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Development of ultraviolet rigidizable materialsA series of tests was performed to determine an optimum resin to be used as a UV rigidizable matrix in expandable rigidizable space structures. Commercially available resins including several types of polyesters, epoxies, epoxy-acrylics, an acrylic and a urethane were used as well as a polyester, produced by 3M Company's Solar Laboratory facility, which was found the best from the standpoint of physical properties and ability to be 'B' staged. Two other synthesized materials were also tested, but were not found to be superior to the Solar resin. An optimum fabric for use with the preferred resin was not found; however, the 15 ounce fabric from Solar Laboratories has the best combination of physical properties with respect to handling and processing characteristics. Expansion techniques for tubular structures, 'B' staging of the solar resin, and stowage techniques for up to 5 months were developed. A one meter high tetrahedron preprototype structure was prepared to evaluate and demonstrate stowage, deployment, and rigidization techniques.
Document ID
19800014004
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Salisbury, D. P.
(Hughes Aircraft Co. Culver City, CA, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1979
Subject Category
Nonmetallic Materials
Report/Patent Number
HAC-F2545
FR-79-76-1290
NASA-CR-161426
Report Number: HAC-F2545
Report Number: FR-79-76-1290
Report Number: NASA-CR-161426
Accession Number
80N22491
Funding Number(s)
CONTRACT_GRANT: NAS8-32895
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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