention consists in simplified design of rocket and in diminished distance error of initiation of explosive charge from surface of target. While target and rocket are simultaneously positioned in controlling field of laser beam there are formed in it additional control channels through which distance difference from control unit to target and to rocket is constantly read. Signal for operation of fuze is automatically sent when this difference achieves value entered into control unit beforehand. EFFECT: simplified design of rocket and diminished distance error of initiation of explosive charge from surface of target.
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