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Space Station Freedom electrical power system hardware commonality with the United States Polar PlatformThe National Aeronautics and Space Administration has adopted the policy to achieve the maximum practical level of commonality for the Space Station Freedom program in order to significantly reduce life cycle costs. Commonality means using identical or similar hardware/software for meeting common sets of functionally similar requirements. Information on how the concept of commonality is being implemented with respect to electric power system hardware for the Space Station Freedom and the U.S. Polar Platform is presented. Included is a historical account of the candidate common items which have the potential to serve the same power system functions on both Freedom and the Polar Platform.
Document ID
19890015068
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rieker, Lorra L.
(NASA Lewis Research Center Cleveland, OH, United States)
Haraburda, Francis M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1989
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.15:102074
NASA-TM-102074
E-4833
Report Number: NAS 1.15:102074
Report Number: NASA-TM-102074
Report Number: E-4833
Meeting Information
Meeting: Intersociety Energy Conversion Engineering Conference
Location: Washington, DC
Country: United States
Start Date: August 6, 1989
End Date: August 11, 1989
Sponsors: ANS, AIAA, AIChE, SAE, ASME, IEEE, ACS
Accession Number
89N24439
Funding Number(s)
PROJECT: RTOP 474-46-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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