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