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UDK: 662.311.1

2008. - V. 22. - N 4(84). - P. 56-61

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Influence of nickel carbonate and copper-lead phthalate on combustion of propellants with various caloric contents (from 2150 up to 4540 kJ/kg) is investigated. It is shown, that influence of these additives is very sensitive to change of propellant composition and pressure at which it burns. Nickel carbonate severely influences on combustion of low-caloric propellants (QL≤2700 kJ/kg), and maximal influence of copper-lead phthalate is displayed in combustion of propellant with QL=3000 – 4000 kJ/kg at pressure ~1 MPa.

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ВЛИЯНИЕ РАЗЛИЧНЫХ КАТАЛИЗАТОРОВ НА ГОРЕНИЕ ПОРОХОВ РАЗЛИЧНОЙ КАЛОРИЙНОСТИ

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