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A unique approach to fabricating precision space structures elementsA procedure of fabricating graphite epoxy columns used in the assembly of large space platforms is described. The requirement for precise dimensional control led to a unique hot resin injection process. Dry, high modulus fiber is wound over a vertically mounted steam-heated mandrel. A steam-heated sleeve or caul is slipped over the wound mandrel and resin is injected and cured in place. Approximately 200 column elements have been fabricated using this efficient process.
Document ID
19820033998
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Cohan, H.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Johnson, R. R.
(Lockheed Missiles and Space Co., Inc. Sunnyvale, CA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1981
Subject Category
Astronautics (General)
Meeting Information
Meeting: Composite structures
Location: Paisley
Start Date: September 16, 1981
End Date: September 18, 1981
Accession Number
82A17533
Funding Number(s)
CONTRACT_GRANT: NAS1-14887
Distribution Limits
Public
Copyright
Other

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