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2 170 910

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IPC

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Application

2000103008/02, 2000-02-10

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Start date

2000-02-10

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Actual filing date

2000-02-10

(45)

Published

2001-07-20

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Inventor

Trapeznikov P.I.Gilik G.B.Pygin A.F.Ivanov A.N.Denezhkin G.A.Podchufarov V.I.Filatov V.G.Peturkin D.M.Zakharov O.L.Kashirkin A.A.Obozov L.I.Sidjakov V.S.

(73)

Holder

Brjanskij Khimicheskij Zavod

ROCKET Russian patent published in 2001 - IPC

Abstract RU 2170910 C1

FIELD: jet salvo-fire systems. SUBSTANCE: the rocket has a nose, stabilizer assembly and a solid fuel engine. A cavity is formed in the engine between the front bottom and the front diaphragm. The diaphragm is made in the form of plates with holes, (0.01 to 0.015)D thick, and fastened between the front bottom and the engine body at a distance of (0.05 to 0.25)L from the front bottom, where D-inside diameter of the engine body in the point of installation of the front diaphragm, and L-length of the multiple-block charge. EFFECT: enhanced close grouping of shots and accuracy of fire. 1 dwg

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RU 2 170 910 C1

Authors

Trapeznikov P.I.

Gilik G.B.

Pygin A.F.

Ivanov A.N.

Denezhkin G.A.

Podchufarov V.I.

Filatov V.G.

Peturkin D.M.

Zakharov O.L.

Kashirkin A.A.

Obozov L.I.

Sidjakov V.S.

Dates

2001-07-20—Published

2000-02-10—Filed