24th Joint Propulsion Conference · 1988 · 46 citations · 6 references
EngineeringElectrical EngineeringPhysicsElectrochemistryPlasma PhysicsPropulsionCathode MaterialsElectric PropulsionIon PropulsionCathode BehaviorCathode ErosionCurrentsDischarge Chamber PhysicsElectrode ErosionHigh-voltage CathodesHollow Cathode DischargesHollow Cathodes
The development of high power, high thrust ion engines requires the development of long life hollow cathodes capable of producing emission currents of hundreds of amperes. This paper describes results obtained through the extended testing of two 12.7 mm diameter hollow cathodes at high emission currents. The first cathode, operated on xenon for a total of 170 hours at an emission current of 100 A, sustained very little damage except for an increase in the cathode orifice diameter, from 0.953 to 1.71 mm. The second cathode was operated on xenon at 150 A emission current continuously for 24 hours, and for over 1000 hours at 100 A on argon with essentially no change in the cathode operating characteristics. Operation of this cathode was terminated due to severe erosion of several discharge chamber components located downstream of the cathode. The erosion of these components occurred despite operation at discharge voltages less than 24 volts, and poses a serious challenge to the sucessful implementation of multi-hundred ampere cathodes and high thrust ion engines.
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A Study of Hollow Cathode Discharge Characteristics
C. M. PHILIP · AIAA Journal · 1971 · 24 citations
A 30-cm diameter argon ion source
James S. Sovey · 1976 · 15 citations