Filament 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
Filament tensile strengths and pressure-strain characteristics of high modulus, high-strength, boron...
A theoretical investigation of the factors controlling the stress rupture life of the National Aeron...
By the beginning of the 1970's composite pressure vessels had received a significant amount of devel...
Two different Kevlar-49 filament-reinforced metal sphere designs were developed, and six vessels of ...
A high modulus polymeric fiber was evaluated as a reinforcement for filament wound pressure vessels....
This experimental program was undertaken to establish a fracture control method for composite tanks ...
The experimental program was based on the premise that the plastic sizing cycle, which each pressure...
The development of structurally efficient, metal-lined, glass-fiber composite pressure vessels. Both...
A review of recent advances is presented for lightweight, high performance composite pressure vessel...
Bosses were made of fiber/resin composite materials to evaluate their potential in lightweight press...
The NASA Engineering and Safety Center (NESC) has been conducting an independent technical assessmen...
Work is reported for fabricating and testing the fiberglass overwrapped titanium pressure vessel for...
A theoretical investigation of the factors controlling the stress rupture life of the National Aeron...
Acoustic emissions (AE) generated from Kevlar 49/epoxy composite pressure vessels subjected to susta...
This paper reports stress rupture testing of Kevlar(TradeMark) composite overwrapped pressure vessel...
Filament tensile strengths and pressure-strain characteristics of high modulus, high-strength, boron...
A theoretical investigation of the factors controlling the stress rupture life of the National Aeron...
By the beginning of the 1970's composite pressure vessels had received a significant amount of devel...
Two different Kevlar-49 filament-reinforced metal sphere designs were developed, and six vessels of ...
A high modulus polymeric fiber was evaluated as a reinforcement for filament wound pressure vessels....
This experimental program was undertaken to establish a fracture control method for composite tanks ...
The experimental program was based on the premise that the plastic sizing cycle, which each pressure...
The development of structurally efficient, metal-lined, glass-fiber composite pressure vessels. Both...
A review of recent advances is presented for lightweight, high performance composite pressure vessel...
Bosses were made of fiber/resin composite materials to evaluate their potential in lightweight press...
The NASA Engineering and Safety Center (NESC) has been conducting an independent technical assessmen...
Work is reported for fabricating and testing the fiberglass overwrapped titanium pressure vessel for...
A theoretical investigation of the factors controlling the stress rupture life of the National Aeron...
Acoustic emissions (AE) generated from Kevlar 49/epoxy composite pressure vessels subjected to susta...
This paper reports stress rupture testing of Kevlar(TradeMark) composite overwrapped pressure vessel...
Filament tensile strengths and pressure-strain characteristics of high modulus, high-strength, boron...
A theoretical investigation of the factors controlling the stress rupture life of the National Aeron...
By the beginning of the 1970's composite pressure vessels had received a significant amount of devel...