Ti-10V-2Fe-3Al-Solution treated and aged (900-950 F) Conventional die forging: MIL-HDBK-5J Design Allowables
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| Material class | Titanium |
| Alloy / temper / form | Ti-10V-2Fe-3Al / Solution treated and aged (900-950 F) / Conventional die forging |
| Specifications | AMS 4983; AMS 4984 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 5.5.3.0, Table 5.5.3.0(b) (pdf page 141 of the chapter file) |
| Dimension bands | 2 |
| Density | 465 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 | 0–1 in (0–25.4 mm) | 0–3 in (0–76.2 mm) | |
|---|---|---|---|
| Specification | AMS 4983 | AMS 4984 | |
| Basis | S | S | |
| Ftu, MPa | L | 1241 | 1193 |
| LT | 1241 | 1193 | |
| ST | … | 1193 | |
| Fty, MPa | L | 1103 | 1103 |
| LT | 1103 | 1103 | |
| ST | … | 1103 | |
| Fcy, MPa | L | 1158 | 1158 |
| LT | 1145 | 1145 | |
| ST | … | 1145 | |
| Fsu, MPa | L | 696.4 | 668.8 |
| LT | 696.4 | 668.8 | |
| ST | … | 668.8 | |
| Fbru (e/D = 1.5), MPa | L | 1682 | 1613 |
| LT | 1682 | 1613 | |
| ST | … | 1613 | |
| Fbru (e/D = 2.0), MPa | L | 2034 | 1958 |
| LT | 2034 | 1958 | |
| ST | … | 1958 | |
| Fbry (e/D = 1.5), MPa | L | 1565 | 1565 |
| LT | 1565 | 1565 | |
| ST | … | 1565 | |
| Fbry (e/D = 2.0), MPa | L | 1800 | 1800 |
| LT | 1800 | 1800 | |
| ST | … | 1800 | |
| e, % | L | 4 | 4 |
| LT | 4 | 4 | |
| ST | … | 4 | |
| E, GPa | 109.6 | 109.6 | |
| Ec, GPa | 112.4 | 112.4 | |
| ρ, kg/m³ | 4650 | 4650 | |
Effect of Temperature
The handbook maps no temperature-effect figure to this table.
Other Ti-10V-2Fe-3Al Tables
- Ti-10V-2Fe-3Al-Solution treated and aged (950-1000 F) Hand forging (Table 5.5.3.0(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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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.