Ti-6Al-2Sn-4Zr-2Mo-Triplex annealed Sheet: 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-2Sn-4Zr-2Mo / Triplex annealed / Sheet |
| Specifications | AMS-T-9046, Comp. AB-4 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 5.3.3.0, Table 5.3.3.0(b) (pdf page 45 of the chapter file) |
| Dimension bands | 1 |
| 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 | 0.000–0.187 in (0–4.75 mm) | |
|---|---|---|
| Specification | AMS-T-9046, Comp. AB-4 | |
| Basis | S | |
| Ftu, MPa | L | 999.7 |
| LT | 999.7 | |
| Fty, MPa | L | 930.8 |
| LT | 930.8 | |
| E, GPa | 113.8 | |
| Ec, GPa | 124.1 | |
| G, GPa | 42.75 | |
| ρ, kg/m³ | 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
Moduli at temperature
| °C | F_tu | F_ty |
|---|---|---|
| 38 | 97.6 | 97.6 |
| 93 | 92.2 | 89.5 |
| 149 | 86.8 | 82.3 |
| 204 | 82.3 | 75.5 |
| 26 | 78.3 | 69.8 |
| 316 | 75.3 | 65.3 |
| 371 | 73.8 | 62.6 |
| 427 | 60.8 |
Factors in percent of the room-temperature allowable.
Other Ti-6Al-2Sn-4Zr-2Mo Tables
- Ti-6Al-2Sn-4Zr-2Mo-Duplex annealed Sheet (Table 5.3.3.0(b))
- Ti-6Al-2Sn-4Zr-2Mo-STA (Duplex annealed) Bar (Table 5.3.3.0(c))
- Ti-6Al-2Sn-4Zr-2Mo-STA (Duplex annealed) Forging (Table 5.3.3.0(c))
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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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.