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2 172 730

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C1

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Application

2000102745/02, 2000-02-03

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Start date

2000-02-03

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Actual filing date

2000-02-03

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Published

2001-08-27

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Inventor

Talalaev A.P.Zhuravleva L.A.Ibragimov N.G.Chebukov G.I.Okhrimenko Eh.F.Kuz'Mitskij G.Eh.

(73)

Holder

Gosudarstvennoe Unitarnoe Predprijatie Nauchno-Issledovatel'Skij Institut Polimernykh MaterialovFederal'Noe Gosudarstvennoe Unitarnoe Predprijatie Permskij Zavod Im. S.M. Kirova

BALLISTITE-TYPE SOLID ROCKET FUEL Russian patent published in 2001 - IPC

Abstract RU 2172730 C1

FIELD: rocket fuels. SUBSTANCE: rocket fuel of invention is intended for use in various-destination systems: gas generators, gun-powder pressure accumulators, anti-tank controlled rocket systems, and others, which require fuels having, along with high energetic and performance characteristics, a complex of special properties, namely high purity of combustion products, improved combustion rate-pressure dependence, and reduced combustion rate. These objectives are achieved by using complex combustion rate regulator containing gamma-polyoxymethylene in combination with phthalic acid lead-copper salt or complex consisting of lead phthalate and copper oxide or their mixture with calcium carbonate at useful ratio of components. Use of indicated components provides fuel with level of characteristics meeting requirements of constructors: combustion rate at temperature 20 C and pressure 40 kg/sq. cm lies between 2.5 and 5.0 mm/s, and exponent in combustion rate low ranges from 0.5 to 0.316. EFFECT: improved working characteristics. 2 cl, 1 tbl

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RU 2 172 730 C1

Authors

Talalaev A.P.

Zhuravleva L.A.

Ibragimov N.G.

Chebukov G.I.

Okhrimenko Eh.F.

Kuz'Mitskij G.Eh.

Dates

2001-08-27—Published

2000-02-03—Filed

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