METHOD AND DEVICE FOR FEED OF PROJECTILE TO THE POINT OF DESTINATION Russian patent published in 2001 - IPC

FIELD: rocketry, applicable in launching of projectiles. SUBSTANCE: first the projectile is ejected from the barrel under the action of compressed air injected from the compressor, acceleration is imparted to it and its flight is ensured. The head air flow rotates the fins of the turbine installed on the rotor excitation windings of the generator and electric motor relative to the stator windings. Electric power is generated for rotation of the turbine through which the head air flow passes thus producing the reactive force. Means are provided for maneuver of the projectile in flight. The projectile is controlled from a ground radar set. EFFECT: reduced power consumption. 4 cl, 1 dwg