FIELD: weaponry.
SUBSTANCE: designs of hybrid ammunition. A hybrid jet guided munition, combining the properties of an aircraft and a missile, includes a body made according to the “tailless” aerodynamic design with a swept wing and elevons, at least one vertical fin with rudders, a battery and a control system with a homing module on target. The lower part of the body has fittings for attaching at least two 122 mm caliber shells for MLRS. The ammunition contains a system for simultaneous launching of projectile jet engines. Targeting is carried out by a homing module with the possibility of additional adjustment of target coordinates from an additional reconnaissance source.
EFFECT: possibility to fly ammunition at a low altitude, repeating the folds of the terrain, with control in height and direction for delivering targeted missile and bomb strikes against enemy targets.
3 cl, 2 dwg
