FIELD: weapons.
SUBSTANCE: invention relates to military equipment, namely to guided missiles and missiles. Anti-aircraft guided missile comprises a body, a sustainer turbofan with an electric drive, an annular nozzle as a wing unit, steering surfaces with a span equal to the diameter of the nozzle, without the need for folding for transportation, guidance equipment based on inertial control system and optoelectronic homing head, special software for vertical or inclined start, remote fuse, safety actuator, warhead and current source. Rocket is made according to X-shaped aerodynamic configuration "canard". Missile is tightly placed in the transport-launch container and corrects the trajectory depending on the movement of the target.
EFFECT: simplified design, reduced weight, application both as part of portable air defence system, and as part of air defence system of group protection.
1 cl, 1 dwg
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