FIELD: process engineering.
SUBSTANCE: invention relates to electronics, optoelectronics and science of materials. Carbon powder is mixed with inert gas flow in mixing gas generator 8. Obtained mix is mixed with hydrocarbon rocket fuel flow and heated at outlet 17 of rocket or aircraft jet engine combustion chamber. Produced mix is directed into enclosed induction heating zone 4 to ignite it and generate plasma. Generated plasma jet is directed via nozzle unit 13 to cooled carbon black trap 10 arranged in independent accumulation tank 9.
EFFECT: higher efficiency.
12 cl, 1 dwg
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