7075-T6 and T62 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 | Aluminum |
| Alloy / temper / form | 7075 / T6 and T62 / Sheet |
| Specifications | AMS 4045 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 371 of the chapter file) |
| Dimension bands | 4 |
| 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 | 0.008–0.011 in (0.2032–0.2794 mm) | 0.012–0.039 in (0.3048–0.9906 mm) | 0.040–0.125 in (1.016–3.175 mm) | 0.126–0.249 in (3.2–6.325 mm) | ||||
|---|---|---|---|---|---|---|---|---|
| Specification | AMS 4045 and AMS-QQ-A-250/12 | AMS 4045 and AMS-QQ-A-250/12 | AMS 4045 and AMS-QQ-A-250/12 | AMS 4045 and AMS-QQ-A-250/12 | ||||
| Basis | S | A | B | A | B | A | B | |
| Ftu, MPa | L | … | 524 | 537.8 | 537.8 | 551.6 | 537.8 | 551.6 |
| LT | 510.2 | 524 | 537.8 | 537.8 | 551.6 | 537.8 | 551.6 | |
| Fty, MPa | L | … | 475.7 | 496.4 | 482.6 | 496.4 | 489.5 | 503.3 |
| LT | 434.4 | 461.9 | 482.6 | 468.8 | 482.6 | 475.7 | 489.5 | |
| Fcy, MPa | L | … | 468.8 | 489.5 | 475.7 | 489.5 | 482.6 | 496.4 |
| LT | … | 489.5 | 510.2 | 496.4 | 510.2 | 503.3 | 517.1 | |
| Fsu, MPa | L | … | 317.2 | 324.1 | 324.1 | 330.9 | 324.1 | 330.9 |
| LT | … | 317.2 | 324.1 | 324.1 | 330.9 | 324.1 | 330.9 | |
| Fbru (e/D = 1.5), MPa | L | … | 813.6 | 834.3 | 834.3 | 854.9 | 834.3 | 854.9 |
| LT | … | 813.6 | 834.3 | 834.3 | 854.9 | 834.3 | 854.9 | |
| Fbru (e/D = 2.0), MPa | L | … | 1048 | 1076 | 1076 | 1103 | 1076 | 1103 |
| LT | … | 1048 | 1076 | 1076 | 1103 | 1076 | 1103 | |
| Fbry (e/D = 1.5), MPa | L | … | 689.5 | 723.9 | 703.3 | 723.9 | 710.2 | 730.8 |
| LT | … | 689.5 | 723.9 | 703.3 | 723.9 | 710.2 | 730.8 | |
| Fbry (e/D = 2.0), MPa | L | … | 806.7 | 841.2 | 820.5 | 841.2 | 834.3 | 854.9 |
| LT | … | 806.7 | 841.2 | 820.5 | 841.2 | 834.3 | 854.9 | |
| e, % | L | … | … | … | … | … | … | … |
| LT | 5 | 7 | 7 | 8 | 8 | 8 | 8 | |
| E, GPa | … | 71.02 | 71.02 | 71.02 | 71.02 | 71.02 | 71.02 | |
| Ec, GPa | … | 72.39 | 72.39 | 72.39 | 72.39 | 72.39 | 72.39 | |
| G, GPa | … | 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 | |
| nt (Ramberg-Osgood) | … | 12 | 12 | 12 | 12 | 12 | 12 | |
| nc (Ramberg-Osgood) | … | 15 | 15 | 15 | 15 | 15 | 15 | |
| ρ, kg/m³ | … | 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.
Strength allowables at temperature, percent of room temperature
Moduli at temperature
Elongation and exposure effects
| °C | F_tu | F_ty | F_cy | F_su | F_bru | F_bry |
|---|---|---|---|---|---|---|
| -184 | 117.8 | 117.6 | ||||
| -129 | 110 | 110 | ||||
| -73 | 105.5 | 105.6 | ||||
| -18 | 102.9 | 102.8 | ||||
| 38 | 98.6 | 98.9 | 99.8 | 99.8 | 97.2 | 99.5 |
| 93 | 89.2 | 91.2 | 94.7 | 97 | 87.5 | 96.1 |
| 149 | 74.2 | 79 | 80.5 | 84.6 | 77.8 | 84.3 |
| 204 | 45.7 | 50 | 50.5 | 58.2 | 53.1 | 58.5 |
| 26 | 19.9 | 19.8 | 20.2 | 27.7 | 24.3 | 23.1 |
| 316 | 11.8 | 11.8 | 15.6 | 14.5 |
Factors in percent of the room-temperature allowable.
Stress-Strain Curves (Ramberg-Osgood)
ε = σ/E + 0.002 (σ/F_y)^n with the first band's A-basis yield strength and the exponent on file for it (the tension curve stops at F_tu).
Ramberg-Osgood design stress-strain curves at room 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, 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-T7351 Plate (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.