Electrical Facility Effects on Hall Thruster Cathode Coupling: Performance and Plume Properties

The impact of facility conductivity on Hall effect thruster cathode coupling is experimentally investigated. The 3.4 kW Aerojet Rocketdyne T-140 Hall effect thruster operating at a discharge voltage of 300 V, a discharge current of 10.3 A, and an anode flow rate of 11.6 mg/s serves as a representat...

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Veröffentlicht in:	Journal of propulsion and power 2016-01, Vol.32 (1), p.251-264
Hauptverfasser:	Frieman, Jason D, Walker, Jonathan A, Walker, Mitchell L. R, Khayms, Vadim, King, David Q
Format:	Artikel
Sprache:	eng
Schlagworte:	Aluminum Cathodes Circuits Coupling Discharge Electric potential Electrical resistivity Electromagnetism Electron recombination Electrons Far fields Flow velocity Grounds Hall effect Metal plates Plates Position (location) Position measurement Propulsion Thrusters Vacuum chambers Xenon
Online-Zugang:	Volltext
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