NASA NTRS · 19780012307
Extended performance electric propulsion power processor design study. Volume 1: Executive summary
Abstract
Several power processor design concepts were evaluated and compared. Emphasis was placed on a 30cm ion thruster power processor with a beam supply rating of 2.2kW to 10kW. Extensions in power processor performance were defined and were designed in sufficient detail to determine efficiency, component weight, part count, reliability and thermal control. Preliminary electrical design, mechanical design, and thermal analysis were performed on a 6kW power transformer for the beam supply. Bi-Mod mechanical, structural, and thermal control configurations were evaluated for the power processor, and preliminary estimates of mechanical weight were determined. A program development plan was formulated that outlines the work breakdown structure for the development, qualification and fabrication of the power processor flight hardware.
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Biess, J. J., Inouye, L. Y., Schoenfeld, A. D.. 1977-11-01. Extended performance electric propulsion power processor design study. Volume 1: Executive summary. https://ntrs.nasa.gov/citations/19780012307
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