Add to ORKGA high modulus polymeric fiber was evaluated as a reinforcement for filament wound pressure vessels. Winding parameters and design data were established for the fiber with two different epoxy resin systems. Comparison was made between the performance factors of the polymeric fiber and those of S-glass and high modulus graphite vessels
Interlaminar-shear testing of resin-filament wound composite materials for cryogenic us
By the beginning of the 1970's composite pressure vessels had received a significant amount of devel...
To achieve NASA's mission of space exploration, innovative manufacturing processes are being applied...
Filament tensile strengths and pressure-strain characteristics of high modulus, high-strength, boron...
Filament wound NOL rings, 4-inch and 8-inch diameter closed-end vessels involving three epoxy resin ...
The work performed in selecting a TRW A-type polyimide resin that would be suitable for fabrication ...
Filament wound pressure vessels of various configurations were evaluated for burst strength and fati...
Advanced unidirectional and bidirectional carbon fiber/epoxy resin composites were evaluated for phy...
A review of recent advances is presented for lightweight, high performance composite pressure vessel...
Tensile and interlaminar shear strengths of glass, boron, and graphite filament wound resin composit...
Tensile strength properties of glass, boron, and graphite filament wound resin composites and liners...
Internal pressure vessels were designed; the filament was wound of carbon fibers and epoxy resin and...
Two different Kevlar-49 filament-reinforced metal sphere designs were developed, and six vessels of ...
Bonded plastic tape liner for filament-wound glass fiber cryogenic propellant tan
The Engineering Guide presents curves and general equations for safelife design of lightweight glass...
Interlaminar-shear testing of resin-filament wound composite materials for cryogenic us
By the beginning of the 1970's composite pressure vessels had received a significant amount of devel...
To achieve NASA's mission of space exploration, innovative manufacturing processes are being applied...
Filament tensile strengths and pressure-strain characteristics of high modulus, high-strength, boron...
Filament wound NOL rings, 4-inch and 8-inch diameter closed-end vessels involving three epoxy resin ...
The work performed in selecting a TRW A-type polyimide resin that would be suitable for fabrication ...
Filament wound pressure vessels of various configurations were evaluated for burst strength and fati...
Advanced unidirectional and bidirectional carbon fiber/epoxy resin composites were evaluated for phy...
A review of recent advances is presented for lightweight, high performance composite pressure vessel...
Tensile and interlaminar shear strengths of glass, boron, and graphite filament wound resin composit...
Tensile strength properties of glass, boron, and graphite filament wound resin composites and liners...
Internal pressure vessels were designed; the filament was wound of carbon fibers and epoxy resin and...
Two different Kevlar-49 filament-reinforced metal sphere designs were developed, and six vessels of ...
Bonded plastic tape liner for filament-wound glass fiber cryogenic propellant tan
The Engineering Guide presents curves and general equations for safelife design of lightweight glass...
Interlaminar-shear testing of resin-filament wound composite materials for cryogenic us
By the beginning of the 1970's composite pressure vessels had received a significant amount of devel...
To achieve NASA's mission of space exploration, innovative manufacturing processes are being applied...