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Aerospace Materials: 7050 EXTRUSION T74511

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: 7050 EXTRUSION T745115 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
7050 EXTRUSION T74511 1.001-2.000 S7010.310.710413584100636240736963593.9ST745110.1027Extrusion0.33AMS 43421.001-2.000
7050 EXTRUSION T74511 2.001-3.000 S7010.310.71001308298636140736863583.9ST745110.1027Extrusion0.33AMS 43422.001-3.000
7050 EXTRUSION T74511 3.001-4.000 S7010.310.7951258095645939736463563.9ST745110.1027Extrusion0.33AMS 43423.001-4.000
7050 EXTRUSION T74511 4.001-5.000 S7010.310.7911217892645738736463543.9ST745110.1027Extrusion0.33AMS 43424.001-5.000
7050 EXTRUSION T74511 LE1.000 S7010.310.710713986106636341737163603.9ST745110.1027Extrusion0.33AMS 4342<=1.000

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