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2 085 825

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C1

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IPC

(21) (22)

Application

95107196/11, 1995-05-11

(22)

Actual filing date

1995-05-11

(45)

Published

1997-07-27

(72)

Inventor

Beljaev V.N.Bogatskij V.G.Bychkov E.A.Vatolin V.V.Dreer D.L.Il'In A.M.Ishchenko V.V.Levishchev O.N.Lerner L.I.Maloletnev N.A.Pirjazev V.F.Pustovojtov V.A.Rejdel' A.L.Sokolovskij G.A.Fetisov V.K.Shmugljakov S.L.

(73)

Holder

Gosudarstvennoe Mashinostroitel'Noe Konstruktorskoe Bjuro

ROCKET WITH NORMAL AERODYNAMIC CONFIGURATION Russian patent published in 1997 - IPC

Abstract RU 2085825 C1

FIELD: rocket engineering. SUBSTANCE: invention refers to guided rockets and can be used in various types and classes of rockets with lattice control vanes. Rocket with normal aerodynamic configuration has immobile wings and mobile vanes uniformly arranged on body relative to longitudinal axis. Vanes are fitted with mechanisms for unfolding and securing. Rocket has pyrotechnical pressure accumulator. Lattice vanes are provided with pins to secure them in folded position. Each mechanism of unfolding of vane is manufactured in the form of pneumatic cylinder and each mechanism securing vane in unfolded position is made in the form of spring-loaded rods and in the form of gripping shears to keep vane in folded position. EFFECT: simplified design and improved functional reliability of rocket. 4 cl, 4 dwg

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RU 2 085 825 C1

Authors

Beljaev V.N.

Bogatskij V.G.

Bychkov E.A.

Vatolin V.V.

Dreer D.L.

Il'In A.M.

Ishchenko V.V.

Levishchev O.N.

Lerner L.I.

Maloletnev N.A.

Pirjazev V.F.

Pustovojtov V.A.

Rejdel' A.L.

Sokolovskij G.A.

Fetisov V.K.

Shmugljakov S.L.

Dates

1997-07-27—Published

1995-05-11—Filed

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