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Space station electric power system requirements and designAn overview of the conceptual definition and design of the space station Electric Power System (EPS) is given. Responsibilities for the design and development of the EPS are defined. The EPS requirements are listed and discussed, including average and peak power requirements, contingency requirements, and fault tolerance. The most significant Phase B trade study results are summarized, and the design selections and rationale are given. Finally, the power management and distribution system architecture is presented.
Document ID
19870012568
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Teren, Fred (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-3577
AIAA PAPER 87-9003
NAS 1.15:89889
NASA-TM-89889
Accession Number
87N22001
Funding Number(s)
PROJECT: RTOP 481-54-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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