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2 103 655

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C1

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IPC

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Application

95107009/02, 1995-04-28

(22)

Actual filing date

1995-04-28

(45)

Published

1998-01-27

(72)

Inventor

Tikhonov V.P.Zakharov L.G.Morozov V.I.Kopylov Ju.D.Golomidov B.A.Gusarov N.I.

(73)

Holder

Konstruktorskoe Bjuro Priborostroenija

GUIDED MISSILE Russian patent published in 1998 - IPC

Abstract RU 2103655 C1

FIELD: missile armament. SUBSTANCE: guided bank-spinning missile has control surfaces, stabilizer fin and a jet sustainer engine with side nozzles, with are installed with a shift towards missile bank spinning through a bank angle of 3 to 10 deg. relative to the plane of symmetry passing between the stabilizer fin cantilevers through the missile longitudinal axis. The distance between the stabilizer fin cantilevers and the side nozzles is determined from relation: X=L/tgα, where: X-distance between the stabilizer fin cantilevers and the side nozzles; L - span of one cantilever of the stabilizer fin; α - angle of inclination of side nozzles towards the missile longitudinal axis. EFFECT: improved design. 4 dwg

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RU 2 103 655 C1

Authors

Tikhonov V.P.

Zakharov L.G.

Morozov V.I.

Kopylov Ju.D.

Golomidov B.A.

Gusarov N.I.

Dates

1998-01-27—Published

1995-04-28—Filed

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