FIELD: space engineering.
SUBSTANCE: electric propulsion systems with an electric rocket engine (ERE). A multichannel plasma engine contains a hemispherical gas-discharge chamber; at least two guide tubes; at least one antenna; high frequency current generator; at least two magnetic nozzles (according to the number of guide tubes); at least one power supply for magnetic nozzles; system of storage and supply of the working fluid; onboard power conversion module; control module.
EFFECT: eliminating losses due to the contribution of power to the devices for controlling the direction of plasma outflow and the need to use mechanical devices to change the orientation of the spacecraft.
2 cl, 4 dwg
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RU2568960C1 |
