Aerospace Materials: TI-6AL-4V 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) | 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 BAR UNK ANY S T5 4 1 0d C3 | 70 | 16.9 | 17.2 | 150 | 150 | 140 | 140 | 6.2 | 20 | 20 | S | 0.16 | 10 | 10 | Bar | 0.31 |
| TI-6AL-4V BAR UNK ANY S T5 4 1 0d C4 | 70 | 16.9 | 17.2 | 150 | 150 | 140 | 140 | 6.2 | 20 | 20 | S | 0.16 | 10 | 10 | Bar | 0.31 |
| TI-6AL-4V BAR UNK ANY S T5 4 1 0d C5 | 70 | 16.9 | 17.2 | 145 | 145 | 135 | 135 | 6.2 | 20 | 20 | S | 0.16 | 10 | 10 | Bar | 0.31 |
| TI-6AL-4V BAR UNK ANY S T5 4 1 0d C6 | 70 | 16.9 | 17.2 | 145 | 145 | 135 | 135 | 6.2 | 20 | 20 | S | 0.16 | 10 | 10 | Bar | 0.31 |
| TI-6AL-4V BAR UNK ANY S T5 4 1 0d C7 | 70 | 16.9 | 17.2 | 140 | 140 | 130 | 130 | 6.2 | 20 | 20 | S | 0.16 | 10 | 10 | Bar | 0.31 |
| TI-6AL-4V BAR UNK ANY S T5 4 1 0d C8 | 70 | 16.9 | 17.2 | 135 | 135 | 125 | 125 | 6.2 | 20 | 20 | S | 0.16 | 10 | 10 | Bar | 0.31 |
| TI-6AL-4V BAR UNK ANY S T5 4 1 0d C9 | 70 | 16.9 | 17.2 | 130 | 130 | 120 | 120 | 6.2 | 15 | 15 | S | 0.16 | 8 | 8 | Bar | 0.31 |
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