FIELD: rocket fuels.
SUBSTANCE: invention provides solid rocket fuel containing plasticizer: nitroisobutyl trinitrate glycerol; oxidant: cyclotetramethylenetetranitroamine or hexanitrohexaazaisovurcitan, and/or hexanitrohexaazaadamantane, and/or ammoniodinitroamide; combustive component: dispersed aluminum and aluminum hydride; high-molecular binder: polybutadiene-nitrile rubber or polyurethane rubber; and process additives.
EFFECT: enabled preparation of low-smoke solid rocket fuel with high impulse and density, low sensibility to mechanical effects, and working temperature range between +50 and -50оС.
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Authors
Dates
2004-12-10—Published
2003-05-19—Filed