FIELD: rocket fuels. SUBSTANCE: rocket fuel of invention is intended for use in various-destination systems: gas generators, gun-powder pressure accumulators, anti-tank controlled rocket systems, and others, which require fuels having, along with high energetic and performance characteristics, a complex of special properties, namely high purity of combustion products, improved combustion rate-pressure dependence, and reduced combustion rate. These objectives are achieved by using complex combustion rate regulator containing gamma-polyoxymethylene in combination with phthalic acid lead-copper salt or complex consisting of lead phthalate and copper oxide or their mixture with calcium carbonate at useful ratio of components. Use of indicated components provides fuel with level of characteristics meeting requirements of constructors: combustion rate at temperature 20 C and pressure 40 kg/sq. cm lies between 2.5 and 5.0 mm/s, and exponent in combustion rate low ranges from 0.5 to 0.316. EFFECT: improved working characteristics. 2 cl, 1 tbl
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Authors
Dates
2001-08-27—Published
2000-02-03—Filed