HYPERSONIC MISSILE Russian patent published in 2023 - IPC F42B15/00 

FIELD: weapons and ammunition.

SUBSTANCE: hypersonic missile. A hypersonic missile contains a body with a pointed nose, aerodynamic control surfaces, a jet engine and a stabilizer with deployable arcuate blades mounted on axles fixed in the cylindrical nose. The diameter of the nose of the rocket body in the middle of the side chord of the aerodynamic controls is made at least 0.3 of the full span of the aerodynamic controls and is 0.6…0.9 caliber of rocket. The side chord of the controls is made equal to 0.2…0.5 caliber of rocket, and the axis of rotation of each control is 0.40 from the leading edge of its side chord for 0.40…0.65 of its magnitude. The arcuate blades of the stabilizer are mounted with convex surfaces in the direction of rotation of the missile on a cylindrical nose with a diameter of 0.85…0.95 caliber of rocket. The span of the arcuate blades when open is 1.6…2.3 caliber of rocket.

EFFECT: improving aeroballistic characteristics and increasing shooting accuracy.

1 cl, 1 dwg