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2-D Modeling of Orificed Hollow Cathodes of Stationary Plasma Thrusters SPT-100. / Liu, Hui; Li, Min; Ning, Zhongxi; Ren, Junxue; Tang, Haibin; Yu, Daren; Demidov, Evgenii V.; Eliseev, Stepan I.; Kudryavtsev, Anatoly A.

в: IEEE Transactions on Plasma Science, Том 43, № 12, 7182760, 12.2015, стр. 4024-4033.

Результаты исследований: Научные публикации в периодических изданияхстатьяРецензирование

Harvard

Liu, H, Li, M, Ning, Z, Ren, J, Tang, H, Yu, D, Demidov, EV, Eliseev, SI & Kudryavtsev, AA 2015, '2-D Modeling of Orificed Hollow Cathodes of Stationary Plasma Thrusters SPT-100', IEEE Transactions on Plasma Science, Том. 43, № 12, 7182760, стр. 4024-4033. https://doi.org/10.1109/TPS.2015.2457677, https://doi.org/10.1109/TPS.2015.2457677

APA

Liu, H., Li, M., Ning, Z., Ren, J., Tang, H., Yu, D., Demidov, E. V., Eliseev, S. I., & Kudryavtsev, A. A. (2015). 2-D Modeling of Orificed Hollow Cathodes of Stationary Plasma Thrusters SPT-100. IEEE Transactions on Plasma Science, 43(12), 4024-4033. [7182760]. https://doi.org/10.1109/TPS.2015.2457677, https://doi.org/10.1109/TPS.2015.2457677

Vancouver

Liu H, Li M, Ning Z, Ren J, Tang H, Yu D и пр. 2-D Modeling of Orificed Hollow Cathodes of Stationary Plasma Thrusters SPT-100. IEEE Transactions on Plasma Science. 2015 Дек.;43(12):4024-4033. 7182760. https://doi.org/10.1109/TPS.2015.2457677, https://doi.org/10.1109/TPS.2015.2457677

Author

Liu, Hui ; Li, Min ; Ning, Zhongxi ; Ren, Junxue ; Tang, Haibin ; Yu, Daren ; Demidov, Evgenii V. ; Eliseev, Stepan I. ; Kudryavtsev, Anatoly A. / 2-D Modeling of Orificed Hollow Cathodes of Stationary Plasma Thrusters SPT-100. в: IEEE Transactions on Plasma Science. 2015 ; Том 43, № 12. стр. 4024-4033.

BibTeX

@article{e5d28b228ff146f0be292a5a05c3a776,
title = "2-D Modeling of Orificed Hollow Cathodes of Stationary Plasma Thrusters SPT-100",
abstract = "In this paper, 2-D extended fluid model for the simulation of orificed hollow cathode (OHC) discharge in xenon flow of SPT-100 thruster was built using Comsol Multiphysics. Self-consistent discharge model is based on fluid description of ions and excited neutral species and uses drift-diffusion approximation for the particle fluxes. Electron transport and rates of electron-induced plasma-chemical reactions are calculated using Boltzmann equation for electron energy distribution function and corresponding collision cross sections. A reasonable set of plasma-chemical processes with electrons, ions, and excited and neutral particles were considered. The model accounts for gas flow and heating. Self-consistent electric field is calculated from the Poisson equation. The model geometry reproduces that of the experimental OHC for stationary plasma thruster SPT-100, which was studied in Harbin Institute of Technology. Simulations were carried out for different operational modes of the OHC. Distributions of key discharge parameters were obtained. A comparison between the simulation results and experimental data was conducted and showed good agreement.",
keywords = "Arc discharges, plasma devices, plasma simulation.",
author = "Hui Liu and Min Li and Zhongxi Ning and Junxue Ren and Haibin Tang and Daren Yu and Demidov, {Evgenii V.} and Eliseev, {Stepan I.} and Kudryavtsev, {Anatoly A.}",
note = "Publisher Copyright: {\textcopyright} 1973-2012 IEEE.",
year = "2015",
month = dec,
doi = "10.1109/TPS.2015.2457677",
language = "English",
volume = "43",
pages = "4024--4033",
journal = "IEEE Transactions on Plasma Science",
issn = "0093-3813",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
number = "12",

}

RIS

TY - JOUR

T1 - 2-D Modeling of Orificed Hollow Cathodes of Stationary Plasma Thrusters SPT-100

AU - Liu, Hui

AU - Li, Min

AU - Ning, Zhongxi

AU - Ren, Junxue

AU - Tang, Haibin

AU - Yu, Daren

AU - Demidov, Evgenii V.

AU - Eliseev, Stepan I.

AU - Kudryavtsev, Anatoly A.

N1 - Publisher Copyright: © 1973-2012 IEEE.

PY - 2015/12

Y1 - 2015/12

N2 - In this paper, 2-D extended fluid model for the simulation of orificed hollow cathode (OHC) discharge in xenon flow of SPT-100 thruster was built using Comsol Multiphysics. Self-consistent discharge model is based on fluid description of ions and excited neutral species and uses drift-diffusion approximation for the particle fluxes. Electron transport and rates of electron-induced plasma-chemical reactions are calculated using Boltzmann equation for electron energy distribution function and corresponding collision cross sections. A reasonable set of plasma-chemical processes with electrons, ions, and excited and neutral particles were considered. The model accounts for gas flow and heating. Self-consistent electric field is calculated from the Poisson equation. The model geometry reproduces that of the experimental OHC for stationary plasma thruster SPT-100, which was studied in Harbin Institute of Technology. Simulations were carried out for different operational modes of the OHC. Distributions of key discharge parameters were obtained. A comparison between the simulation results and experimental data was conducted and showed good agreement.

AB - In this paper, 2-D extended fluid model for the simulation of orificed hollow cathode (OHC) discharge in xenon flow of SPT-100 thruster was built using Comsol Multiphysics. Self-consistent discharge model is based on fluid description of ions and excited neutral species and uses drift-diffusion approximation for the particle fluxes. Electron transport and rates of electron-induced plasma-chemical reactions are calculated using Boltzmann equation for electron energy distribution function and corresponding collision cross sections. A reasonable set of plasma-chemical processes with electrons, ions, and excited and neutral particles were considered. The model accounts for gas flow and heating. Self-consistent electric field is calculated from the Poisson equation. The model geometry reproduces that of the experimental OHC for stationary plasma thruster SPT-100, which was studied in Harbin Institute of Technology. Simulations were carried out for different operational modes of the OHC. Distributions of key discharge parameters were obtained. A comparison between the simulation results and experimental data was conducted and showed good agreement.

KW - Arc discharges

KW - plasma devices

KW - plasma simulation.

UR - http://www.scopus.com/inward/record.url?scp=84939164656&partnerID=8YFLogxK

U2 - 10.1109/TPS.2015.2457677

DO - 10.1109/TPS.2015.2457677

M3 - Article

VL - 43

SP - 4024

EP - 4033

JO - IEEE Transactions on Plasma Science

JF - IEEE Transactions on Plasma Science

SN - 0093-3813

IS - 12

M1 - 7182760

ER -

ID: 3987302