Aerospace Materials: TI-5AL-2.5SN 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) | Ftu ksi ST (ksi) | Fty ksi (ksi) | Fty ksi LT (ksi) | Fty ksi ST (ksi) | 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 | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| TI-5AL-2.5SN BAR ANN 3.000-4.000 S | 70 | 15.5 | 15.5 | 115 | 115 | 115 | 110 | 110 | 110 | 25 | 25 | 20 | S | Annealed | 0.162 | 10 | 10 | 8 | Bar | AMS 4926a and MIL-T-9047b | 3.000-4.000c |
| TI-5AL-2.5SN BAR ANN LE2.999 A | 70 | 15.5 | 15.5 | 115 | 115 | — | 110 | 110 | — | 25 | 25 | — | A | Annealed | 0.162 | 10 | 10 | — | Bar | AMS 4926a and MIL-T-9047b | <=2.999c |
| TI-5AL-2.5SN BAR ANN LE2.999 B | 70 | 15.5 | 15.5 | 126 | — | — | 120 | — | — | — | — | — | B | Annealed | 0.162 | — | — | — | Bar | AMS 4926a and MIL-T-9047b | <=2.999c |
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