SUPERSONIC GUIDED MISSILE Russian patent published in 2024 - IPC F42B15/00 

Abstract RU 2821940 C1

FIELD: rocketry.

SUBSTANCE: supersonic guided missile, made according to the aerodynamic configuration "canard", contains a body, aerodynamic rudders located in the nose part, and a stabilizer with opening blades, which root chord is parallel to the body generatrix in the place of their location. Span of aerodynamic rudders is related to span of stabilizer by certain ratio depending on length and caliber of supersonic guided missile. Stabilizer blades have symmetrical sharpening of front and rear edges. Distance between the initial position of the center of mass of the missile and the position of the center of mass on the passive section of the trajectory does not exceed two calibers. Rudder end chord length is 0.4... 0.7 of the rudder root chord length.

EFFECT: high stability of the missile in flight, reduced drag and, accordingly, high accuracy when the missile approaches the target.

1 cl, 2 dwg

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RU 2 821 940 C1

Authors

Astashov Vladislav Sergeevich

Belobragin Boris Andreevich

Nasenkov Igor Georgievich

Petrov Igor Pavlovich

Dates

2024-06-28Published

2023-05-10Filed