FIELD: electricity.
SUBSTANCE: after creating an electric propulsion thrust in the fuel combustion mode at a pulsed pressure in a truncated spherical combustion chamber with the formation of a fire core in the combustion chamber and a plasma core in a magnetic field inductor under the action of a microwave field in the electron cyclotron resonance mode, and also creating a direct accelerating impulse voltage on the side of the cation accelerator located in front of the nozzle, the detonation combustion mode in the pulse mode, at which a stable detonation wave is formed in the fire core due to the pulse stream ionization-thermal cation waves from the plasma core, is additionally provided by creating an inverse accelerating pulse voltage on the side of the isolated electrode installed in the combustion chamber. The flow of ionization-thermal cation waves under the action of the reverse accelerating voltage and the flow of combustion products under the action of direct accelerating voltage is affected by a magnetic field whose induction vector coincides with the velocity vector of these flows.
EFFECT: invention allows to increase the specific thrust, efficiency coefficient and efficiency of energy conversion of fuel combustion products into electric power.
3 cl, 1 dwg
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Authors
Dates
2017-11-17—Published
2016-04-25—Filed