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New component development for multi-100 kW low-cost solar array applicationsStudies of the cost and performance of flexible arrays have shown that the most dramatic reductions in the $/Watt figure of merit are achieved by increasing performance. An examination of those properties that contribute to array performance indicated areas where radical changes in current design practice and philosophy would result in significant cost and performance impacts. To take advantage of the predicted cost reductions, modules were fabricated and tested that had ultra-thin superstrates as a load carrying member and large area dielectric wraparound (DWA), gridded back surface and copper contacted solar cells.
Document ID
19840040176
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pack, G. J.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Mann, J. A.
(Lockheed Missiles and Space Co., Inc. Sunnyvale, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1982
Subject Category
Spacecraft Propulsion And Power
Accession Number
84A22963
Funding Number(s)
CONTRACT_GRANT: NAS8-32981
Distribution Limits
Public
Copyright
Other

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