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A comparative study of electric power distribution systems for spacecraftThe electric power distribution systems for spacecraft are compared concentrating on two interrelated issues: the choice between dc and high frequency ac, and the converter/inverter topology to be used at the power source. The relative merits of dc and ac distribution are discussed. Specific converter and inverter topologies are identified and analyzed in detail for the purpose of detailed comparison. Finally, specific topologies are recommended for use in dc and ac systems.
Document ID
19900011797
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stuart, Thomas A. (Toledo Univ. OH, United States)
King, Roger J. (Toledo Univ. OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1990
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:186531
NASA-CR-186531
Report Number: NAS 1.26:186531
Report Number: NASA-CR-186531
Accession Number
90N21113
Funding Number(s)
CONTRACT_GRANT: NAG3-708
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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