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Application

2000111674/06, 2000-05-10

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Start date

2000-05-10

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Actual filing date

2000-05-10

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Published

2002-09-27

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Inventor

Sokolovskij M.I.Sakov Ju.L.Zykov G.A.Ioffe E.I.Chudinov I.P.Zaritskij V.I.Karimov V.Z.Efremov G.A.Leonov A.G.Minasbekov D.A.Talalaev A.P.Kolesnikov V.I.Amarantov G.N.Shamraev V.Ja.Baranov G.N.Kuz'Mitskij G.Eh.Fedchenko N.N.Vronskij N.M.Lomaev V.I.Sirotkin A.K.

(73)

Holder

Otkrytoe Aktsionernoe Obshchestvo Nauchno-Proizvodstvennoe Ob"Edinenie

ROCKET SOLID-PROPELLANT ENGINE PLANT Russian patent published in 2002 - IPC

Abstract RU 2190112 C2

FIELD: rocketry. SUBSTANCE: proposed rocket solid-propellant engine plant includes separate combustion chambers with charge located inside them; one combustion chamber is located in one casing with central nozzle mounted on it and other combustion chamber is made in circular casing embracing the central nozzle at spaced relation. EFFECT: enhanced operational reliability at extended range of operation. 3 cl, 2 dwg

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RU 2 190 112 C2

Authors

Sokolovskij M.I.

Sakov Ju.L.

Zykov G.A.

Ioffe E.I.

Chudinov I.P.

Zaritskij V.I.

Karimov V.Z.

Efremov G.A.

Leonov A.G.

Minasbekov D.A.

Talalaev A.P.

Kolesnikov V.I.

Amarantov G.N.

Shamraev V.Ja.

Baranov G.N.

Kuz'Mitskij G.Eh.

Fedchenko N.N.

Vronskij N.M.

Lomaev V.I.

Sirotkin A.K.

Dates

2002-09-27—Published

2000-05-10—Filed

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