Nonstationary Model of a Low-Density Plasma Jet Ejected from a Stationary Plasma Thruster
- Авторлар: 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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Мекемелер:
- Moscow Institute of Physics and Technology
- Research Institute of Applied Mechanics and Electrodynamics
- Airbus Group Innovations
- Airbus Defense and Space SAS
- Шығарылым: Том 44, № 2 (2018)
- Беттер: 278-288
- Бөлім: Plasma Accelerators
- URL: https://journals.rcsi.science/1063-780X/article/view/186699
- DOI: https://doi.org/10.1134/S1063780X18020010
- ID: 186699
Дәйексөз келтіру
Аннотация
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.
Авторлар туралы
A. Bishaev
Moscow Institute of Physics and Technology
Email: riame4@sokol.ru
Ресей, Dolgoprudnyi, Moscow oblast, 141700
M. Abgaryan
Research Institute of Applied Mechanics and Electrodynamics
Email: riame4@sokol.ru
Ресей, Moscow, 125810
V. Kim
Research Institute of Applied Mechanics and Electrodynamics
Хат алмасуға жауапты Автор.
Email: riame4@sokol.ru
Ресей, Moscow, 125810
D. Merkur’ev
Research Institute of Applied Mechanics and Electrodynamics
Email: riame4@sokol.ru
Ресей, Moscow, 125810
E. Ivanova
Airbus Group Innovations
Email: riame4@sokol.ru
Ресей, Airbus
A. Fomenkov
Airbus Group Innovations
Email: riame4@sokol.ru
Ресей, Airbus
M. Wartelski
Airbus Defense and Space SAS
Email: riame4@sokol.ru
Ресей, Airbus
Ch. Theroude
Airbus Defense and Space SAS
Email: riame4@sokol.ru
Ресей, Airbus