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


Citar

Texto integral

Acesso aberto Acesso aberto
Acesso é fechado Acesso está concedido
Acesso é fechado Somente assinantes

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


Declaração de direitos autorais © Pleiades Publishing, Ltd., 2018

Este site utiliza cookies

Ao continuar usando nosso site, você concorda com o procedimento de cookies que mantêm o site funcionando normalmente.

Informação sobre cookies