ROCKET Russian patent published in 2006 - IPC F42B15/00 F42B10/60 

FIELD: armament.

SUBSTANCE: the rocket, made according to the standard aerodynamic configuration, has a body accommodating a homing head, control system equipment, contactless fuse, warhead, four control actuators, power supply system and an engine installation. Positioned on the body symmetrically relative to the longitudinal axis are two upper and two lower fixed wings and in tandem with them two upper and two lower aerodynamic control surfaces not linked kinematically with individual hinge axes and two lugs installed in the Vee between two upper wings. Two upper aerodynamic control surfaces are made folding so that their folded sections are turned about the axes perpendicularly to the axes of rotation of these control surfaces, and the wings and control surfaces are made so that they have correlations of the overall dimensions according to the need.

EFFECT: provided preservation of the lift qualities of the control surfaces within a wide range of variation of their span, preserved high maneuverability qualities of the rocket.

2 cl, 7 dwg