FIELD: defense equipment, applicable in production of high-accuracy guided missiles and projectiles acting against ground, above-water and air targets.
SUBSTANCE: the guided missile has the main shaped charge, leading shaped charge, control surface bay positioned between them, blasting device with contact and non-contact target sensors, safety-actuating mechanisms of the main and leading charges, as well as with an electronic unit of blast delay. The non-contact target sensor is made of two AND circuits acting in the condition of coincidence of signals, based on different physical principles of action, one of the devices has a magnetometer as a sensitive element, determines the target type, and the second one of the optical type determines the time of the missile approach to the target to the preset ranges, the contact target sensor has an inertial-type sensitive element, whose actuation time depends on the value acting at the moment of collision of g-loads, and the electronic unit of blast delay is provided is a device for selection of the time delay values of supply of signals for blasting of the leading and main charges according to the preset algorithm, the algorithm is selected according to the data of the magnetometric transducer on the target type, and the values of delays are computed with due account made for the missile velocity determined according to the data on the difference of the time of missile approach to the target to the preset ranges.
EFFECT: enhanced efficiency of target hitting.
3 cl, 1 dwg
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Authors
Dates
2006-06-20—Published
2004-11-15—Filed