FIELD: rocket technics.
SUBSTANCE: invention relates to air-to-air missiles. Missile contains a fuselage, an engine and a homing head, as well as a detachable parachute placed in a drop cowling located in front of the missile's nose. Missile has a tail assembly mounted with the possibility to change its position relative to the center of mass of the missile and is located on a limited sliding sleeve on the fuselage of the rocket. Missile’s nose, its rudders and tail assembly have a very sharp leading edge. Tail assembly is fixed in the forward position, with the possibility of unfolding when zeroing.
EFFECT: invention makes it possible to control the direction of motion of the rocket.
3 cl, 2 dwg
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