Aerospace Materials: TI-13V-11CR-3AL SHEET STA
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) | Fbru ksi 2 (ksi) | Fbry ksi (ksi) | Fbry ksi 2 (ksi) | Fcy ksi (ksi) | Fcy ksi LT (ksi) | Fcy ksi ST (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Ftu ksi LT (ksi) | Ftu ksi ST (ksi) | Fty ksi (ksi) | Fty ksi LT (ksi) | Fty ksi ST (ksi) | basis | condition | elongation pct (%) | elongation pct LT (%) | elongation pct ST (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| TI-13V-11CR-3AL SHEET STA LT4.000 S | 70 | 15.5 | 248 | 313 | 217 | 247 | 162 | 162 | 162 | 105 | 170 | 170 | 170 | 160 | 160 | 160 | S | Solution treated and aged | 4 | 4 | 4 | Sheet, strip, and plate | AMS-T-9046, Comp. B-1 | <4.000 |
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