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High performance filament wound composites for pressure vessel applications.A new high modulus fiber was evaluated as a reinforcement for filament wound pressure vessels. Based on preliminary data it offers significant specific strength and modulus improvements over an S-glass reinforcement. Winding parameters and design data were established for the fiber with two different epoxy resin systems. NOL composite rings were evaluated for tensile strength, modulus and interlaminar shear strength at +70 F, -320 F and -423 F. Results showed that the fiber reinforced composite exhibited a specific strength of 4,100,000 inches and a specific modulus of 290,000,000 inches compared to 3,260,000 inches and 110,000,000 inches respectively for S-glass. Utilizing this data to design small filament wound pressure vessels, a performance factor of 806,000 inches was obtained experimentally with PRD 49-1 fiber compared to values of 632,000 inches and 501,000 inches for S-glass and high modulus graphite vessels, respectively.
Document ID
19720027075
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Hoggatt, J. T.
(Boeing Scientific Research Laboratories Seattle, Wash., United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Subject Category
Materials, Nonmetallic
Meeting Information
Meeting: Space shuttle materials; Proceedings of the National Technical Conference
Location: Huntsville, AL
Start Date: October 5, 1971
End Date: October 7, 1971
Accession Number
72A10741
Funding Number(s)
CONTRACT_GRANT: NAS3-13330
Distribution Limits
Public
Copyright
Other

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