NASA NTRS · 19810042822
An improved lamination technique for solar arrays
Abstract
Encapsulating solar cells by lamination has been plagued with problems such as bubbles, cell shifting, ripples, and cracked cells. A low-cost laminating procedure has been developed using a double vacuum bagging technique and recently improved formulations of ethylene vinyl acetate, successfully minimizing these problems. The lamination fixturing used is described. The causes and cures of various problems are discussed and solutions to these problems presented. The apparent modulus of the face sheet seen by the module being laminated is believed to be the primary variable which must be optimized. Conditions at the module edge are also considered to be important for producing an acceptable product.
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Garcia, A., III, Olson, C.. 1980-01-01. An improved lamination technique for solar arrays. https://ntrs.nasa.gov/citations/19810042822
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