Fracture and subcritical flaw growth characteristics were experimentally determined for electroless nickel plated D6 steel in dry air and high pressure oxygen environments as applicable to the Lunar Module/Environmental Control System (LM/ECS) descent gaseous oxygen (GOX) tank. The material tested included forgings, plate, and actual LM/ECS descent GOX tank material. Parent metal and TIG (tungsten inert gas) welds were tested. Tests indicate that proof testing the tanks at 4000 pounds per square inch or higher will insure safe operation at 3060 pounds per square inch. Although significant flaw growth can occur during proofing, subsequent growth of flaws during normal tank operation is negligible
Comparison of flaw growth characteristics under cryogenic proof and ambient test conditions for Apol...
Visual flaw detection method for metals utilizes color precipitate. This method can be used safely i...
Flaw growth rates and fracture toughness data for materials used in thick walled cylindrical tank
Results of sustained-load environmental crack growth threshold tests performed on six spacecraft pre...
Crack growth threshold investigation of Inconel 718 exposed to high pressure oxyge
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...
Fracture and crack growth for welded joints of 5Al-2.5Sn titanium in environment of low pressure, hi...
Failure analysis of flaw growth characteristics of 6Al-4V titanium forgings used in Apollo spacecraf...
The Green Propellant Infusion Mission (GPIM) will demonstrate the performance of AF-M315E monopropel...
Growth of deep surface flaws in thin wall tanks of aluminum and titanium base metal
This experimental program was undertaken to determine the effects of (1) combined tensile and bendin...
This experimental program was divided into two parts. The first part evaluated stress corrosion crac...
Brief discussions of the materials and configurations testing techniques and requirements for the Ap...
Conditions controlling the growth and fracture of deep surface flaws in aerospace alloys were invest...
Comparison of flaw growth characteristics under cryogenic proof and ambient test conditions for Apol...
Visual flaw detection method for metals utilizes color precipitate. This method can be used safely i...
Flaw growth rates and fracture toughness data for materials used in thick walled cylindrical tank
Results of sustained-load environmental crack growth threshold tests performed on six spacecraft pre...
Crack growth threshold investigation of Inconel 718 exposed to high pressure oxyge
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...
Fracture and crack growth for welded joints of 5Al-2.5Sn titanium in environment of low pressure, hi...
Failure analysis of flaw growth characteristics of 6Al-4V titanium forgings used in Apollo spacecraf...
The Green Propellant Infusion Mission (GPIM) will demonstrate the performance of AF-M315E monopropel...
Growth of deep surface flaws in thin wall tanks of aluminum and titanium base metal
This experimental program was undertaken to determine the effects of (1) combined tensile and bendin...
This experimental program was divided into two parts. The first part evaluated stress corrosion crac...
Brief discussions of the materials and configurations testing techniques and requirements for the Ap...
Conditions controlling the growth and fracture of deep surface flaws in aerospace alloys were invest...
Comparison of flaw growth characteristics under cryogenic proof and ambient test conditions for Apol...
Visual flaw detection method for metals utilizes color precipitate. This method can be used safely i...
Flaw growth rates and fracture toughness data for materials used in thick walled cylindrical tank