FIELD: aviation.
SUBSTANCE: low-temperature plasma electrochemical generator for ignition, stabilization and optimisation of supersonic combustion chamber includes thermochemical reactor with nozzle for feeding gas with chemically active component. Thermochemical reactor is docked with supersonic combustion chamber. Generator is equipped with a plasmatron, serially connected with the thermochemical reactor.
EFFECT: invention provides reliable ignition, as well as stabilisation of combustion of hydrocarbon fuels in straight supersonic combustion chambers.
1 cl, 1 dwg
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