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Lightweight, Flexible Solar Cells on Stainless Steel Foil and Polymer for Space and Stratospheric ApplicationsThe availability of low-cost, lightweight and reliable photovoltaic (PV) modules is an important component in reducing the cost of satellites and spacecraft. In addition, future high-power spacecraft will require lightweight PV arrays with reduced stowage volume. In terms of the requirements for low mass, reduced stowage volume, and the harsh space environment, thin film amorphous silicon (a-Si) alloy cells have several advantages over other material technologies (1). The deposition process is relatively simple, inexpensive, and applicable to large area, lightweight, flexible substrates. The temperature coefficient has been found to be between -0.2 and -0.3 %/degC for high-efficiency triple-junction a-Si alloy cells, which is superior for high temperature operation compared to crystalline Si and triple-junction GaAs/InGaP/Ge devices at 0.53 %/degC and 0.45 %/degC, respectively (2). As a result, the reduction in efficiency at high temperature typical in space conditions is less for a-Si alloy cells than for their crystalline counterparts. Additionally, the a-Si alloy cells are relatively insensitive to electron and proton bombardment. We have shown that defects that are created by electrons with energies between 0.2 to 2 MeV with fluence up to 1x10(exp 15) e/sq cm and by protons with energy in the range 0.3 MeV to 5 MeV with fluence up to 1x10(exp 13) p/sq cm can be annealed out at 70 C in less than 50 hours (1). Further, modules incorporating United Solar s a-Si alloy cells have been tested on the MIR space station for 19 months with only minimal degradation (3). For stratospheric applications, such as the high altitude airship, the required PV arrays are typically of considerably higher power than current space arrays. Airships typically have a large area available for the PV, but weight is of critical importance. As a result, low cost and high specific power (W/kg) are key factors for airship PV arrays. Again, thin-film a-Si alloy solar cell technology is well suited to such applications.
Document ID
20090022306
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Beernink, Kevin
(United Solar Ovonic, LLC Troy, MI, United States)
Guha, Subhendu
(United Solar Ovonic, LLC Troy, MI, United States)
Yang, Jeff
(United Solar Ovonic, LLC Troy, MI, United States)
Banerjee, Arindam
(United Solar Ovonic, LLC Troy, MI, United States)
Lord, Ken
(United Solar Ovonic, LLC Troy, MI, United States)
DeMaggio, Greg
(United Solar Ovonic, LLC Troy, MI, United States)
Liu, Frank
(United Solar Ovonic, LLC Troy, MI, United States)
Pietka, Ginger
(United Solar Ovonic, LLC Troy, MI, United States)
Johnson, Todd
(United Solar Ovonic, LLC Troy, MI, United States)
Reinhout, Melanie
(United Solar Ovonic, LLC Troy, MI, United States)
Younan, Kais
(United Solar Ovonic, LLC Troy, MI, United States)
Wolf, David
(United Solar Ovonic, LLC Troy, MI, United States)
Date Acquired
August 24, 2013
Publication Date
February 1, 2007
Publication Information
Publication: Proceedings of the 19th Space Photovoltaic Research and Technology Conference
Subject Category
Space Sciences (General)
Funding Number(s)
CONTRACT_GRANT: F29601-03-C0122.
Distribution Limits
Public
Copyright
Public Use Permitted.
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