5456-O Sheet 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 | Aluminum |
| Alloy / temper / form | 5456 / O / Sheet and plate |
| Specifications | AMS-QQ-A-250/9 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.5.5.0, Table 3.5.5.0(b) (pdf page 253 of the chapter file) |
| Dimension bands | 5 |
| Density | 2657 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 | 0.051–1.500 in (1.295–38.1 mm) | 1.501–3.000 in (38.13–76.2 mm) | 3.001–5.000 in (76.23–127 mm) | 5.001–7.000 in (127–177.8 mm) | 7.001–8.000 in (177.8–203.2 mm) | |
|---|---|---|---|---|---|---|
| Specification | AMS-QQ-A-250/9 | AMS-QQ-A-250/9 | AMS-QQ-A-250/9 | AMS-QQ-A-250/9 | AMS-QQ-A-250/9 | |
| Basis | S | S | S | S | S | |
| Ftu, MPa | L | 289.6 | 282.7 | 275.8 | 268.9 | 262 |
| LT | 289.6 | … | … | … | … | |
| Fty, MPa | L | 131 | 124.1 | 117.2 | 110.3 | 103.4 |
| LT | 131 | … | … | … | … | |
| Fcy, MPa | L | 131 | … | … | … | … |
| LT | 131 | 131 | 131 | 131 | 131 | |
| Fsu, MPa | L | 179.3 | … | … | … | … |
| LT | 179.3 | … | … | … | … | |
| Fbru (e/D = 1.5), MPa | L | 434.4 | … | … | … | … |
| LT | 434.4 | … | … | … | … | |
| Fbru (e/D = 2.0), MPa | L | 579.2 | … | … | … | … |
| LT | 579.2 | … | … | … | … | |
| Fbry (e/D = 1.5), MPa | L | 220.6 | … | … | … | … |
| LT | 220.6 | … | … | … | … | |
| Fbry (e/D = 2.0), MPa | L | 262 | … | … | … | … |
| LT | 262 | … | … | … | … | |
| e, % | L | 16 | 16 | 14 | 14 | 12 |
| LT | … | … | … | … | … | |
| E, GPa | 70.33 | 70.33 | 70.33 | 70.33 | 70.33 | |
| Ec, GPa | 71.71 | 71.71 | 71.71 | 71.71 | 71.71 | |
| G, GPa | 26.54 | 26.54 | 26.54 | 26.54 | 26.54 | |
| ν | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | |
| ρ, kg/m³ | 2657 | 2657 | 2657 | 2657 | 2657 | |
Effect of Temperature
The handbook maps no temperature-effect figure to this table.
Other 5456 Tables
- 5456-H111 Extruded bar, rod, and shapes (Table 3.5.5.0(c))
- 5456-H112 Extruded bar, rod, and shapes (Table 3.5.5.0(c))
- 5456-H112 Sheet and plate (Table 3.5.5.0(b))
- 5456-H321 Sheet and plate (Table 3.5.5.0(b))
- 5456-O Extruded bar, rod, and shapes (Table 3.5.5.0(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.