7075-T7351 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 | 7075 / T7351 / Plate |
| Specifications | AMS 4078 and AMS-QQ-A-250/12 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.7.6.0, Table 3.7.6.0(b) (pdf page 373 of the chapter file) |
| Dimension bands | 8 |
| Density | 2796 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 | 0.250–0.499 in (6.35–12.67 mm) | 0.500–1.000 in (12.7–25.4 mm) | 1.001–1.500 in (25.43–38.1 mm) | 1.501–2.000 in (38.13–50.8 mm) | 2.001–2.500 in (50.83–63.5 mm) | 2.501–3.000 in (63.53–76.2 mm) | 3.001–3.500 in (76.23–88.9 mm) | 3.501–4.000 in (88.93–101.6 mm) | ||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Specification | AMS 4078 and AMS-QQ-A-250/12 | AMS 4078 and AMS-QQ-A-250/12 | AMS 4078 and AMS-QQ-A-250/12 | AMS 4078 and AMS-QQ-A-250/12 | AMS 4078 and AMS-QQ-A-250/12 | AMS 4078 and AMS-QQ-A-250/12 | AMS 4078 and AMS-QQ-A-250/12 | AMS 4078 and AMS-QQ-A-250/12 | ||||||
| Basis | S | A | B | A | B | A | B | A | B | A | B | S | S | |
| Ftu, MPa | L | 468.8 | 468.8 | 482.6 | 461.9 | 475.7 | 455.1 | 468.8 | 448.2 | 461.9 | 434.4 | 448.2 | 427.5 | 413.7 |
| LT | 475.7 | 475.7 | 489.5 | 468.8 | 482.6 | 461.9 | 475.7 | 455.1 | 468.8 | 441.3 | 455.1 | 434.4 | 420.6 | |
| ST | … | … | … | … | … | 434.4 | 448.2 | 427.5 | 441.3 | 413.7 | 427.5 | 406.8 | 393 | |
| Fty, MPa | L | 393 | 393 | 406.8 | 393 | 406.8 | 379.2 | 393 | 358.5 | 379.2 | 337.8 | 365.4 | 337.8 | 330.9 |
| LT | 393 | 393 | 406.8 | 393 | 406.8 | 379.2 | 393 | 358.5 | 379.2 | 337.8 | 365.4 | 337.8 | 330.9 | |
| ST | … | … | … | … | … | 358.5 | 372.3 | 337.8 | 358.5 | 324.1 | 344.7 | 324.1 | 317.2 | |
| Fcy, MPa | L | 386.1 | 386.1 | 399.9 | 386.1 | 399.9 | 365.4 | 379.2 | 344.7 | 365.4 | 324.1 | 351.6 | 324.1 | 310.3 |
| LT | 406.8 | 406.8 | 420.6 | 406.8 | 420.6 | 393 | 406.8 | 372.3 | 393 | 351.6 | 379.2 | 351.6 | 344.7 | |
| ST | 406.8 | 406.8 | 406.8 | 406.8 | 406.8 | 406.8 | 420.6 | 399.9 | 399.9 | 399.9 | 379.2 | 344.7 | 330.9 | |
| Fsu, MPa | L | 262 | 262 | 268.9 | 262 | 275.8 | 268.9 | 275.8 | 268.9 | 275.8 | 262 | 268.9 | 262 | 255.1 |
| LT | 262 | 262 | 268.9 | 262 | 275.8 | 268.9 | 275.8 | 268.9 | 275.8 | 262 | 268.9 | 262 | 255.1 | |
| ST | 262 | 262 | 268.9 | 262 | 275.8 | 268.9 | 275.8 | 268.9 | 275.8 | 262 | 268.9 | 262 | 255.1 | |
| Fbru (e/D = 1.5), MPa | L | 703.3 | 710.2 | 730.8 | 710.2 | 730.8 | 703.3 | 730.8 | 703.3 | 723.9 | 689.5 | 710.2 | 682.6 | 661.9 |
| LT | 703.3 | 710.2 | 730.8 | 710.2 | 730.8 | 703.3 | 730.8 | 703.3 | 723.9 | 689.5 | 710.2 | 682.6 | 661.9 | |
| ST | 703.3 | 710.2 | 730.8 | 710.2 | 730.8 | 703.3 | 730.8 | 703.3 | 723.9 | 689.5 | 710.2 | 682.6 | 661.9 | |
| Fbru (e/D = 2.0), MPa | L | 903.2 | 910.1 | 937.7 | 910.1 | 937.7 | 910.1 | 937.7 | 903.2 | 930.8 | 882.5 | 910.1 | 875.6 | 854.9 |
| LT | 903.2 | 910.1 | 937.7 | 910.1 | 937.7 | 910.1 | 937.7 | 903.2 | 930.8 | 882.5 | 910.1 | 875.6 | 854.9 | |
