Aerospace Materials: TI-4.5AL-3V-2FE-2MO BAR 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).
| material id | temp f | E Msi (Msi) | Ec Msi (Msi) | Fcy ksi (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Ftu ksi LT (ksi) | Fty ksi (ksi) | Fty ksi LT (ksi) | RA pct (%) | RA pct LT (%) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct LT (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| TI-4.5AL-3V-2FE-2MO BAR ANN 2.000 B | 70 | 16 | 16.2 | 128 | 84 | 139 | — | 128 | — | — | — | B | Annealed | 0.164 | — | — | Bar | AMS 4964 | 2.000 |
| TI-4.5AL-3V-2FE-2MO BAR ANN 2.001-4.000 A | 70 | 16 | 16.2 | — | — | 130 | 130 | 119 | 120 | 20 | 20 | A | Annealed | 0.164 | 10 | 10 | Bar | AMS 4964 | 2.001-4.000 |
| TI-4.5AL-3V-2FE-2MO BAR ANN 2.001-4.000 B | 70 | 16 | 16.2 | — | — | 135 | — | 123 | — | — | — | B | Annealed | 0.164 | — | — | Bar | AMS 4964 | 2.001-4.000 |
| TI-4.5AL-3V-2FE-2MO BAR ANN 4.001-6.000 A | 70 | 16 | 16.2 | — | — | 130 | 130 | 119 | 120 | 20 | 20 | A | Annealed | 0.164 | 10 | 10 | Bar | AMS 4964 | 4.001-6.000 |
| TI-4.5AL-3V-2FE-2MO BAR ANN 4.001-6.000 B | 70 | 16 | 16.2 | — | — | 133 | — | 123 | — | — | — | B | Annealed | 0.164 | — | — | Bar | AMS 4964 | 4.001-6.000 |
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