NDLI: Glass-fiber-reinforced metallic tanks for cryogenic service

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Glass-fiber-reinforced metallic tanks for cryogenic service

Content Provider	NASA Technical Reports Server (NTRS)
Author	Morris, E. E.
Organization	The National Aeronautics and Space Administration (NASA)
Copyright Year	1967
Abstract	Advantages of and design requirements for a load-bearing metal shell with an overwrapped glass-filament shell for high-pressure-fluid storage at 75 to -423 deg F were investigated analytically and experimentally. Proper design permits utilization of the maximum load-bearing capabilities of both shells and makes possible tanks of significantly lighter weight than the best cylindrical and spherical homogeneous metal pressure vessels. Glass-fiber-reinforced metal tanks were fabricated and tested; they successfully met design objectives in cyclic fatigue, creep, and burst tests in the 75 t o -423 deg F range, and should be considered for application to aerospace systems. The testing (1) confirmed the results of a parametric study of the vessels, (2) revealed that no degradation in tank strength resulted from cyclic fatigue and sustained-loading tests at 75, -320, and -423 deg F, and (3) established that vessel strength increased about 25% at cryogenic temperatures.
File Size	77220875
File Format	PDF
Alternate Webpage(s)	http://www.archive.org/details/nasa_techdoc_19680002620
Archival Resource Key	ark:/13960/t6h13qj3w
Language	English
Publisher Date	1967-06-01
Access Restriction	Open
Subject Keyword	Cryogenic Fluid Storage Loads (forces) Materials Tests Pressure Vessels Reinforcing Fibers Storage Tanks Glass Fibers Metal Shells Reinforced Shells Creep Properties Cylindrical Shells Fuel Tanks High Pressure Loading Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text

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