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Algorithms of automatic monitoring of the parameters of the electric rocket propulsion system are considered. The informative features of the subsystems of the electric rocket propulsion systems and the nature of their changes in the process of operation of the propulsion system are determined. The algorithms for detecting jump-like changes in informative features for different…

The results of numerical simulation of the process of motion of ions of a working mass in the accelerating channel of a stationary plasma engine SPD-70 on the basis of a direct numerical solution of the kinetic equation of rarefied plasma in an accelerating electrostatic field are presented. Introduction.  Formulation of the research task The…

The results of development and calibration of flow rate control units for gaseous propellants (argon, xenon, etc.) for laboratory testing of Hall thrusters are presented. The developed units allow for the independent supply of gaseous working substances to the anode unit and the hollow cathode. The units of flow control are based on the industrial…