Aerospace Materials: TI-6AL-4V EXTRUSION 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) | 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) | G Msi (Msi) | RA pct (%) | RA pct LT (%) | basis | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct LT (%) | form | poisson ratio |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| TI-6AL-4V EXTRUSION UNK ANY S T5 4 1 0e C11 | 70 | 16.9 | 17.2 | 220 | 281 | 196 | 228 | 139 | 139 | 85 | 140 | 140 | 130 | 130 | 6.5 | 12 | 12 | S | 0.16 | 6 | 6 | Extrusion | 0.31 |
| TI-6AL-4V EXTRUSION UNK ANY S T5 4 1 0e C12 | 70 | 16.9 | 17.2 | 204 | 261 | 182 | 210 | 128 | 128 | 79 | 130 | 130 | 120 | 120 | 6.5 | 12 | 12 | S | 0.16 | 6 | 6 | Extrusion | 0.31 |
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