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Metal-Clad Graphite/Epoxy TubesStructural parts feature low weight, low thermal expansion, and high stiffness. Unique, non-labor-intensive manufacturing process developed for fabricating aluminum-clad graphite/epoxy (Gr/E) struts which meet Space Station requirements. Method of manufacturing struts provides procedure for using Gr/E material system in very efficient manner. Technique places all fibers in longitudinal direction for stiffness and strength. Aluminum surfaces provide transverse strength and resistance to atomic oxygen in environment.
Document ID
19870000252
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Bush, Harold G.
(NASA Langley Research Center, Hampton, Va.)
Bluck, Raymond M.
(Lockheed Missiles and Space Company)
Johnson, Robert R.
(Lockheed Missiles and Space Company)
Date Acquired
August 13, 2013
Publication Date
May 1, 1987
Publication Information
Publication: NASA Tech Briefs
Volume: 11
Issue: 5
ISSN: 0145-319X
Subject Category
Fabrication Technology
Report/Patent Number
LAR-13562
ISSN: 0145-319X
Report Number: LAR-13562
Accession Number
87B10252
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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