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IPC

(21) (22)

Application

98103793/02, 1998-03-16

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Actual filing date

1998-03-16

(45)

Published

1999-01-27

(72)

Inventor

Belobragin V.N.Gromov N.I.Gushchin V.A.Denezhkin G.A.Makarovets N.A.Obozov L.I.Petrov V.L.Podchufarov V.I.Semilet V.V.

(73)

Holder

Gosudarstvennoe Nauchno-Proizvodstvennoe Predprijatie

ROCKET Russian patent published in 1999 - IPC

Abstract RU 2125701 C1

FIELD: military equipment, rockets with gas dynamic control ( stabilization ) system, design of rocket projectiles for salvo firing systems. SUBSTANCE: rocket has cylindrical body with front conical part, rocket engine, empennage and gas dynamic system of angular stabilization with nozzles. Nozzles are made on cylindrical body at distance from front conical part equal to (0.1-0.15)L_cLk, where Lk is length of conical part of rocket. Cross-section area of nozzle of gas dynamic system of angular stabilization amounts to (0.008-0.017)L_cSm, where Sm is midsection area of rocket and length of conical part of body amounts to 2.3-2.5 diameter of cylindrical part of rocket body. Invention makes it possible to design rocket with stabilization characteristics of gas dynamic system of angular stabilization and to hit targets with high accuracy. EFFECT: high accuracy of target hitting. 1 cl, 1 dwg

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RU 2 125 701 C1

Authors

Belobragin V.N.

Gromov N.I.

Gushchin V.A.

Denezhkin G.A.

Makarovets N.A.

Obozov L.I.

Petrov V.L.

Podchufarov V.I.

Semilet V.V.

Dates

1999-01-27—Published

1998-03-16—Filed