Ti-8Al-1Mo-1V-Solution treated and stabilized Forging: 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-8Al-1Mo-1V / Solution treated and stabilized / Forging |
| Specifications | AMS 4973 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 5.3.2.0, Table 5.3.2.0(c) (pdf page 31 of the chapter file) |
| Dimension bands | 2 |
| Density | 4373 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 | 0.000–2.499 in (0–63.47 mm) | 2.500–4.000 in (63.5–101.6 mm) | |
|---|---|---|---|
| Specification | AMS 4973 | AMS 4973 | |
| Basis | S | S | |
| Ftu, MPa | L | 896.3 | 827.4 |
| LT | 896.3 | 827.4 | |
| ST | … | 827.4 | |
| Fty, MPa | L | 827.4 | 758.4 |
| LT | 827.4 | 758.4 | |
| ST | … | 758.4 | |
| e, % | L | 10 | 10 |
| LT | 10 | 10 | |
| ST | … | 10 | |
| E, GPa | 120.7 | 120.7 | |
| Ec, GPa | 124.1 | 124.1 | |
| G, GPa | 46.19 | 46.19 | |
| ν | 0.32 | 0.32 | |
| ρ, kg/m³ | 4373 | 4373 | |
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.
Moduli at temperature
Other Ti-8Al-1Mo-1V Tables
- Ti-8Al-1Mo-1V-Duplex annealed Bar (Table 5.3.2.0(c))
- Ti-8Al-1Mo-1V-Duplex Annealed Plate (Table 5.3.2.0(b))
- Ti-8Al-1Mo-1V-Duplex Annealed Sheet (Table 5.3.2.0(b))
- Ti-8Al-1Mo-1V-Single Annealed Plate (Table 5.3.2.0(b))
- Ti-8Al-1Mo-1V-Single Annealed Sheet (Table 5.3.2.0(b))
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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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.