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2 096 734

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IPC

(21) (22)

Application

96109569/02, 1996-05-23

(22)

Actual filing date

1996-05-23

(45)

Published

1997-11-20

(72)

Inventor

Sokolovskij G.A.Afonin V.N.Vatolin V.V.Dorokhov A.I.Kapyrin Ju.M.Kegeles A.L.Makarovskij Eh.G.Mileshkin Ju.P.Oreliov G.R.Smol'Skij G.N.

(73)

Holder

Gosudarstvennoe Mashinostroitel'Noe Konstruktorskoe Bjuro

ROCKET WITH COMBINED CONTROL Russian patent published in 1997 - IPC

Abstract RU 2096734 C1

FIELD: rocket engineering. SUBSTANCE: rocket with combined control includes body, engine, guidance and control equipment, four aerodynamic vanes and immobile wings uniformly positioned over body relative to its longitudinal axis, gas dynamic control unit in the form of four interceptors placed diametrically for entry into gas stream after cut of nozzle of engine anchored on gas conduit of engine. Each interceptor is also installed in plane of arrangement of corresponding aerodynamic vane. Diametrically positioned interceptors are joined in pairs by means of cross-piece of two levers each kinematically coupled to autonomous drive. Mutually perpendicular rotation axes of levers cross in point located on longitudinal axis of rocket. EFFECT: enhanced efficiency of control over rocket. 5 cl, 6 dwg

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RU 2 096 734 C1

Authors

Sokolovskij G.A.

Afonin V.N.

Vatolin V.V.

Dorokhov A.I.

Kapyrin Ju.M.

Kegeles A.L.

Makarovskij Eh.G.

Mileshkin Ju.P.

Oreliov G.R.

Smol'Skij G.N.

Dates

1997-11-20—Published

1996-05-23—Filed