Computer simulation of the jet of rarefied plasma outflowing from a nozzle of a plasma thruster
- Авторы: Kotel’nikov V.A.1, Kotel’nikov M.V.1, Morozov A.V.1
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Учреждения:
- Moscow Aviation Institute (National Research University)
- Выпуск: Том 54, № 3 (2016)
- Страницы: 303-307
- Раздел: Plasma Investigations
- URL: https://bakhtiniada.ru/0018-151X/article/view/156774
- DOI: https://doi.org/10.1134/S0018151X1603007X
- ID: 156774
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Аннотация
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.
Об авторах
V. Kotel’nikov
Moscow Aviation Institute (National Research University)
Email: Mvk_home@mail.ru
Россия, Moscow
M. Kotel’nikov
Moscow Aviation Institute (National Research University)
Автор, ответственный за переписку.
Email: Mvk_home@mail.ru
Россия, Moscow
A. Morozov
Moscow Aviation Institute (National Research University)
Email: Mvk_home@mail.ru
Россия, Moscow
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