Nonstationary Model of a Low-Density Plasma Jet Ejected from a Stationary Plasma Thruster
- Autores: Bishaev A.1, Abgaryan M.2, Kim V.2, Merkur’ev D.2, Ivanova E.3, Fomenkov A.3, Wartelski M.4, Theroude C.4
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Afiliações:
- Moscow Institute of Physics and Technology
- Research Institute of Applied Mechanics and Electrodynamics
- Airbus Group Innovations
- Airbus Defense and Space SAS
- Edição: Volume 44, Nº 2 (2018)
- Páginas: 278-288
- Seção: Plasma Accelerators
- URL: https://journals.rcsi.science/1063-780X/article/view/186699
- DOI: https://doi.org/10.1134/S1063780X18020010
- ID: 186699
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Resumo
A time-dependent problem on finding the parameters of a low-density plasma jet ejected from a stationary plasma thruster is analyzed. In contrast to earlier works in which a stationary problem was solved using a Crook-type kinetic model, a set of kinetic equations is derived at the accuracy level accepted in the kinetic theory with allowance for resonant charge-exchange interaction between ions and neutrals. A method to solve the obtained set of equations is developed and used to perform test simulations, some results of which are presented.
Sobre autores
A. Bishaev
Moscow Institute of Physics and Technology
Email: riame4@sokol.ru
Rússia, Dolgoprudnyi, Moscow oblast, 141700
M. Abgaryan
Research Institute of Applied Mechanics and Electrodynamics
Email: riame4@sokol.ru
Rússia, Moscow, 125810
V. Kim
Research Institute of Applied Mechanics and Electrodynamics
Autor responsável pela correspondência
Email: riame4@sokol.ru
Rússia, Moscow, 125810
D. Merkur’ev
Research Institute of Applied Mechanics and Electrodynamics
Email: riame4@sokol.ru
Rússia, Moscow, 125810
E. Ivanova
Airbus Group Innovations
Email: riame4@sokol.ru
Rússia, Airbus
A. Fomenkov
Airbus Group Innovations
Email: riame4@sokol.ru
Rússia, Airbus
M. Wartelski
Airbus Defense and Space SAS
Email: riame4@sokol.ru
Rússia, Airbus
Ch. Theroude
Airbus Defense and Space SAS
Email: riame4@sokol.ru
Rússia, Airbus