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The LDEF heat pipe experiment power systemsA heatpipe experiment for a long duration exposure facility is described. The design and configuration of the power system of the spacecraft is reported with emphasis placed on its solar array panels, 12-ampere hour 18-cell nickel battery, and its electronic controller.
Document ID
19800012359
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tiller, S. E. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 10, 2013
Publication Date
April 1, 1980
Publication Information
Publication: The 1979 Goddard Space Flight Center Battery Workshop
Subject Category
Energy Production And Conversion
Accession Number
80N20843
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19800012336Collected WorksThe 1979 Goddard Space Flight Center Battery Workshop
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