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Fundamental difference between the two Hall thruster variants
E. Y. Choueiri
Mechanical & Aerospace Engineering
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peer-review
101
Scopus citations
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Keyphrases
Stationary Plasma Thruster
100%
Axial Location
33%
Wall Potential
33%
Boron Nitride
33%
Higher Secondary
33%
Secondary Electron Emission Coefficient
33%
Engineering
Secondary Electrons
53%
Emission Coefficient
26%
Potential Gradient
26%
Axial Location
26%
Material Science
Boron Nitride
33%