FIELD: armament.
SUBSTANCE: the guided missile has in-line positioned control section with controls, acceleration engine, warhead, stabilizer unit in the form of flexible cantilevers, flare, booster engine and a coil of wire communication line. The flare in a clamp is positioned on the upper edge of the stabilizer cantilever for its folding under the cantilever when the missile is positioned in the launch tube and fixed by a latch. The stabilizer cantilever is provided with a folded hinge in the form of clamps. The movable part of the hinge is made in the form of a clamp with the flare fastened in its periphery, and a latch placed under it made in the form of a flat spring formed by a bent V-shaped plate.
EFFECT: enhanced accuracy of missile guidance, as well as enhanced its efficiency and reliability.
2 cl, 6 dwg
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