Aerospace Materials: TI-6AL-6V-2SN 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 | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| TI-6AL-6V-2SN BAR UNK 1.501-....1.5003.000 A | 70 | 16 | 16.4 | 144 | 147 | 131 | 136 | 6.2 | 20 | 15 | A | 0.164 | 10 | 8 | Bar | 0.31 | 1.501-. . . . 1.500 3.000 |
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