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Power Systems integrationPower systems integration in large flexible space structures is discussed with emphasis upon body control. A solar array is discussed as a typical example of spacecraft configuration problems. Information on how electric batteries dominate life-cycle costs is presented in chart form. Information is given on liquid metal droplet generators and collectors, hot spot analysis, power dissipation in solar arrays, solar array protection optimization, and electromagnetic compatibility for a power system platform.
Document ID
19820019502
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brantley, L. W. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1982
Publication Information
Publication: NASA. Lewis Research Center Large Space Systems(Propulsion Interactions
Subject Category
Spacecraft Propulsion And Power
Accession Number
82N27378
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19820019482Collected WorksLarge Space Systems/Propulsion Interactions
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