ANTIAIRCRAFT GUIDED MISSILE Russian patent published in 2008 - IPC F42B15/00 

FIELD: weapons and ammunition.

SUBSTANCE: missile contains case, impellent installation placed in it, control system equipment, fighting equipment, four folding aerodynamic flight controls and four folding stabilisers. The aerodynamic flight controls are established on a tail part of the case, and the stabilisers are placed before flight controls. The stabilisers are executed with the area, smaller than the area of flight controls, and rotary parts of stabilisers in the course of disclosing are executed with possibility of their shift along the case towards the flight controls.

EFFECT: reduction of mass and dimensions parametres at maintenance of demanded aerodynamic characteristics.

3 cl, 10 dwg