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Extended performance electric propulsion power processor design study. Volume 2: Technical summaryElectric propulsion power processor technology has processed during the past decade to the point that it is considered ready for application. Several power processor design concepts were evaluated and compared. Emphasis was placed on a 30 cm ion thruster power processor with a beam power rating supply of 2.2KW to 10KW for the main propulsion power stage. Extension in power processor performance were defined and were designed in sufficient detail to determine efficiency, component weight, part count, reliability and thermal control. A detail design was performed on a microprocessor as the thyristor power processor controller. A reliability analysis was performed to evaluate the effect of the control electronics redesign. 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.
Document ID
19780020226
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Biess, J. J.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Inouye, L. Y.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Schoenfeld, A. D.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1977
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-135358
TRW-31526.000-VOL-2
Report Number: NASA-CR-135358
Report Number: TRW-31526.000-VOL-2
Accession Number
78N28169
Funding Number(s)
CONTRACT_GRANT: NAS3-20403
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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