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Critical electrical aspects of alternating-current power source for Centaur space vehicleReliability of silicon rectifiers as inverters for alternating current power source for Atlas Centaur launch vehicles
Document ID
19680012093
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Baddour, M. F. (NASA Lewis Research Center Cleveland, OH, United States)
Quitter, J. P. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1968
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TM-X-1569
Report Number: NASA-TM-X-1569
Accession Number
68N21562
Funding Number(s)
CONTRACT_GRANT: 491-03-00-01-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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