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Composite materials for precision space reflector panelsOne of the critical technology needs of large precision reflectors for future astrophysical and optical communications satellites lies in the area of structural materials. Results from a materials research and development program at NASA Langley Research Center to provide materials for these reflector applications are discussed. Advanced materials that meet the reflector panel requirements are identified, and thermal, mechanical and durability properties of candidate materials after exposure to simulated space environments are compared. A parabolic, graphite-phenolic honeycomb composite panel having a surface accuracy of 70.8 microinches rms and an areal weight of 1.17 lbm/sq ft was fabricated with T50/ERL1962 facesheets, a PAEI thermoplastic surface film, and Al and SiO(x) coatings.
Document ID
19930045792
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tompkins, Stephen S.
(NASA Langley Research Center Hampton, VA, United States)
Funk, Joan G.
(NASA Langley Research Center Hampton, VA, United States)
Bowles, David E.
(NASA Langley Research Center Hampton, VA, United States)
Towell, Timothy W.
(NASA Langley Research Center Hampton, VA, United States)
Connell, John W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: Design of optical instruments; Proceedings of the Meeting, Orlando, FL, Apr. 22-24, 1992 (A93-29781 11-74)
Publisher: Society of Photo-Optical Instrumentation Engineers
Subject Category
Composite Materials
Accession Number
93A29789
Distribution Limits
Public
Copyright
Other

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