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Aerospace Materials: 2024 EXTRUSION T81

Aerospace material mechanical properties and design allowables at ambient, elevated, and cryogenic temperatures per MMPDS-11 (Metallic Materials Properties Development and Standardization). Covers primary structural alloys: aluminum (2024-T3, 7075-T6, 6061-T6, 2219-T87), titanium (Ti-6Al-4V), nickel superalloys (Inconel 718), and steels (300M, 4130, 4340).

Materials Sciencematerial id: 2024 EXTRUSION T813 rows
material idtemp fE Msi (Msi)Ec Msi (Msi)Fbru ksi (ksi)Fbru ksi 2 (ksi)Fbry ksi (ksi)Fbry ksi 2 (ksi)Fcy ksi (ksi)Fcy ksi LT (ksi)Fsu ksi (ksi)Ftu ksi (ksi)Ftu ksi LT (ksi)Fty ksi (ksi)Fty ksi LT (ksi)G Msi (Msi)basisconditiondensity lb in3 (lb/in^3)elongation pct (%)formpoisson ratiospecificationthickness range
2024 EXTRUSION T81 0.050-0.249 S7010.811941237993575735646456554.1ST81, T8510, and T85110.14Extruded bar, rod, and shapes0.33AMS-QQ-A-200/30.050-0.249
2024 EXTRUSION T81 0.250-1.499 S7010.811961238296595936666458574.1ST81, T8510, and T85110.15Extruded bar, rod, and shapes0.33AMS-QQ-A-200/30.250-1.499
2024 EXTRUSION T81 1.500-4.500 S7010.811921178296595936666158574.1ST81, T8510, and T85110.15Extruded bar, rod, and shapes0.33AMS-QQ-A-200/31.500-4.500

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