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Development of structural composite mirror technology for submillimeter space telescopesThe technical approach to the design, manufacturing, testing, and analytical simulation of lightweight graphite/epoxy mirrors is described. The precision segmented reflector (PSR) program has produced (1) 1.0-m graphite/epoxy panels with areal densities of 7 kg/sq m as-manufactured surface precision near 1 micron rms, (2) 0.5-m panels with figure changes less than 1 micron rms for temperature reductions of 100 K, (3) analytical performance-prediction capability with submicron accuracy relative to panel thermal distortion, and (4) a unique thermal vacuum test facility for structural composite mirrors.
Document ID
19920032109
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Freeland, R. E.
(JPL Pasadena, CA, United States)
Johnston, R. D.
(Hexcel Corp. Dublin, CA, United States)
Date Acquired
August 15, 2013
Publication Date
October 1, 1991
Subject Category
Astronomy
Report/Patent Number
IAF PAPER 91-317
Report Number: IAF PAPER 91-317
Accession Number
92A14733
Distribution Limits
Public
Copyright
Other

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