FIELD: chemistry.
SUBSTANCE: invention describes supersonic combustion ramjet fuel based on a mixture of hydrocarbon fuel T-10 and 1,7-dimethyldicarba-closo-octocarborane, wherein the mixture further includes a combustion promoter - tert-butyl hydroperoxide, with the following composition, wt %: 1,7-dimethyldicarba-closo-octocarborane 70, fuel T-10 29-29.5, tert-butyl hydroperoxide 0.5-1.
EFFECT: obtaining supersonic combustion ramjet fuel with high energy output and improved combustion properties in the combustion chamber.
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