GUIDED MISSILE Russian patent published in 2004 - IPC

FIELD: armament, in particular, small-sized anti-tank guided missiles, mainly with subsonic and transonic speeds, applicable in structures with various aerodynamic configurations.

SUBSTANCE: the missile has a canard configuration. The missile has a cylindrical body with a tail section narrowing in diameter and a nose section with a fairing, a fin with cantilevers folding to the side surface. The control surface is installed on the fairing of the nose section. A cone fairing with an angle of inclination of the generating line to the missile longitudinal axis not exceeding 20 dwg. Is made between the body cylindrical and tail sections. The body cylindrical-to-tail section ratio makes up 1:0.6 to 0.8. A flat surface, whose length equals the root chord may be made on the fairing of the missile nose section. The width of the flat surface is determined by a certain dependence.

EFFECT: enhanced efficiency of missile control.

2 cl, 6 dwg