Computer simulation of the jet of rarefied plasma outflowing from a nozzle of a plasma thruster


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Abstract

Physical, mathematical and numerical models for the problem of the outflow of a jet of rarefied plasma from the nozzle of a plasma thruster of the cylindrical and rectangular shape have been considered. The main results of computation experiments have been presented: distribution functions of charged particles in the plasma flow, velocity and concentration fields of charged particles, and isolines of the potential of the self-consistent electric field.

About the authors

V. A. Kotel’nikov

Moscow Aviation Institute (National Research University)

Email: Mvk_home@mail.ru
Russian Federation, Moscow

M. V. Kotel’nikov

Moscow Aviation Institute (National Research University)

Author for correspondence.
Email: Mvk_home@mail.ru
Russian Federation, Moscow

A. V. Morozov

Moscow Aviation Institute (National Research University)

Email: Mvk_home@mail.ru
Russian Federation, Moscow

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