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Centaur solid state inverter failure during simulated flight in an environmental space chamberCentaur solid state inverter failure during simulated flight in environmental space chamber
Document ID
19670031206
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dastoli, B. J. (NASA Lewis Research Center Cleveland, OH, United States)
Schmiedlin, R. F. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1967
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TM-X-52336
Accession Number
67N40535
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SPACECRAFT COMPONENT
FLIGHT SIMULATION
CENTAUR LAUNCH VEHICLE
ENVIRONMENTAL TESTING
ELECTRIC BREAKDOWN

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