Standard

Design optimization of a magnetoplasmadynamic thruster by numerical methods. / Li, M.; Liu, H.; Ning, Z.; Ren, J.; Tang, H.; Yu, D.; Eliseev, S.; Kudryavtsev, A.

в: High Temperature Materials and Processes, Том 18, № 1-2, 2014, стр. 83-90.

Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование

Harvard

Li, M, Liu, H, Ning, Z, Ren, J, Tang, H, Yu, D, Eliseev, S & Kudryavtsev, A 2014, 'Design optimization of a magnetoplasmadynamic thruster by numerical methods', High Temperature Materials and Processes, Том. 18, № 1-2, стр. 83-90. https://doi.org/10.1615/HighTempMatProc.2015015355, https://doi.org/10.1615/HighTempMatProc.2015015355

APA

Li, M., Liu, H., Ning, Z., Ren, J., Tang, H., Yu, D., Eliseev, S., & Kudryavtsev, A. (2014). Design optimization of a magnetoplasmadynamic thruster by numerical methods. High Temperature Materials and Processes, 18(1-2), 83-90. https://doi.org/10.1615/HighTempMatProc.2015015355, https://doi.org/10.1615/HighTempMatProc.2015015355

Vancouver

Li M, Liu H, Ning Z, Ren J, Tang H, Yu D и пр. Design optimization of a magnetoplasmadynamic thruster by numerical methods. High Temperature Materials and Processes. 2014;18(1-2):83-90. https://doi.org/10.1615/HighTempMatProc.2015015355, https://doi.org/10.1615/HighTempMatProc.2015015355

Author

Li, M. ; Liu, H. ; Ning, Z. ; Ren, J. ; Tang, H. ; Yu, D. ; Eliseev, S. ; Kudryavtsev, A. / Design optimization of a magnetoplasmadynamic thruster by numerical methods. в: High Temperature Materials and Processes. 2014 ; Том 18, № 1-2. стр. 83-90.

BibTeX

@article{ac7da59b80ec459ca14adf9e179071b3,
title = "Design optimization of a magnetoplasmadynamic thruster by numerical methods",
abstract = "In this work a 2D model for simulating an applied-field magnetoplasmadynamic (AF-MPD) thruster with a hollow cathode made of thoriated tungsten was constructed using Comsol Multiphysics. The model allowed for self-consistent description of plasma processes inside an ionization chamber in the thruster and heating of the cathode due to ion bombardment. The distribution of such discharge parameters as charged and excited particle densities, charged particles{\textquoteright} mean energies and temperatures, gas temperature, cathode temperature, and electric potential were obtained. Numerical experiments were carried out for different geometries and optimal configuration of AFMPD thruster with a hollow cathode was obtained.",
keywords = "Arc discharges, MPD thruster, Plasma propulsion, Plasma simulations",
author = "M. Li and H. Liu and Z. Ning and J. Ren and H. Tang and D. Yu and S. Eliseev and A. Kudryavtsev",
note = "Publisher Copyright: {\textcopyright} 2014, by Begell House, Inc.",
year = "2014",
doi = "10.1615/HighTempMatProc.2015015355",
language = "English",
volume = "18",
pages = "83--90",
journal = "High Temperature Material Processes",
issn = "1093-3611",
publisher = "Begell House Inc.",
number = "1-2",

}

RIS

TY - JOUR

T1 - Design optimization of a magnetoplasmadynamic thruster by numerical methods

AU - Li, M.

AU - Liu, H.

AU - Ning, Z.

AU - Ren, J.

AU - Tang, H.

AU - Yu, D.

AU - Eliseev, S.

AU - Kudryavtsev, A.

N1 - Publisher Copyright: © 2014, by Begell House, Inc.

PY - 2014

Y1 - 2014

N2 - In this work a 2D model for simulating an applied-field magnetoplasmadynamic (AF-MPD) thruster with a hollow cathode made of thoriated tungsten was constructed using Comsol Multiphysics. The model allowed for self-consistent description of plasma processes inside an ionization chamber in the thruster and heating of the cathode due to ion bombardment. The distribution of such discharge parameters as charged and excited particle densities, charged particles’ mean energies and temperatures, gas temperature, cathode temperature, and electric potential were obtained. Numerical experiments were carried out for different geometries and optimal configuration of AFMPD thruster with a hollow cathode was obtained.

AB - In this work a 2D model for simulating an applied-field magnetoplasmadynamic (AF-MPD) thruster with a hollow cathode made of thoriated tungsten was constructed using Comsol Multiphysics. The model allowed for self-consistent description of plasma processes inside an ionization chamber in the thruster and heating of the cathode due to ion bombardment. The distribution of such discharge parameters as charged and excited particle densities, charged particles’ mean energies and temperatures, gas temperature, cathode temperature, and electric potential were obtained. Numerical experiments were carried out for different geometries and optimal configuration of AFMPD thruster with a hollow cathode was obtained.

KW - Arc discharges

KW - MPD thruster

KW - Plasma propulsion

KW - Plasma simulations

UR - http://www.scopus.com/inward/record.url?scp=84947941445&partnerID=8YFLogxK

U2 - 10.1615/HighTempMatProc.2015015355

DO - 10.1615/HighTempMatProc.2015015355

M3 - Article

VL - 18

SP - 83

EP - 90

JO - High Temperature Material Processes

JF - High Temperature Material Processes

SN - 1093-3611

IS - 1-2

ER -

ID: 7062994