GUIDED MISSILE Russian patent published in 2001 - IPC

Abstract RU 2166724 C1

FIELD: jet artillery ammunition. SUBSTANCE: the guided missile uses the canard configuration with air vanes. The nozzles of the cruise engine are located on the lateral surface of the missile body before the fin at a distance equal to two-three spans of one of its cantilevers from the leading-edge of the on-board chord. The diameter of the nozzle outlet section relates to the diameter of the throat section as 2.0...2.6:1.0. EFFECT: enhanced efficiency of missile guidance in the initial leg of flight. 8 dwg

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RU 2 166 724 C1

Authors

Shipunov A.G.

Morozov V.I.

Golomidov B.A.

Gusarov N.I.

Maksimov F.A.

Dates

2001-05-10—Published

2000-04-03—Filed