FIELD: military equipment; space equipment.;SUBSTANCE: invention is intended for use in combat space equipment for aircraft damage. Missile consists of body, damaging element and pyro charge for ejection of damaging element. Said body is coupled with body by multiple hinged parallelogram and additional multiple hinged parallelogram. Additional hinged parallelogram is installed perpendicular to main multiple hinged parallelogram. Damaging element is connected to an additional multiple hinged parallelogram. Target sensor is in form of a pin. Piezoelectric element is secured at its end. It is configured to generate electric current at impact for the purpose of pyro charge explosion initiation.;EFFECT: increase of destructive ability.;3 cl, 3 dwg
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