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Properties of conductive coatings for thermal control mirrors and solar cell coversConductive transparent coatings applied to the dielectric surfaces of a spacecraft offer the possibility of distributing charge uniformly over the entire spacecraft surface. Optical and electrical measurements of such a coating as a function of temperature are described. These results are used in considering the impact of a conductive coating on the absorptance of thermal control mirrors and on the transmittance of solar cell cover glass, which can be improved by the application of an antireflection coating.
Document ID
19760004042
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Joslin, D. E. (Aerospace Corp. El Segundo, CA, United States)
Kan, H. K. A. (Aerospace Corp. El Segundo, CA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: NASA. Goddard Space Flight Center 8th Conf. on Space Simulation
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
PAPER-17
Accession Number
76N11130
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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