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Thermoelastic analysis of solar cell arrays and their material propertiesA thermoelastic stress analysis procedure is reported for predicting the thermally induced stresses and failures in silicon solar cell arrays. A prerequisite for the analysis is the characterization of the temperature-dependent thermal and mechanical properties of the solar cell materials. Extensive material property testing was carried out in the temperature range -200 to +200 C for the filter glass, P- and N-type silicon, interconnector metals, solder, and several candidate silicone rubber adhesives. The analysis procedure is applied to several solar cell array design configurations. Results of the analysis indicate the optimum design configuration, with respect to compatible materials, effect of the solder coating, and effect of the interconnector geometry. Good agreement was found between results of the analysis and the test program.
Document ID
19730023261
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Salama, M. A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Rowe, W. M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Yasui, R. K.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1973
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-CR-135713
JPL-TM-33-626
Report Number: NASA-CR-135713
Report Number: JPL-TM-33-626
Accession Number
73N31993
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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