FIELD: chemistry.
SUBSTANCE: invention describes fuel for hypersonic straight-jet engine based on a mixture of hydrocarbon fuel T-10 and 1,7-dimethyl dicarbo-closo-octocarborane, wherein mixture further includes a combustion promoter isopropyl nitrate, with following ratio (wt%): 1,7-dimethyl dicarbo-closo-octocarborane - 70; fuel T-10 - 29-29.5; isopropyl nitrate - 0.5-1.
EFFECT: technical result consists in creation of fuel for hypersonic straight-jet engine with high energy output, with improved conditions of its combustion in combustion chamber.
1 cl, 1 ex
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