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Preliminary design of a 10-kW thermophotovoltaic system for space applicationsA very high degree of reflection of sub-bandgap energy photons from the cell back to the emitter was found to be crucial in achieving high efficiencies for a TPV system. Results show that small increases in reflectance above 0.85 lead to progressively larger increases in cell efficiency. In general, for a required power output, the radiator area, emitter temperature, emitter material and cell temperature may be chosen to satisfy various external constraints. The results can then be used to determine the optimum cell material and its operating temperature.
Document ID
19840024357
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Piszczor, M. F., Jr.
(NASA Lewis Research Center Cleveland, OH, United States)
Ghalla-Goradia, M.
(Cleveland State Univ.)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-2259
NAS 1.15:83768
NASA-TM-83768
Meeting Information
Meeting: Ann. Intersoc. Energy Conversion Eng. Conf. (IECEC)
Location: San Francisco, CA
Country: United States
Start Date: August 19, 1984
End Date: August 24, 1984
Sponsors: SAE, IEEE, AIChE, ACS, ANS, ASME, AIAA
Accession Number
84N32427
Funding Number(s)
PROJECT: RTOP 506-55-42
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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