Aerospace Materials: TI-6AL-4V BAR
-320 to 800
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) | Fbru ksi (ksi) | Fcy ksi (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Fty ksi (ksi) | elongation pct (%) | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|
| TI-6AL-4V BAR | 70 | 16 | 220 | 132 | 82 | 138 | 128 | 10 | AMS 4928 | up to 2.0 in dia |
| TI-6AL-4V BAR | 200 | 15.4 | 202 | 112 | 76 | 126 | 108 | 10 | AMS 4928 | up to 2.0 in dia |
| TI-6AL-4V BAR | 300 | 15 | 190 | 105 | 72 | 118 | 100 | 10 | AMS 4928 | up to 2.0 in dia |
| TI-6AL-4V BAR | 400 | 14.6 | 178 | 97 | 67 | 110 | 93 | 10 | AMS 4928 | up to 2.0 in dia |
| TI-6AL-4V BAR | 600 | 13.9 | 156 | 82 | 58 | 96 | 78 | 10 | AMS 4928 | up to 2.0 in dia |
| TI-6AL-4V BAR | 800 | 13 | 126 | 62 | 46 | 78 | 58 | 10 | AMS 4928 | up to 2.0 in dia |
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