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Solar concentrator advanced development projectA solar dynamic concentrator design developed for use with a solar-thermodynamic power generation module intended for the Space Station is considered. The truss hexagonal panel reflector uses a modular design approach and is flexible in attainable flux profiles and assembly techniques. Preliminary structural, thermal, and optical analysis results are discussed. Accuracy of the surface reflectors should be within 5 mrad rms slope error, resulting in the need for close fabrication tolerances. Significant fabrication issues to be addressed include the facet reflective and protective coating processes and the surface specularity requirements.
Document ID
19880024572
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Corrigan, Robert D.
(NASA Lewis Research Center Cleveland, OH, United States)
Ehresman, Derik T.
(Harris Corp. Melbourne, FL, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: IECEC ''87
Location: Philadelphia, PA
Country: United States
Start Date: August 10, 1987
End Date: August 14, 1987
Accession Number
88A11799
Distribution Limits
Public
Copyright
Other

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