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Space Station Freedom secondary power wiring requirementsSecondary power is produced by DDCU's (direct current to direct current converter units) and routed to and through secondary power distribution assemblies (SPDA's) to loads or tertiary distribution assemblies. This presentation outlines requirements of Space Station Freedom (SSF) EEE (electrical, electronic, and electromechanical) parts wire and the approved electrical wire and cable. The SSF PDRD (Program Definition and Requirements Document) language problems and resolution are reviewed. The cable routing to and from the SPDA's is presented as diagrams and the wire recommendations and characteristics are given.
Document ID
19950009637
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sawyer, C. R.
(Boeing Aerospace and Electronics Co. Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1994
Publication Information
Publication: NASA. Lewis Research Center, First NASA Workshop on Wiring for Space Applications
Subject Category
Spacecraft Propulsion And Power
Accession Number
95N16052
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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