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Design considerations for long-lived glass mirrors for spaceLarge mirrors intended for long-term operation in orbital space will have to retain high reflectance in the presence of contamination or destruction by high-energy particles, meteorites, and orbiting debris. These conditions require the use of low-energy outer surfaces that resist the buildup of contamination, the use of small mirror segments that restrict local damage and facilitate replacement, and the use of surface coatings that minimize the effects of atomic oxygen and/or charge buildup. The present recommendations are based on experience accumulated with terrestrial solar-concentrator mirror materials.
Document ID
19870049257
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bouquet, Frank L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Maag, Carl R.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Heggen, Philip M.
(Energy General Menlo Park, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Optics
Accession Number
87A36531
Distribution Limits
Public
Copyright
Other

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