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Space Station Freedom electrical power system hardware commonality with the United States Polar PlatformInformation is presented 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. 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. The Space Station program and objectives are described, focusing on the test and development responsibilities. The program definition and preliminary design phase and the design and development phase are discussed. The goal of this work is to reduce the program cost.
Document ID
19900051018
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
August 14, 2013
Publication Date
January 1, 1989
Subject Category
SPACECRAFT PROPULSION AND POWER
Meeting Information
IECEC-89(Washington, DC)
Distribution Limits
Public
Copyright
Other