NASA NTRS · 19820033998
A unique approach to fabricating precision space structures elements
Abstract
A 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.
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Cohan, H., Johnson, R. R.. 1981-01-01. A unique approach to fabricating precision space structures elements. https://ntrs.nasa.gov/citations/19820033998
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