UNCONTROLLED MISSILE WITH ROTATION FROM ENGINE Russian patent published in 2020 - IPC F42B10/30 F42B12/26 

FIELD: weapons and ammunition.

SUBSTANCE: invention relates to ammunition, and more specifically to uncontrolled rockets, which are intended for use in salvo fire systems. Uncontrolled missile with rotation from engine, which is launched from tubular guides, comprises warhead, fairing, rocket engine located after warhead, including housing with distributor. Distributor is equipped with central chamber of preliminary mixing in form of hemisphere-combustion chamber, rigidly connected with sustainer nozzle, and peripheral combustion chambers having hemispherical shape inserted into external housing of combustion chamber, forming a ball joint through copper gaskets connected to nozzles, the axis of which is installed by the guide at screwing on the rear part of the projectile body. Angle of inclination is 0…45° to rocket body generatrix and 0…50° to tangential component of missile cross section. Along inner surface of warhead part of coil to wind steel wire is wound ∅6 mm, having 10-mm-long notches along the wire turn, inside which an explosive substance is filled.

EFFECT: longer flight range, higher stabilization on trajectory and killing force of projectile.

1 cl, 4 dwg