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Thin-metal lined PRD 49-III composite vesselsFilament wound pressure vessels of various configurations were evaluated for burst strength and fatigue performance. The dimensions and characteristics of the vessels are described. The types of tests conducted are explained. It was determined that all vessels leaked in a relatively few cycles (20 to 60 cycles) with failure occurring in all cases in the metallic liner. The thin liner would de-bond from the composite and buckling took place during depressurization. No composite failures or indications of impeding composite failures were obtained in the metal-lined vessels.
Document ID
19740011430
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hoggatt, J. T. (Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1974
Subject Category
Structural Mechanics
Report/Patent Number
ASG-2-5540
NASA-CR-134555
Accession Number
74N19543
Funding Number(s)
CONTRACT_GRANT: NAS3-15840
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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