Mechanical Properties | Metric | English | Comments |
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Tensile Strength, Ultimate | 1138 MPa | 165100 psi | |
Haynes Hastelloy® C-22® alloy, 20% cold worked sheet, aged 100 hours at 500°C HASTELLOY® C-22® alloy is a nickel-chromium-molybdenum-tungsten alloy with excellent overall corrosion resistance compared to other Ni-Cr-Mo alloys, including HASTELLOY C-276 and C-4 alloys an.. |
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Tensile Strength, Ultimate | 1138 MPa | 165100 psi | |
ATI Allvac® Ti-17 Titanium Alloy, Heat Treatment: 899°C (1650°F) + Age Data provided by Allvac.Applications: Compressor discs, heavy section forgings for gas turbine engine components. High tensile strength and good fracture toughness. |
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Tensile Strength, Ultimate | >= 1138 MPa | >= 165100 psi | AMS 5542 aged, sheet |
ATI Allegheny Ludlum Altemp® X-750 Nickel-Based superalloy Characteristics: precipitation hardenable, high strength up to 1300°F, oxidation resistant up to 1800°F. Applications: aerospace, heat treatment fixtures, forming tools, extrusion dies.Information.. |