| ST | 903.2 | 910.1 | 937.7 | 910.1 | 937.7 | 910.1 | 937.7 | 903.2 | 930.8 | 882.5 | 910.1 | 875.6 | 854.9 | |
| Fbry (e/D = 1.5), MPa | L | 544.7 | 558.5 | 572.3 | 572.3 | 592.9 | 565.4 | 586.1 | 544.7 | 572.3 | 524 | 558.5 | 524 | 524 |
| LT | 544.7 | 558.5 | 572.3 | 572.3 | 592.9 | 565.4 | 586.1 | 544.7 | 572.3 | 524 | 558.5 | 524 | 524 | |
| ST | 544.7 | 558.5 | 572.3 | 572.3 | 592.9 | 565.4 | 586.1 | 544.7 | 572.3 | 524 | 558.5 | 524 | 524 | |
| Fbry (e/D = 2.0), MPa | L | 655 | 668.8 | 689.5 | 682.6 | 703.3 | 668.8 | 696.4 | 641.2 | 682.6 | 613.6 | 661.9 | 613.6 | 606.7 |
| LT | 655 | 668.8 | 689.5 | 682.6 | 703.3 | 668.8 | 696.4 | 641.2 | 682.6 | 613.6 | 661.9 | 613.6 | 606.7 | |
| ST | 655 | 668.8 | 689.5 | 682.6 | 703.3 | 668.8 | 696.4 | 641.2 | 682.6 | 613.6 | 661.9 | 613.6 | 606.7 | |
| e, % | L | … | … | … | … | … | … | … | … | … | … | … | … | … |
| LT | 7 | 7 | 7 | 6 | 6 | 6 | 6 | 6 | 6 | 6 | 6 | 6 | 6 | |
| ST | … | … | … | … | … | … | … | … | … | … | … | … | … | |
| E, GPa | 71.02 | 71.02 | 71.02 | 71.02 | 71.02 | 71.02 | 71.02 | 71.02 | 71.02 | 71.02 | 71.02 | 71.02 | 71.02 | |
| Ec, GPa | 73.08 | 73.08 | 73.08 | 73.08 | 73.08 | 73.08 | 73.08 | 73.08 | 73.08 | 73.08 | 73.08 | 73.08 | 73.08 | |
| G, GPa | 26.89 | 26.89 | 26.89 | 26.89 | 26.89 | 26.89 | 26.89 | 26.89 | 26.89 | 26.89 | 26.89 | 26.89 | 26.89 | |
| ν | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | |
| ρ, kg/m³ | 2796 | 2796 | 2796 | 2796 | 2796 | 2796 | 2796 | 2796 | 2796 | 2796 | 2796 | 2796 | 2796 | |
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 7075 Tables
- 7075-T6 Clad sheet (Table 3.7.6.0(c))
- 7075-T6 Die forging (Table 3.7.6.0(e))
- 7075-T6 Hand forging (Table 3.7.6.0(f))
- 7075-T6 and T62 Clad sheet (Table 3.7.6.0(c))
- 7075-T6 and T62 Sheet (Table 3.7.6.0(b))
- 7075-T6, T651, and T62 Bar, rod, and shapes: rolled, drawn, or cold-finished (Table 3.7.6.0(d))
- 7075-T6, T6510, T6511, and T62 Extrusion (rod, bar, and shapes) (Table 3.7.6.0(g))
- 7075-T62 Clad plate (Table 3.7.6.0(c))
- 7075-T62 Plate (Table 3.7.6.0(b))
- 7075-T651 Clad plate (Table 3.7.6.0(c))
- 7075-T651 Plate (Table 3.7.6.0(b))
- 7075-T652 Die forging (Table 3.7.6.0(e))
- 7075-T652 Hand forging (Table 3.7.6.0(f))
- 7075-T73 Hand forging (Table 3.7.6.0(f))
- 7075-T73 Sheet (Table 3.7.6.0(b))
- 7075-T7352 Die forging (Table 3.7.6.0(e))
- 7075-T7352 Hand forging (Table 3.7.6.0(f))
- 7075-T73a, T73510, T73511 Extrusion (rod, bars, and shapes) (Table 3.7.6.0(g))
- 7075-T73a,b Die forging (Table 3.7.6.0(e))
- 7075-T73b or T7351 Bar, rod, and shapes: rolled, drawn, or cold-finished (Table 3.7.6.0(d))
- 7075-T76 Clad sheet (Table 3.7.6.0(c))
- 7075-T76 Sheet and plate (Table 3.7.6.0(b))
- 7075-T76, T76510, T76511 Extrusion (rod, bar, and shapes) (Table 3.7.6.0(g))
- 7075-T7651 Clad plate (Table 3.7.6.0(c))
- 7075-T7651 Sheet and plate (Table 3.7.6.0(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.