FIELD: engines and pumps.
SUBSTANCE: invention describes the fuel for hypersonic athodyd based on T-10 hydrocarbon fuel. Note here that fuel containing 1.7-dimethyl dicarbo-closo-octocarboran at the following ratio of components, wt %: 1.7-dimethyl dicarbo-closo-octocarboran - 70, T-10 fuel - 30.
EFFECT: invariable physical-chemical properties in the wide temperature range.
1 tbl
Title | Year | Author | Number |
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SUPERSONIC COMBUSTION RAMJET FUEL | 2014 |
|
RU2571088C1 |
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RU2738300C1 |
DETONATION COMBUSTION PULSE-JET ENGINE | 1997 |
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HYBRID ROCKET TURBINE ENGINE | 1992 |
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RU2288207C1 |
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Authors
Dates
2015-02-20—Published
2013-12-10—Filed