2020
DOI: 10.1063/1.5144851
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Discharge characteristics and increased electron current during azimuthally nonuniform propellant supply in an anode layer Hall thruster

Abstract: Discharge current components, such as electron, ion beam, and lost-to-wall currents, are obtained as functions of azimuthal propellant inhomogeneity in a Hall thruster. Discharge characteristics are discussed based on discharge current oscillation and radial–azimuthal discharge photography. A highly oscillative operation regime is found to be accompanied by radially enlarged expansion of discharge under limited electron currents. Further increases in neutral inhomogeneity lead to quiescent discharge combined w… Show more

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Cited by 8 publications
(3 citation statements)
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“…putational load of the hybrid model. Further, the entire circumference simulation may enable in-depth analyses of longwavelength rotating spokes 26,47 and thruster operations with artificial inhomogeneities 38,48 .…”
Section: Grid Convergencementioning
confidence: 99%
“…putational load of the hybrid model. Further, the entire circumference simulation may enable in-depth analyses of longwavelength rotating spokes 26,47 and thruster operations with artificial inhomogeneities 38,48 .…”
Section: Grid Convergencementioning
confidence: 99%
“…The changes in these parameters are explained using the force balance on electrons. It is noteworthy that the present work is distinguished from our past works where the focus was made on resolving the plasma structure and identifying electron flux by E θ , 16 and characterizing discharge behavior depending on the input neutral inhomogeneity level 17 .…”
Section: Introductionmentioning
confidence: 99%
“…E × B plasmas is reported in a number of numerical [10][11][12][13] and experimental studies [14][15][16][17] of E × B plasma. Similar transport effects by an induced (fluctuating) field is often discussed in the magnetically confined fusion machines 18 .…”
Section: Introductionmentioning
confidence: 99%