BALLISTIC SOLID ROCKET PROPELLANT Russian patent published in 2010 - IPC C06B25/24 C06B23/00 C06D5/06 

FIELD: explosives.

SUBSTANCE: ballistic solid rocket propellant includes combustion modifying agent which consists of lead copper complex of phthalic acid or nickel lead complex of phthalic acid as combustion catalyst, chrome (III) - copper (II) - oxides or dioxides of titanium, or titanium disilicide, or calcium carbonate as combustion stabiliser, technical carbon and 1,2-dibutoxybenzol. Combustion catalyst is included in the propellant in quantity of 1.5-4.0 wt %, combustion stabilising agent 0.4 - 3.0 wt %, technical carbon 0.1 - 1.0 wt %, 1,2-dibutoxybenzol - 0.5 - 2.0 wt %.

EFFECT: low dependence of propellant combustion velocity on pressure, and increased propellant chemical durability.

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