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Aerospace Materials: TI-6AL-4V FORGING AB-ANN

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: TI-6AL-4V FORGING AB-ANN5 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)Ftu ksi ST (ksi)Fty ksi (ksi)Fty ksi LT (ksi)Fty ksi ST (ksi)G Msi (Msi)RA pct (%)RA pct LT (%)RA pct ST (%)basisconditiondensity lb in3 (lb/in^3)elongation pct (%)elongation pct LT (%)elongation pct ST (%)formpoisson ratiospecificationthickness range
TI-6AL-4V FORGING AB-ANN 2.000 S T5 4 1 0f C17016.917.21351351251256.52520SAlpha-beta processed, annealed0.161010Die forging0.31AMS 49282.000
TI-6AL-4V FORGING AB-ANN 2.000 S T5 4 1 0f C47016.917.21301301201206.51515SAlpha-beta or beta processed, annealed0.1688Die forging0.31AMS 49202.000
TI-6AL-4V FORGING AB-ANN 2.001-4.000 S7016.917.2203257171201123128791301301301201201206.5252015SAlpha-beta processed, annealed0.16101010Die forging0.31AMS 49282.001-4.000
TI-6AL-4V FORGING AB-ANN 2.001-6.000 S7016.917.2203257171201123128791301301301201201206.5151515SAlpha-beta or beta processed, annealed0.16888Die forging0.31AMS 49202.001-6.000
TI-6AL-4V FORGING AB-ANN 4.001-6.000 S7016.917.2203257171201123128791301301301201201206.5202015SAlpha-beta processed, annealed0.1610108Die forging0.31AMS 49284.001-6.000

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