FIELD: means of destruction of armored targets. SUBSTANCE: prior to blasting of shaped charge 2 in rocket flight, metal facing 1 of the shaped-charge cavity is heated. Heat is supplied to the base of facing 1 over its end face 3. Heat supply cam be effected by means of heat carrier 4 from heat energy source 5. Material with a high thermal diffusivity is used as material of heat carrier 4. EFFECT: enhanced efficiency. 3 cl, 1 dwg
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