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2 045 741

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IPC

(21) (22)

Application

92001916/23, 1992-10-23

(22)

Actual filing date

1992-10-23

(45)

Published

1995-10-10

(72)

Inventor

Arkhangel'Skij I.I.Beljavskij S.P.Bolotov E.G.Grushin P.D.Kaloshin Ju.G.Mizrokhi V.Ja.Mikheev V.P.Svetlov V.G.Stanevskij G.A.

(73)

Holder

Mashinostroitel'Noe Konstruktorskoe Bjuro

METHOD OF ROCKET CONTROL AND DEVICE FOR ITS ACCOMPLISHMENT Russian patent published in 1995 - IPC

Abstract RU 2045741 C1

FIELD: aerospace vehicles control. SUBSTANCE: for turn of rocket on target and simultaneous roll control use is made of total thrust of jet efflux acting in the same direction as aerodynamic force of the control surface. It provides for a quick turn of the rocket on target thus decreasing the response time and final miss. Control is accomplished by a combination antireaction device, having gas source 1 positioned in rocket body 2, aerodynamic control surfaces 6 and gas distributors located in the body of each control surface 6, and deflected with the aid of common drive 8. EFFECT: facilitated procedure. 6 cl, 8 dwg

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RU 2 045 741 C1

Authors

Arkhangel'Skij I.I.

Beljavskij S.P.

Bolotov E.G.

Grushin P.D.

Kaloshin Ju.G.

Mizrokhi V.Ja.

Mikheev V.P.

Svetlov V.G.

Stanevskij G.A.

Dates

1995-10-10—Published

1992-10-23—Filed