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The effects of simulated low Earth orbit environments on spacecraft thermal control coatingsCandidate Space Station Freedom radiator coatings including Z-93, YB-71, anodized aluminum and SiO(x) coated silvered Teflon have been characterized for optical properties degradation upon exposure to environments containing atomic oxygen, vacuum ultraviolet (VUV) radiation, and/or silicone contamination. YB-71 coating showed a blue-gray discoloration, which has not been observed in space, upon exposure in atomic oxygen facilities which also provide exaggerated VUV radiation. This is evidence that damage mechanisms occur in these ground laboratory facilities which are different from those which occur in space. Radiator coatings exposed to an electron cyclotron resonance (ECR) atomic oxygen source in the presence of silicone-containing samples showed severe darkening from the intense VUV radiation provided by the ECR and from silicone contamination. Samples exposed to atomic oxygen from the ECR source and to VUV lamps, simultaneously, with in situ reflectance measurement, showed that significantly greater degradation occurred when samples received line-of-site ECR beam exposure than when samples were exposed to atomic oxygen scattered off of quartz surfaces without line-of-site view of the ECR beam. For white paints, exposure to air following atomic oxygen/VUV exposure reversed the darkening due to VUV damage. This illustrates the importance of in situ reflectance measurement.
Document ID
19930017830
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dever, Joyce A.
(NASA Lewis Research Center Cleveland, OH, United States)
Rutledge, Sharon K.
(NASA Lewis Research Center Cleveland, OH, United States)
Bruckner, Eric J.
(Cleveland State Univ. OH., United States)
Stidham, Curtis R.
(Sverdrup Technology, Inc. Brook Park, OH., United States)
Stueber, Thomas J.
(Sverdrup Technology, Inc. Brook Park, OH., United States)
Booth, Roy E.
(Vought Corp. Dallas, TX., United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1993
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:106146
NASA-TM-106146
E-7829
Meeting Information
Meeting: International SAMPE Symposium and Exhibition
Location: Anaheim, CA
Country: United States
Start Date: May 10, 1993
End Date: May 13, 1993
Sponsors: Society for the Advancement of Materials and Process Engineering
Accession Number
93N27019
Funding Number(s)
PROJECT: RTOP 474-46-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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