Simplified power processing for ion-thruster subsystems

Abstract

A review of the thruster/power-processor-interface requirements for (mercury and inert gas) ion-thrusters, an evaluation of various approaches to simplifying the power-processor circuitry, and the test results of the recently developed 8-cm mercury-ion-thruster simplified power-processor unit (SPPU) are presented. The SPPU demonstrates the feasibility of stable thruster operation using highly simplified power-processing techniques and achieves an approximately tenfold reduction in the electronic parts count when compared to the existing power-processor unit (PPU) used in the Hughes/NASA Lewis Research Center 8-cm-diameter (mercury) Ion Auxiliary Propulsion Subsystem (IAPS).