Aerospace Materials: TI-6AL-6V-2SN BAR ANN
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 (%) | RA pct ST (%) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct LT (%) | elongation pct ST (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| TI-6AL-6V-2SN BAR ANN 1.501-....1.5003.000 A | 70 | 16 | 16.4 | 139 | 143 | 126 | 131 | 6.2 | 20 | 15 | 15 | A | Air-cool annealeda | 0.164 | 10 | 8 | 8 | Bar | 0.31 | AMS 4978 | 1.501-. . . . 1.500 3.000 |
| TI-6AL-6V-2SN BAR ANN 1.501-....1.5003.000 B T5 4 2 0c C2 | 70 | 16 | 16.4 | 150 | 152 | 138 | 141 | 6.2 | — | — | — | B | Air-cool annealeda | 0.164 | — | — | — | Bar | 0.31 | AMS 4978 | 1.501-. . . . 1.500 3.000 |
| TI-6AL-6V-2SN BAR ANN 1.501-....1.5003.000 B T5 4 2 0c C4 | 70 | 16 | 16.4 | 145 | 148 | 132 | 136 | 6.2 | — | — | — | B | Air-cool annealeda | 0.164 | — | — | — | Bar | 0.31 | AMS 4978 | 1.501-. . . . 1.500 3.000 |
| TI-6AL-6V-2SN BAR ANN 3.001-1.0004.000 A | 70 | 16 | 16.4 | 136 | 140 | 123 | 127 | 6.2 | 15 | 15 | 15 | A | Air-cool annealeda | 0.164 | 10 | 8 | 8 | Bar | 0.31 | AMS 4978 | 3.001-1.000 4.000 |
| TI-6AL-6V-2SN BAR ANN 3.001-1.0004.000 B | 70 | 16 | 16.4 | 142 | 145 | 129 | 132 | 6.2 | — | — | — | B | Air-cool annealeda | 0.164 | — | — | — | Bar | 0.31 | AMS 4978 | 3.001-1.000 4.000 |
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