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Extended performance electric propulsion power processor design study. Volume 1: Executive summarySeveral 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.
Document ID
19780012307
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-135357
TRW-31526.000-VOL-1
Report Number: NASA-CR-135357
Report Number: TRW-31526.000-VOL-1
Accession Number
78N20250
Funding Number(s)
CONTRACT_GRANT: NAS3-20403
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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