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Investigation of welded interconnection of large area wraparound contacted silicon solar cellsAn investigation was conducted to evaluate the welding and temperature cycle testing of large area 5.9 x 5.9 wraparound silicon solar cells utilizing printed circuit substrates with SSC-155 interconnect copper metals and the LMSC Infrared Controlled weld station. An initial group of 5 welded modules containing Phase 2 developmental 5.9 x 5.9 cm cells were subjected to cyclical temperatures of + or 80 C at a rate of 120 cycles per day. Anomalies were noted in the adhesion of the cell contact metallization; therefore, 5 additional modules were fabricated and tested using available Phase I cells with demonstrated contact integrity. Cycling of the later module type through 12,000 cycles indicated the viability of this type of lightweight flexible array concept. This project demonstrated acceptable use of an alternate interconnect copper in combination with large area wraparound cells and emphasized the necessity to implement weld pull as opposed to solder pull procedures at the cell vendors for cells that will be interconnected by welding.
Document ID
19850011209
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lott, D. R.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1984
Subject Category
Energy Production And Conversion
Report/Patent Number
NASA-CR-174438
NAS 1.26:174438
JPL-9950-975
LMSC-D973421
Report Number: NASA-CR-174438
Report Number: NAS 1.26:174438
Report Number: JPL-9950-975
Report Number: LMSC-D973421
Accession Number
85N19519
Funding Number(s)
CONTRACT_GRANT: JPL-956020
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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