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Utility of Thin-Film Solar Cells on Flexible Substrates for Space PowerThe thin-film solar cell program at NASA GRC is developing solar cell technologies for space applications which address two critical metrics: specific power (power per unit mass) and launch stowed volume. To be competitive for many space applications, an array using thin film solar cells must significantly increase specific power while reducing stowed volume when compared to the present baseline technology utilizing crystalline solar cells. The NASA GRC program is developing two approaches. Since the vast majority of the mass of a thin film solar cell is in the substrate, a thin film solar cell on a very lightweight flexible substrate (polymer or metal films) is being developed as the first approach. The second approach is the development of multijunction thin film solar cells. Total cell efficiency can be increased by stacking multiple cells having bandgaps tuned to convert the spectrum passing through the upper cells to the lower cells. Once developed, the two approaches will be merged to yield a multijunction, thin film solar cell on a very lightweight, flexible substrate. The ultimate utility of such solar cells in space require the development of monolithic interconnections, lightweight array structures, and ultra-lightweight support and deployment techniques.
Document ID
20040035568
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Dickman, J. E.
(NASA Glenn Research Center Cleveland, OH, United States)
Hepp, A. F.
(NASA Glenn Research Center Cleveland, OH, United States)
Morel, D. L.
(University of South Florida Tampa, FL, United States)
Ferekides, C. S.
(University of South Florida Tampa, FL, United States)
Tuttle, J. R.
(Daystar Technologies, Inc. Grass Valley, CA, United States)
Hoffman, D. J.
(NASA Glenn Research Center Cleveland, OH, United States)
Dhere, N. G.
(Florida Solar Energy Center Cocoa Beach, FL, United States)
Date Acquired
September 7, 2013
Publication Date
March 1, 2004
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA/TM-2004-212554
E-14120
AIAA Paper 2003-5922
Report Number: NASA/TM-2004-212554
Report Number: E-14120
Report Number: AIAA Paper 2003-5922
Meeting Information
Meeting: First International Energy Conversion Engineering Conference
Location: Portsmouth, VA
Country: United States
Start Date: August 17, 2003
End Date: August 21, 2003
Sponsors: American Society of Mechanical Engineers, Institute of Electrical and Electronics Engineers, American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 22-755-60-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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