NASA STI Repository (National Aeronautics and Space Administration) · 12 citations · 8 references
Open access
EngineeringAerospace EngineeringElectrical EngineeringPower ElectronicsPropulsionSpacecraft DesignElectric PropulsionIon PropulsionPower ManagementPower SystemsPropulsion System IntegrationPropulsion System PerformanceExploration MissionsManufacturabilityPower OutputPower Processing UnitsPropulsion System EfficiencyScalabilitySpacecraft Electric PropulsionSpacecraft Power Processing Units
The NASA s Evolutionary Xenon Thruster (NEXT) project is developing an advanced ion propulsion system for future NASA missions for solar system exploration. An engineering model (EM) power processing unit (PPU) for the NEXT project was designed and fabricated by L-3 Communications under contract with NASA Glenn Research Center (GRC). This modular PPU is capable of processing up from 0.5 to 7.0 kW of output power for the NEXT ion thruster. Its design includes many significant improvements for better performance over the state-of-the-art PPU. The most significant difference is the beam supply which is comprised of six modules and capable of very efficient operation through a wide voltage range because of innovative features like dual controls, module addressing, and a high current mode. The low voltage power supplies are based on elements of the previously validated NASA Solar Electric Propulsion Technology Application Readiness (NSTAR) PPU. The highly modular construction of the PPU resulted in improved manufacturability, simpler scalability, and lower cost. This paper describes the design of the EM PPU and the results of the bench-top performance tests.
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Development and Testing of the Dawn Ion Propulsion System
John Brophy, Michael Etters, Jason Gates et al. · 2006 · 43 citations