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Large boron--epoxy filament-wound pressure vessels
- Publication Year :
- 1973
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1973.
-
Abstract
- Advanced composite material used to fabricate pressure vessel is prepeg (partially cured) consisting of continuous, parallel boron filaments in epoxy resin matrix arranged to form tape. To fabricate chamber, tape is wound on form which must be removable after composite has been cured. Configuration of boron--epoxy composite pressure vessel was determined by computer program.
- Subjects :
- Fabrication Technology
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Publication Type :
- Report
- Accession number :
- edsnas.19730000038
- Document Type :
- Report