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Filament-wound composite vessels material technologyPrograms are reviewed that were conducted to establish a technology base for applying advanced fibers or resins to high performance filament-wound pressure vessels for containment of cryogens and high pressure gases. Materials evaluated included boron, graphite, PRD 49-1 and 3/epoxy and S-glass/polyimide composites. Closed-end cylindrical, and oblate spheroid-shaped vessels were fabricated in 4- and 8-inch diameter sizes. Vessels were subjected to single-cycle burst, low-cycle fatigue, and sustained loading tests over a -423 F to room temperature range for epoxy composites and a -423 to 500 F temperature range for the polyimide composites. Vessels tested at cryogenic and/or 500 F had thin (3 to 20 mils) metallic liners whereas vessels tested at room temperature had elastomeric liners. Correlations between acoustic emissions and burst and cyclic properties of PRD 49-1 filament-wound vessels are discussed.
Document ID
19730011196
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lark, R. F.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1973
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-68196
E-7357
Report Number: NASA-TM-X-68196
Report Number: E-7357
Meeting Information
Meeting: Intern. Conf. on Pressure Vessel Technol.,
Location: San Antonio, TX
Country: United States
Start Date: October 1, 1973
End Date: October 4, 1973
Sponsors: ASME
Accession Number
73N19923
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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