FIELD: military tech.
SUBSTANCE: invention applies to anti-aircraft missiles, and can be used in the development of guided missiles, anti-missile and ballistic missiles. The anti-aircraft missile contains a warhead, aerodynamic control surfaces and an axisymmetric body. The body contains a rocket engine, control and power supply systems, four steering jet nozzles. These nozzles are located on aerodynamic control surfaces perpendicular to the building axis of the anti-aircraft missile. The regulator of gas flow through the steering jet nozzles is made according to the jet relay scheme. This jet relay is located on the axis of the aerodynamic control surface or on its lower chord.
EFFECT: improved dynamics of the rocket due to significant increase in the shoulder of the application of the missile control forces and insurance of joint action of aerodynamic and gas-dynamic control forces from one control unit.
1 cl, 1 dwg
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