GUIDED MISSILE Russian patent published in 1997 - IPC

FIELD: defence equipment, in particular, guided missiles having a canard aerodynamic configuration. SUBSTANCE: the missile has controls with a control actuator and a control system, cavities accommodating the controls are made on the missile external surface behind the frontal section before the forward points of the control-surface chords; the control-surface chords are positioned in the radial direction below the outer edge of the frontal section before the forward points of the control - surface chords; the rear part of the cavities bottom accommodating the controls may be connected to the missile external surface behind the controls over a smoothly rising surface. EFFECT: improved design. 2 cl, 3 dwg