Sample data from Engineering Database — 375 reference tables, deterministic calculators, and Engineering AI. Sign up free
Home/Reference Data/Aerospace Materials/TI-10V-2FE-3AL FORGING STA

Aerospace Materials: TI-10V-2FE-3AL FORGING STA

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-10V-2FE-3AL FORGING STA4 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)RA pct (%)RA pct LT (%)basisconditiondensity lb in3 (lb/in^3)elongation pct (%)elongation pct LT (%)elongation pct ST (%)formspecificationthickness range
TI-10V-2FE-3AL FORGING STA 3.001-4.000 S7015.916.31601601451451010SSolution treated and aged (950-1000(F)0.16866Hand forgingAMS 49863.001-4.000
TI-10V-2FE-3AL FORGING STA LT1.000 S7015.916.3244295227261168166101180180160160SSolution treated and aged (900-950(F)0.16844Conventional die forgingAMS 4983<1.000
TI-10V-2FE-3AL FORGING STA LT3.000 S T5 5 3 0b C27015.916.323428422726116816616697173173173160160160SSolution treated and aged (900-950(F)0.168444Conventional die forgingAMS 4984<3.000
TI-10V-2FE-3AL FORGING STA LT3.000 S T5 5 3 0c C17015.916.3241293218245154971601601451451010SSolution treated and aged (950-1000(F)0.16866Hand forgingAMS 4986<3.000

What else is in Engineering Database

Related data