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Protective coatings for composite tubes in space applicationsProtective coatings for graphite/epoxy (Gr/Ep) tubular structures for a Manned Space Station truss structure were evaluated. The success of the composite tube truss structure depends on its stability to long-term exposure to the Low Earth Orbit (LEO) environment with particular emphasis placed on atomic oxygen. Concepts for protectively coating Gr/Ep tubes include use of inorganic coated metal foils and electroplating. These coatings were applied to Gr/Ep tubes and then subjected to simulated LEO environmnet to evaluate survivability of coatings and coated tubes. Evaluation included: atomic oxygen resistance, changes in optical properties and adhesion, abrasion resistancem surface preparation required, coating uniformity, and formation of microcracks in the Gr/Ep tubes caused by thermal cycling. Program results demonstrated that both phosphoric and chromic acid anodized Al foil provided excellent adhesion to Gr/Ep tubes and exhibited stable optical properties when subjected to simulated LEO environment. The SiO2/Al coatings speuttered onto Al foils also resulted in an excellent protective coating. Electroplated Ni exhibited unaccepatble adhesion loss to Gr/Ep tubes during atomic oxygen exposure.
Document ID
19870009236
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dursch, Harry W.
(Boeing Aerospace Co. Seattle, WA, United States)
Hendricks, Carl L.
(Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Subject Category
Nonmetallic Materials
Report/Patent Number
NAS 1.26:178116
NASA-CR-178116
Report Number: NAS 1.26:178116
Report Number: NASA-CR-178116
Accession Number
87N18669
Funding Number(s)
CONTRACT_GRANT: NAS1-16854
PROJECT: RTOP 506-43-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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