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Atomic oxygen effects on candidate coatings for long-term spacecraft in low earth orbitCandidate atomic oxygen protective coatings for long-term low Earth orbit (LEO) spacecraft were evaluated using the Los Alamos National Laboratory O-atom exposure facility. The coatings studied include Teflon, Al2O3, SiO2, and SWS-V-10, a silicon material. Preliminary results indicate that sputtered PTFE Teflon (0.1 micrometers) has a fluence lifetime of 10 to the 19th power O-atoms/cm (2), and sputtered silicon dioxide (0.1 micrometers), aluminum oxide (0.1 micrometers), and SWS-V-10, a silicone, (4 micrometers) have fluence lifetimes of 10 to the 20th power to 10 to the 21st power O-atoms/cm (2). There are large variations in fluence lifetime data for these coatings.
Document ID
19890003221
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lan, E. H.
(McDonnell-Douglas Corp. Huntington Beach, CA., United States)
Smith, Charles A.
(McDonnell-Douglas Corp. Huntington Beach, CA., United States)
Cross, J. B.
(Los Alamos National Lab. N. Mex., United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Publication Information
Publication: NASA, Goddard Space Flight Center, 15th Space Simulation Conference: Support the Highway to Space Through Testing
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
89N12592
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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