GUIDED MISSILE Russian patent published in 2002 - IPC

FIELD: guided jet ammunition. SUBSTANCE: the guided missile made according to the aerodynamic canard configuration has an engine with a front arrangement of the nozzles, self-oscillating control actuator located before the nozzles, and a signal-receiving device positioned in the plane of the missile rear end face. The control surfaces of the self-oscillating control actuator are unfolded in the plane perpendicular to the missile longitudinal axis, relative to the nozzles in the direction of missile spinning through a bank angle determined according to the relation given in the description of the innovation. EFFECT: enhanced accuracy of fire due to reduced smoke content in the optical communication line during engine operation on the flight path. 3 dwg