MISSILE Russian patent published in 2024 - IPC F42B15/10 F42B10/38 F42B10/16 

FIELD: military equipment.

SUBSTANCE: missile comprises a control system with aerodynamic rudders, a warhead, a jet engine with a nozzle, an aerodynamic stabilizer with a fairing and bearings between the fairing and the nozzle. The fairing is equipped with drop-down arched blades having a combined shape of the leading edges of the blades. The blades are installed at a zero nominal mean angle in the aerodynamic stabilizer to the longitudinal axis of the missile. The tolerance value for the average installation angle of the blades in the aerodynamic stabilizer does not exceed ± 0.33 degrees. The sharpening angle in the form of a wedge on the convex surface of the arcuate blades is made within 7° to 10° in a plane perpendicular to the leading edges of the arcuate blades.

EFFECT: increased reliability of the missile, improved aeroballistic characteristics, increased firing accuracy, preserved shape of the blade edges, reduced resistance of the stabilizer blades and aerodynamic rudders, and resonance-free flight with zero angles of attack.

1 cl, 3 dwg