Abstract
A procedure for 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.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
Bush, Harold G. and Mikulas, Martin M., JR. A nestable tapered column concept for large space structures, NASA TM X-73927, 1976.
Mikulas, Martin M., JR., Bush, Harold G. and Card, Michael F. Structural stiffness, strength and dynamics characteristics of large tetrahedral space truss structures, NASA TM X-74001, March 1977.
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 1981 Applied Science Publishers Ltd
About this chapter
Cite this chapter
Cohan, H., Johnson, R.R. (1981). A Unique Approach to Fabricating Precision Space Structures Elements. In: Marshall, I.H. (eds) Composite Structures. Springer, Dordrecht. https://doi.org/10.1007/978-94-009-8120-1_39
Download citation
DOI: https://doi.org/10.1007/978-94-009-8120-1_39
Publisher Name: Springer, Dordrecht
Print ISBN: 978-94-009-8122-5
Online ISBN: 978-94-009-8120-1
eBook Packages: Springer Book Archive