Nonstationary Model of a Low-Density Plasma Jet Ejected from a Stationary Plasma Thruster
- 作者: Bishaev A.M.1, Abgaryan M.V.2, Kim V.2, Merkur’ev D.V.2, Ivanova E.P.3, Fomenkov A.I.3, Wartelski M.4, Theroude C.4
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隶属关系:
- Moscow Institute of Physics and Technology
- Research Institute of Applied Mechanics and Electrodynamics
- Airbus Group Innovations
- Airbus Defense and Space SAS
- 期: 卷 44, 编号 2 (2018)
- 页面: 278-288
- 栏目: 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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详细
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.
作者简介
A. Bishaev
Moscow Institute of Physics and Technology
Email: riame4@sokol.ru
俄罗斯联邦, Dolgoprudnyi, Moscow oblast, 141700
M. Abgaryan
Research Institute of Applied Mechanics and Electrodynamics
Email: riame4@sokol.ru
俄罗斯联邦, Moscow, 125810
V. Kim
Research Institute of Applied Mechanics and Electrodynamics
编辑信件的主要联系方式.
Email: riame4@sokol.ru
俄罗斯联邦, Moscow, 125810
D. Merkur’ev
Research Institute of Applied Mechanics and Electrodynamics
Email: riame4@sokol.ru
俄罗斯联邦, Moscow, 125810
E. Ivanova
Airbus Group Innovations
Email: riame4@sokol.ru
俄罗斯联邦, Airbus
A. Fomenkov
Airbus Group Innovations
Email: riame4@sokol.ru
俄罗斯联邦, Airbus
M. Wartelski
Airbus Defense and Space SAS
Email: riame4@sokol.ru
俄罗斯联邦, Airbus
Ch. Theroude
Airbus Defense and Space SAS
Email: riame4@sokol.ru
俄罗斯联邦, Airbus
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