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Aerospace Materials: 6061 FORGING T6A and T652

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: 6061 FORGING T6A and T6523 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)Fcy ksi ST (ksi)Fsu ksi (ksi)Ftu ksi (ksi)Ftu ksi LT (ksi)Ftu ksi ST (ksi)Fty ksi (ksi)Fty ksi LT (ksi)Fty ksi ST (ksi)G Msi (Msi)basisconditiondensity lb in3 (lb/in^3)elongation pct (%)elongation pct LT (%)elongation pct ST (%)formpoisson ratiospecificationthickness range
6061 FORGING T6A AND T652 2.000 S709.910.161765461363625383835353.8ST6a and T6520.098108Hand forging0.33AMS 4127, AMS 4248, AMS-A-22771, and AMS-QQ-A-3672.000
6061 FORGING T6A AND T652 2.001-4.000 S709.910.161765461363634253838373535333.8ST6a and T6520.0981085Hand forging0.33AMS 4127, AMS 4248, AMS-A-22771, and AMS-QQ-A-3672.001-4.000
6061 FORGING T6A AND T652 4.001-8.000 S709.910.159745359353533243737353434323.8ST6a and T6520.098864Hand forging0.33AMS 4127, AMS 4248, AMS-A-22771, and AMS-QQ-A-3674.001-8.000

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