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1 840 811

(13)

(51)

IPC

F02K9/26(2006-01-01)

(21) (22)

Application

1572572/06, 1973-12-04

(22)

Actual filing date

1973-12-04

(45)

Published

2010-12-27

(72)

Inventor

Pozdnjakov V.V.Podporina V.A.Gerasimov V.A.Baranov V.P.Kapitula R.I.Strukov S.I.Sukharev I.E.Baskakov O.N.Maksimov I.S.Morozov V.A.

SOLID PROPELLANT ROCKET ENGINE Russian patent published in 2010 - IPC F02K9/26

Abstract SU 1840811 A1

FIELD: weapons and ammunition.

SUBSTANCE: invention relates to the field of rocket engines operating on low-smoke solid propellant and intended for small-scale missiles controlled under conditions of direct optical visibility. Solid propellant rocket engine comprises the combustion chamber with nozzle unit, powder channel bomb of low-smoke composition, pyrotechnical igniter arranged at the side of the nozzle unit, coaxially to the bomb channel, and mixed solid propellant bomb. Mixed solid propellant bomb is arranged in the expanding part of channel near engine bottom.

EFFECT: invention makes it possible to provide for stable burning of powder channel bomb.

1 dwg

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SU 1 840 811 A1

Authors

Pozdnjakov V.V.

Podporina V.A.

Gerasimov V.A.

Baranov V.P.

Kapitula R.I.

Strukov S.I.

Sukharev I.E.

Baskakov O.N.

Maksimov I.S.

Morozov V.A.

Dates

2010-12-27—Published

1973-12-04—Filed