Computer simulation of the jet of rarefied plasma outflowing from a nozzle of a plasma thruster
- Authors: Kotel’nikov V.A.1, Kotel’nikov M.V.1, Morozov A.V.1
-
Affiliations:
- Moscow Aviation Institute (National Research University)
- Issue: Vol 54, No 3 (2016)
- Pages: 303-307
- Section: Plasma Investigations
- URL: https://journals.rcsi.science/0018-151X/article/view/156774
- DOI: https://doi.org/10.1134/S0018151X1603007X
- ID: 156774
Cite item
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
Supplementary files
