FIELD: weapons.
SUBSTANCE: invention relates to military equipment, particularly to accurate delivery of useful load, for example missiles with separating warheads, and can be used in air defense of military and civil objects. Proposed device comprises missile with stabilisation unit to allow axial missile rotation. Warhead separation assembly comprises uncoupling charge and pyro generator dynamically communicated, via gas path, with missile assembly and, via electric circuitry, with actuating assembly. Parachute compartment is furnished with parachute release mechanism rigidly fixed in parachute compartment head section with swivel attached to its bottom. Buoyancy device represents gas generator, inflatable enclosure mechanism of its release representing a piston coupled with sector casing. Aforesaid device is located between parachute compartment and useful load.
EFFECT: higher efficiency of air defense.
2 cl, 1 dwg
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