Ti-6Al-6V-2Sn-Solution treated and aged Sheet, strip, and plate: MIL-HDBK-5J Design Allowables
show US units (ksi, Msi, lb/in³) open the MIL-HDBK-5J tool compare against temperature find alternatives
| Material class | Titanium |
| Alloy / temper / form | Ti-6Al-6V-2Sn / Solution treated and aged / Sheet, strip, and plate |
| Specifications | AMS-T-9046, Comp. AB-3 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 5.4.2.0, Table 5.4.2.0(b) (pdf page 94 of the chapter file) |
| Dimension bands | 4 |
| Density | 454 kg/m³ |
Design Mechanical and Physical Properties (room temperature)
Converted from the handbook table (ksi, Msi, lb/in³) and rounded to 4 significant figures; dimension bands in inches with mm in parentheses. Bases: A and B are statistical minimums (99 % and 90 % probability at 95 % confidence), S the specification minimum. Grain directions: L longitudinal, LT long transverse, ST short transverse.
| Dimension band | 0.000–0.188 in (0–4.763 mm) | 0.188–1.500 in (4.763–38.1 mm) | 1.501–2.500 in (38.13–63.5 mm) | 2.501–4.000 in (63.53–101.6 mm) | |
|---|---|---|---|---|---|
| Specification | AMS-T-9046, Comp. AB-3 | AMS-T-9046, Comp. AB-3 | AMS-T-9046, Comp. AB-3 | AMS-T-9046, Comp. AB-3 | |
| Basis | S | S | S | S | |
| Ftu, MPa | L | 1172 | 1172 | 1103 | 1034 |
| LT | 1172 | 1172 | 1103 | 1034 | |
| Fty, MPa | L | 1103 | 1103 | 1034 | 965.3 |
| LT | 1103 | 1103 | 1034 | 965.3 | |
| Fcy, MPa | L | 1172 | 1172 | 1172 | 1172 |
| LT | … | 1172 | … | … | |
| Fsu, MPa | L | 655 | 655 | 655 | 655 |
| LT | 655 | 655 | 655 | 655 | |
| Fbru (e/D = 1.5), MPa | L | … | 1820 | … | … |
| LT | … | 1820 | … | … | |
| Fbru (e/D = 2.0), MPa | L | 2186 | 2186 | 2186 | 2186 |
| LT | 2186 | 2186 | 2186 | 2186 | |
| Fbry (e/D = 1.5), MPa | L | … | 1634 | … | … |
| LT | … | 1634 | … | … | |
| Fbry (e/D = 2.0), MPa | L | … | 1834 | … | … |
| LT | … | 1834 | … | … | |
| e, % | L | 8 | 8 | 6 | 8 |
| LT | 6 | 8 | 6 | 6 | |
| E, GPa | 110.3 | 110.3 | 110.3 | 110.3 | |
| Ec, GPa | 113.1 | 113.1 | 113.1 | 113.1 | |
| G, GPa | 42.75 | 42.75 | 42.75 | 42.75 | |
| ν | 0.31 | 0.31 | 0.31 | 0.31 | |
| ρ, kg/m³ | 4540 | 4540 | 4540 | 4540 | |
Effect of Temperature
Percent of the room-temperature value against temperature, digitized from the handbook figures (the shortest exposure of each figure, every 10 °F). Strength curves give the allowable at temperature; "after exposure" curves give the room-temperature property after a soak at that temperature.
Strength allowables at temperature, percent of room temperature
| °C | F_tu | F_ty | F_cy |
|---|---|---|---|
| 38 | 97.9 | 97.9 | 96.6 |
| 93 | 91.7 | 88.9 | 85.8 |
| 149 | 86.2 | 82.3 | 78.1 |
| 204 | 82.2 | 77.1 | 72 |
| 26 | 78.5 | 72.5 | 67.4 |
| 316 | 75.7 | 69.4 | 63.4 |
| 371 | 73.2 | 66.7 | 59.8 |
Factors in percent of the room-temperature allowable.
Other Ti-6Al-6V-2Sn Tables
- Ti-6Al-6V-2Sn-Air-cool annealed Bar (Table 5.4.2.0(c))
- Ti-6Al-6V-2Sn-Annealed Extruded bar and shapes (Table 5.4.2.0(e))
- Ti-6Al-6V-2Sn-Annealed Forging (Table 5.4.2.0(d))
- Ti-6Al-6V-2Sn-Annealed Sheet, strip, and plate (Table 5.4.2.0(b))
- Ti-6Al-6V-2Sn-Solution treated and aged Bar and forging (Table 5.4.2.0(c))
- Ti-6Al-6V-2Sn-Solution treated and aged Extruded bar and shapes (Table 5.4.2.0(e))
Source and Use
U.S. Department of Defense (2003). Metallic Materials and Elements for Aerospace Vehicle Structures. MIL-HDBK-5J, 31 January 2003 (public domain). The values are the handbook's design allowables as extracted from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ. No warranty is given.