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Photovoltaic options for solar electric propulsionThis paper discusses both state-of-the-art and advanced development cell and array technology. Present technology includes rigid, roll-out, and foldout flexible substrate designs, with silicon and GaAs solar cells. The use of concentrator array systems is discussed based on both DOD efforts and NASA work. The benefits of advanced lightweight array technology, for both near term and far term utilization, and of advanced high efficiency thin radiation resistant cells is examined. This includes gallium arsenide/germanium, indium phosphide, and thin film devices such as copper indium disclenide.
Document ID
19900065508
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stella, Paul M.
(JPL Pasadena, CA, United States)
Flood, Dennis J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1990
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 90-2529
Accession Number
90A52563
Distribution Limits
Public
Copyright
Other

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