7475-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 | 7475 / T7351 / Plate |
| Specifications | AMS 4202 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.7.10.0, Table 3.7.10.0(c) (pdf page 461 of the chapter file) |
| Dimension bands | 6 |
| 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 | 0.250–1.500 in (6.35–38.1 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 4202 | AMS 4202 | AMS 4202 | AMS 4202 | AMS 4202 | AMS 4202 | |||||||
| Basis | A | B | A | B | A | B | A | B | A | B | A | B | |
| Ftu, MPa | L | 482.6 | 496.4 | 482.6 | 489.5 | 468.8 | 482.6 | 468.8 | 475.7 | 441.3 | 461.9 | 441.3 | 455.1 |
| LT | 489.5 | 503.3 | 482.6 | 496.4 | 468.8 | 482.6 | 468.8 | 475.7 | 441.3 | 468.8 | 441.3 | 461.9 | |
| ST | 455.1 | 482.6 | 448.2 | 475.7 | 448.2 | 475.7 | 448.2 | 468.8 | 434.4 | 461.9 | 434.4 | 455.1 | |
| Fty, MPa | L | 406.8 | 427.5 | 399.9 | 413.7 | 386.1 | 406.8 | 386.1 | 399.9 | 358.5 | 386.1 | 358.5 | 372.3 |
| LT | 413.7 | 427.5 | 399.9 | 420.6 | 386.1 | 406.8 | 386.1 | 399.9 | 358.5 | 386.1 | 358.5 | 372.3 | |
| ST | 372.3 | 393 | 365.4 | 386.1 | 365.4 | 386.1 | 365.4 | 379.2 | 344.7 | 365.4 | 344.7 | 358.5 | |
| Fcy, MPa | L | 399.9 | 413.7 | 386.1 | 406.8 | 372.3 | 393 | 365.4 | 379.2 | 337.8 | 365.4 | 337.8 | 351.6 |
| LT | 420.6 | 434.4 | 413.7 | 434.4 | 399.9 | 420.6 | 399.9 | 413.7 | 372.3 | 399.9 | 372.3 | 386.1 | |
| ST | 427.5 | 441.3 | 413.7 | 434.4 | 399.9 | 420.6 | 399.9 | 413.7 | 372.3 | 399.9 | 372.3 | 386.1 | |
| Fsu, MPa | L | 282.7 | 289.6 | 289.6 | 296.5 | 282.7 | 289.6 | 282.7 | 289.6 | 268.9 | 289.6 | 268.9 | 282.7 |
| LT | 282.7 | 289.6 | 289.6 | 296.5 | 282.7 | 289.6 | 282.7 | 289.6 | 268.9 | 289.6 | 268.9 | 282.7 | |
| ST | 282.7 | 289.6 | 289.6 | 296.5 | 282.7 | 289.6 | 282.7 | 289.6 | 268.9 | 289.6 | 268.9 | 282.7 | |
| Fbru (e/D = 1.5), MPa | L | 703.3 | 723.9 | 710.2 | 730.8 | 696.4 | 717.1 | 696.4 | 710.2 | 668.8 | 703.3 | 668.8 | 696.4 |
| LT | 703.3 | 723.9 | 710.2 | 730.8 | 696.4 | 717.1 | 696.4 | 710.2 | 668.8 | 703.3 | 668.8 | 696.4 | |
| ST | 703.3 | 723.9 | 710.2 | 730.8 | 696.4 | 717.1 | 696.4 | 710.2 | 668.8 | 703.3 | 668.8 | 696.4 | |
| Fbru (e/D = 2.0), MPa | L | 910.1 | 937.7 | 923.9 | 951.5 | 903.2 | 930.8 | 903.2 | 923.9 | 861.8 | 917 | 861.8 | 903.2 |
| LT | 910.1 | 937.7 | 923.9 | 951.5 | 903.2 | 930.8 | 903.2 | 923.9 | 861.8 | 917 | 861.8 | 903.2 | |
| ST | 910.1 | 937.7 | 923.9 | 951.5 | 903.2 | 930.8 | 903.2 | 923.9 | 861.8 | 917 | 861.8 | 903.2 | |
| Fbry (e/D = 1.5), MPa | L | 558.5 | 579.2 | 565.4 | 592.9 | 558.5 | 579.2 | 558.5 | 579.2 | 530.9 | 565.4 | 530.9 | 551.6 |
| LT | 558.5 | 579.2 | 565.4 | 592.9 | 558.5 | 579.2 | 558.5 | 579.2 | 530.9 | 565.4 | 530.9 | 551.6 | |
| ST | 558.5 | 579.2 | 565.4 | 592.9 | 558.5 | 579.2 | 558.5 | 579.2 | 530.9 | 565.4 | 530.9 | 551.6 | |
| Fbry (e/D = 2.0), MPa | L | 668.8 | 696.4 | 668.8 | 703.3 | 655 | 689.5 | 655 | 682.6 | 613.6 | 661.9 | 613.6 | 641.2 |
| LT | 668.8 | 696.4 | 668.8 | 703.3 | 655 | 689.5 | 655 | 682.6 | 613.6 | 661.9 | 613.6 | 641.2 | |
| ST | 668.8 | 696.4 | 668.8 | 703.3 | 655 | 689.5 | 655 | 682.6 | 613.6 | 661.9 | 613.6 | 641.2 | |
| e, % | L | 10 | 10 | 10 | 10 | 10 | 10 | 10 | 10 | 10 | 10 | 9 | 9 |
| LT | 9 | 9 | 8 | 8 | 8 | 8 | 8 | 8 | 8 | 8 | 7 | 7 | |
| ST | 4 | 4 | 4 | 4 | 4 | 4 | 3 | 3 | 3 | 3 | 3 | 3 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| ρ, kg/m³ | 2796 | 2796 | 2796 | 2796 | 2796 | 2796 | 2796 | 2796 | 2796 | 2796 | 2796 | 2796 | |
Effect of Temperature
The handbook maps no temperature-effect figure to this table.
Other 7475 Tables
- 7475-T61 Clad sheet (Table 3.7.10.0(d))
- 7475-T61 Sheet (Table 3.7.10.0(b))
- 7475-T651 Plate (Table 3.7.10.0(b))
- 7475-T761 Clad sheet (Table 3.7.10.0(d))
- 7475-T761 Sheet (Table 3.7.10.0(b))
- 7475-T7651 Plate (Table 3.7.10.0(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.