Nonstationary Model of a Low-Density Plasma Jet Ejected from a Stationary Plasma Thruster


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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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