SPACECRAFT CORRECTING PROPULSION SYSTEM Russian patent published in 2024 - IPC B64G1/26 F03H1/00 

FIELD: cosmonautics.

SUBSTANCE: invention relates to space engineering, particularly to low-thrust plasma engines. Correcting ablation propulsion system of the spacecraft comprises a solid working medium, two working channels, cathodes and anodes, an end insulator, dielectric blocks, an energy accumulation unit and two electric discharge initiation units, a control system and a voltage converter. Electric discharge initiation units consist of a resistor, a capacitor, a controlled switch and a pulse transformer.

EFFECT: increasing the reliability of the plasma correcting propulsion system of a spacecraft.

1 cl, 2 dwg