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2 167 384

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IPC

(21) (22)

Application

2000103009/02, 2000-02-10

(24)

Start date

2000-02-10

(22)

Actual filing date

2000-02-10

(45)

Published

2001-05-20

(72)

Inventor

Gushchin V.A.Petrov V.L.Van'Kov V.T.Makarovets N.A.Denezhkin G.A.Semilet V.V.Aljazhedinov V.R.Bondarenko V.I.Zhogov V.A.Peturkin D.M.Filatov V.G.Eremeev N.I.

(73)

Holder

Novosibirskij Zavod Iskusstvennogo Volokna

MISSILE Russian patent published in 2001 - IPC

Abstract RU 2167384 C1

FIELD: rocketry. SUBSTANCE: missile has a warhead with a bottom piston, rocket engine with a stabilizing fin and leading pins, control system unit with a separation connector. Made between the rocket engine and warhead on the body is a stiffness unit in the form of a cylinder with a wall thickness equal to 2.0 to 6.0 of the wall thickness of the missile body and a length of 0.3 to 1.5 of its caliber with fastened supporting disk. The cavity formed by the supporting disk and bottom piston of the warhead accommodates the separation powder charge and the regulator of the dynamic and frequency responses. The regulator has a set of similar in dimensions of metal and nonmetal plates, whose total number is invariable. The control system unit is rigidly attached to the warhead by coupling members closed from the outside by an aerodynamic fairing. EFFECT: enhanced close-grouping of shots and accuracy of fire, automatic joining of separation connector at loading. 4 dwg

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RU 2 167 384 C1

Authors

Gushchin V.A.

Petrov V.L.

Van'Kov V.T.

Makarovets N.A.

Denezhkin G.A.

Semilet V.V.

Aljazhedinov V.R.

Bondarenko V.I.

Zhogov V.A.

Peturkin D.M.

Filatov V.G.

Eremeev N.I.

Dates

2001-05-20—Published

2000-02-10—Filed