Aerospace Materials: TI-4.5AL-3V-2FE-2MO SHEET ANN 0.063-0.187 EXCLUSIV
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) | 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) | Fty ksi (ksi) | Fty ksi LT (ksi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct LT (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| TI-4.5AL-3V-2FE-2MO SHEET ANN 0.063-0.187 EXCLUSIV A | 70 | 16 | 16.2 | 207 | 276 | 165 | 198 | 130 | 132 | 91 | 134 | 134 | 126 | 126 | A | Annealed | 0.164 | 10 | 10 | Sheet | AMS 4899 | 0.063 to 0.187, exclusive |
| TI-4.5AL-3V-2FE-2MO SHEET ANN 0.063-0.187 EXCLUSIV B | 70 | 16 | 16.2 | 223 | 296 | 176 | 210 | 139 | 141 | 98 | 144 | 144 | 132 | 134 | B | Annealed | 0.164 | — | — | Sheet | AMS 4899 | 0.063 to 0.187, exclusive |
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