1976 · 17 citations · 0 references
EngineeringAerospace EngineeringElectrical EngineeringPlasma PhysicsPower ElectronicsPropulsionElectric PropulsionIon PropulsionPlasma PropulsionPropulsion System PerformanceSpace PlasmasThrust SystemsErosion MechanismsIon Thruster Performance AnalysisIon ThrustersPerformance CharacterizationPlasma ThrustersThruster DesignThruster LifetimeThruster Lifetime Testing
The 10,000 hour endurance test of the first engineering model 30-cm thruster (S/N 701) identified discharge chamber erosion as a life limiting problem. Modifications to minimize this problem have been implemented in the 900 series thrusters. This paper describes a test conducted to evaluate the success of these modifications. The post-test analysis results of thruster 701 are summarized and the erosion reducing modifications described. Test results for thruster 901 up to 4165 hours, when the test was interrupted by a shorted wire, are described. The conclusions of a post-test examination of thruster 901 are included. Also being evaluated was a thermal vacuum breadboard SCR series inverter power processor which is described.