NASA NTRS · 19930066165
Simplified power processing for inert gas ion thrusters
Abstract
Significant simplifications to power processors for inert gas ion thrusters in the 1 to 5 kW range have been identified. They include elimination of all but three power supplies - one each for the neutralizer, main discharge, and beam. The neutralizer and discharge power supplies would provide both cathode heating and plasma generating functions. This dual-use power supply concept was validated via integration tests with a 30 cm diameter xenon ion thruster. The beam/accelerator power supply would have positive and negative outputs to allow a single power supply to provide both functions. The discharge and beam power supplies would incorporate full-bridge inverters similar to those proven for flight-ready arcjet propulsion systems. Operation of this simplified power processing scheme at an inverter frequency of 50 kHz results in a projected power processor design with low mass and high efficiency. A 2 kW reference point design has estimated values of specific mass of 5.4 kg/kW and an efficiency of 93 percent.
Keep this discovery
Explore connections, maps & timelines
Rawlin, V. K., Pinero, L. R., Hamley, J. A.. 1993-06-01. Simplified power processing for inert gas ion thrusters. https://ntrs.nasa.gov/citations/19930066165
Cite the original work for its findings. Save a collection to share your selection of sources.