NASA NTRS · 19740029493
Interface requirements for electric propulsion power processing equipment
Abstract
Power processor interfaces, internal functions, and design techniques established for the 30-cm ion engine power processor are discussed. The interfaces include the ion engine interface, the spacecraft interface, source/load interactions, protection, and optimization criteria. In the analysis, particular attention is given to the interaction and protection aspects. A breadbord system designed and built for the 30-cm ion engine is discussed which will be used as an engineering tool to establish guidelines for electric propulsion systems.
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Biess, J. J., Schoenfeld, A. D., Goldin, D. S., Shank, J. H.. 1973-10-01. Interface requirements for electric propulsion power processing equipment. https://ntrs.nasa.gov/citations/19740029493
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