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2 380 346

(13)

C2

(51)

IPC

C06B25/24(2006-01-01)

C06D5/06(2006-01-01)

(21) (22)

Application

2008114589/02, 2008-04-14

(24)

Start date

2008-04-14

(22)

Actual filing date

2008-04-14

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Published

2010-01-27

(72)

Inventor

Ibragimov Nail' GumerovichZhuravleva Lidija AlekseevnaVshivkova Valentina IvanovnaMolchanov Vladimir FedorovichPechenkina Marija AleksandrovnaKoz'Jakov Aleksej Vasil'EvichKutsenko Gennadij Vasil'Evich

(73)

Holder

Federal'Noe Gosudarstvennoe Unitarnoe Predprijatie Institut Polimernykh Materialov"

BALLISTITE TYPE SOLID ROCKET PROPELLANT Russian patent published in 2010 - IPC C06B25/24 C06D5/06 

Abstract RU 2380346 C2

FIELD: chemistry.

SUBSTANCE: invention relates to ballistite type solid rocket propellant which can be used, for example in anti-tank guided missile systems. Ballistite solid rocket propellant contains nitrocellulose, plasticiser - nitroglycerin, dinitrotoluene and dinitrodiethyleneglycol, chemical resistance stabiliser - centralite or its mixture with diphenylamine, processing additives - industrial oil and zinc stearate, combustion catalyst - mixture of a lead-nickel complex of phthalic acid with calcium carbonate or magnesium oxide.

EFFECT: invention reduces dependency of fuel combustion rate on pressure in a pressure range below 40 kgf/cm2.

1 tbl

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RU 2 380 346 C2

Authors

Ibragimov Nail' Gumerovich

Zhuravleva Lidija Alekseevna

Vshivkova Valentina Ivanovna

Molchanov Vladimir Fedorovich

Pechenkina Marija Aleksandrovna

Koz'Jakov Aleksej Vasil'Evich

Kutsenko Gennadij Vasil'Evich

Dates

2010-01-27—Published

2008-04-14—Filed

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