Results of sustained-load environmental crack growth threshold tests performed on six spacecraft pressure vessel alloys are presented. The alloys were Inconel 718, 6Al-4V titanium, A-286 steel, AM-350 stainless steel, cryoformed AISI 301 stainless steel; and cryoformed AISI 304L steel. The test environments for the program were air, pressurized gases of hydrogen, oxygen, nitrogen, and carbon dioxide, and liquid environments of distilled water, sea water, nitrogen tetroxide, hydrazine, aerozine 50, monomethyl hydrazine, and hydrogen peroxide. Surface flaw type specimens were used with flaws located in both base metal and weld metal
Results of mechanical-properties and axial-load fatigue and fracture tests performed on thick welded...
Candidate alloys for the Shuttle Solid Rocket Booster (SRB) case were tested under simulated service...
To provide NASA with a suite of materials strength, fracture toughness and crack growth rate test re...
This experimental program was undertaken to determine the effects of combined cyclic/sustained loads...
Crack propagation in aluminum notched tensile and pressure vessel specimens cyclically loaded at cry...
This experimental program was divided into two parts. The first part evaluated stress corrosion crac...
The elastic fracture toughness of the three steels is shown to not decrease significantly with decre...
Fracture and subcritical flaw growth characteristics were experimentally determined for electroless ...
Stress corrosion cracking (SSC) tests were performed on 13 aluminum alloys, 13 precipitation hardeni...
The plane strain threshold stress intensity and sustained stress flaw growth rates were experimental...
The aluminum alloy 2219-T87 has great potential for use as a cryogenic material for various manned a...
After nearly 53 months of exposure to marine atmosphere, crack growth in SL DCB specimens from 7075,...
Unexpected occurrence of failures, due to stress corrosion cracking (SCC) of structural components, ...
Conditions controlling the growth and fracture of deep surface flaws in aerospace alloys were invest...
The Green Propellant Infusion Mission (GPIM) will demonstrate the performance of AF-M315E monopropel...
Results of mechanical-properties and axial-load fatigue and fracture tests performed on thick welded...
Candidate alloys for the Shuttle Solid Rocket Booster (SRB) case were tested under simulated service...
To provide NASA with a suite of materials strength, fracture toughness and crack growth rate test re...
This experimental program was undertaken to determine the effects of combined cyclic/sustained loads...
Crack propagation in aluminum notched tensile and pressure vessel specimens cyclically loaded at cry...
This experimental program was divided into two parts. The first part evaluated stress corrosion crac...
The elastic fracture toughness of the three steels is shown to not decrease significantly with decre...
Fracture and subcritical flaw growth characteristics were experimentally determined for electroless ...
Stress corrosion cracking (SSC) tests were performed on 13 aluminum alloys, 13 precipitation hardeni...
The plane strain threshold stress intensity and sustained stress flaw growth rates were experimental...
The aluminum alloy 2219-T87 has great potential for use as a cryogenic material for various manned a...
After nearly 53 months of exposure to marine atmosphere, crack growth in SL DCB specimens from 7075,...
Unexpected occurrence of failures, due to stress corrosion cracking (SCC) of structural components, ...
Conditions controlling the growth and fracture of deep surface flaws in aerospace alloys were invest...
The Green Propellant Infusion Mission (GPIM) will demonstrate the performance of AF-M315E monopropel...
Results of mechanical-properties and axial-load fatigue and fracture tests performed on thick welded...
Candidate alloys for the Shuttle Solid Rocket Booster (SRB) case were tested under simulated service...
To provide NASA with a suite of materials strength, fracture toughness and crack growth rate test re...