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Space station electrical power distribution analysis using a load flow approachThe space station's electrical power system will evolve and grow in a manner much similar to the present terrestrial electrical power system utilities. The initial baseline reference configuration will contain more than 50 nodes or busses, inverters, transformers, overcurrent protection devices, distribution lines, solar arrays, and/or solar dynamic power generating sources. The system is designed to manage and distribute 75 KW of power single phase or three phase at 20 KHz, and grow to a level of 300 KW steady state, and must be capable of operating at a peak of 450 KW for 5 to 10 min. In order to plan far into the future and keep pace with load growth, a load flow power system analysis approach must be developed and utilized. This method is a well known energy assessment and management tool that is widely used throughout the Electrical Power Utility Industry. The results of a comprehensive evaluation and assessment of an Electrical Distribution System Analysis Program (EDSA) is discussed. Its potential use as an analysis and design tool for the 20 KHz space station electrical power system is addressed.
Document ID
19870017266
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Emanuel, Ervin M.
(Prairie View Agricultural and Mechanical Coll. TX, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1987
Publication Information
Publication: NASA. Lyndon B.
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87N26699
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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