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Aerospace Materials: 7050 FORGING T74

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 FORGING T744 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 ST (ksi)Fsu ksi (ksi)Ftu ksi (ksi)Fty ksi (ksi)G Msi (Msi)basisconditiondensity lb in3 (lb/in^3)elongation pct (%)formpoisson ratiospecification
7050 FORGING T74 ANY S T3 7 4 0c1 C17010.210.799131829663604272623.9ST74a0.1027Die forging0.33AMS 4107 and AMS-A-22771
7050 FORGING T74 ANY S T3 7 4 0c1 C27010.210.798129819563594271613.9ST74a0.1027Die forging0.33AMS 4107 and AMS-A-22771
7050 FORGING T74 ANY S T3 7 4 0c1 C37010.210.797127789263584170603.9ST74a0.1027Die forging0.33AMS 4107 and AMS-A-22771
7050 FORGING T74 ANY S T3 7 4 0c1 C47010.210.797127789262574170593.9ST74a0.1027Die forging0.33AMS 4107 and AMS-A-22771

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