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A lightweight solar array studyA sample module was assembled to model a portion of a flexible extendable solar array, a type that promises to become the next generation of solar array design. The resulting study of this module is intended to provide technical support to the array designer for lightweight component selection, specifications, and tests. Selected from available lightweight components were 127-micron-thick wrap-around contacted solar cells, 34- micron-thick sputtered glass covers, and as a substrate a 13-micron-thick polyimide film clad with a copper printed circuit. Each component displayed weaknesses. The thin solar cells had excessive breakage losses. Sputtered glass cover adhesion was poor, and the covered cell was weaker than the cell uncovered. Thermal stresses caused some cell delamination from the model solar array substrate.
Document ID
19770015667
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Josephs, R. H.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 3, 2013
Publication Date
February 15, 1977
Subject Category
Energy Production And Conversion
Report/Patent Number
JPL-PUBL-77-3
NASA-CR-152676
Report Number: JPL-PUBL-77-3
Report Number: NASA-CR-152676
Accession Number
77N22611
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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