FIELD: weapons and ammunition.
SUBSTANCE: anti-ship missile contains control system with inertial guidance system unit, missile internal control unit and target coordinator, ranging computer, threshold device, defensive payload with safety and arming unit, protective unit of top semi-sphere with beam pattern directed towards missile top semi-sphere and with carrying frequency of transmitted pulses and periods of their coming corresponding to the carrying frequency and period of transmitted pulses coming of anti-ship missile self-homing head, ejected dipole scatterers unit, unit OR and unit AND. Ejected dipole scatterers unit is made as a system of pyro-energy sensors the working surfaces of which are directed to front top semi-sphere. The inlet of ejected dipole scatterers unit is connected to the output of ranging computer through threshold device, unit OR, unit AND and top semi-sphere protective unit. The second input of unit OR is connected to the output of inertial guidance system, the second input of unit AND is connected to the output of missile internal control unit. Pyro-technical composition of pyro-energy sensors has dipole scatterers, the coating of which is made of high-melting metals. Protective unit of top semi-sphere is located in payload. Ejected dipole scatterers unit is located in the recess made in weapon body. Increase of efficiency of air defence zones overcoming by anti-ship missiles and effective use of released part of internal volume and mass of the missile in nuclear-powered version.
EFFECT: increase of efficiency of air defence zones overcoming by anti-ship missiles.
1 dwg
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Authors
Dates
2013-03-20—Published
2011-04-19—Filed