Aerospace Materials: TI-4.5AL-3V-2FE-2MO BAR UNK
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 | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct LT (%) | form | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| TI-4.5AL-3V-2FE-2MO BAR UNK 2.000 A | 70 | 16 | 16.2 | 124 | 81 | 135 | 135 | 124 | 125 | 25 | 20 | A | 0.164 | 10 | 10 | Bar | 2.000 |
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