7075-T7351 Plate: MIL-HDBK-5J Design Allowables
show SI units (MPa, GPa, kg/m³) 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 | 0.101 lb/in3 |
Design Mechanical and Physical Properties (room temperature)
As printed in the handbook table. 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 | 0.500–1.000 in | 1.001–1.500 in | 1.501–2.000 in | 2.001–2.500 in | 2.501–3.000 in | 3.001–3.500 in | 3.501–4.000 in | ||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 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, ksi | L | 68 | 68 | 70 | 67 | 69 | 66 | 68 | 65 | 67 | 63 | 65 | 62 | 60 |
| LT | 69 | 69 | 71 | 68 | 70 | 67 | 69 | 66 | 68 | 64 | 66 | 63 | 61 | |
| ST | … | … | … | … | … | 63 | 65 | 62 | 64 | 60 | 62 | 59 | 57 | |
| Fty, ksi | L | 57 | 57 | 59 | 57 | 59 | 55 | 57 | 52 | 55 | 49 | 53 | 49 | 48 |
| LT | 57 | 57 | 59 | 57 | 59 | 55 | 57 | 52 | 55 | 49 | 53 | 49 | 48 | |
| ST | … | … | … | … | … | 52 | 54 | 49 | 52 | 47 | 50 | 47 | 46 | |
| Fcy, ksi | L | 56 | 56 | 58 | 56 | 58 | 53 | 55 | 50 | 53 | 47 | 51 | 47 | 45 |
| LT | 59 | 59 | 61 | 59 | 61 | 57 | 59 | 54 | 57 | 51 | 55 | 51 | 50 | |
| ST | 59 | 59 | 59 | 59 | 59 | 59 | 61 | 58 | 58 | 58 | 55 | 50 | 48 | |
| Fsu, ksi | L | 38 | 38 | 39 | 38 | 40 | 39 | 40 | 39 | 40 | 38 | 39 | 38 | 37 |
| LT | 38 | 38 | 39 | 38 | 40 | 39 | 40 | 39 | 40 | 38 | 39 | 38 | 37 | |
| ST | 38 | 38 | 39 | 38 | 40 | 39 | 40 | 39 | 40 | 38 | 39 | 38 | 37 | |
| Fbru (e/D = 1.5), ksi | L | 102 | 103 | 106 | 103 | 106 | 102 | 106 | 102 | 105 | 100 | 103 | 99 | 96 |
| LT | 102 | 103 | 106 | 103 | 106 | 102 | 106 | 102 | 105 | 100 | 103 | 99 | 96 | |
| ST | 102 | 103 | 106 | 103 | 106 | 102 | 106 | 102 | 105 | 100 | 103 | 99 | 96 | |
| Fbru (e/D = 2.0), ksi | L | 131 | 132 | 136 | 132 | 136 | 132 | 136 | 131 | 135 | 128 | 132 | 127 | 124 |
| LT | 131 | 132 | 136 | 132 | 136 | 132 | 136 | 131 | 135 | 128 | 132 | 127 | 124 | |
| ST | 131 | 132 | 136 | 132 | 136 | 132 | 136 | 131 | 135 | 128 | 132 | 127 | 124 | |
| Fbry (e/D = 1.5), ksi | L | 79 | 81 | 83 | 83 | 86 | 82 | 85 | 79 | 83 | 76 | 81 | 76 | 76 |
| LT | 79 | 81 | 83 | 83 | 86 | 82 | 85 | 79 | 83 | 76 | 81 | 76 | 76 | |
| ST | 79 | 81 | 83 | 83 | 86 | 82 | 85 | 79 | 83 | 76 | 81 | 76 | 76 | |
| Fbry (e/D = 2.0), ksi | L | 95 | 97 | 100 | 99 | 102 | 97 | 101 | 93 | 99 | 89 | 96 | 89 | 88 |
| LT | 95 | 97 | 100 | 99 | 102 | 97 | 101 | 93 | 99 | 89 | 96 | 89 | 88 | |
| ST | 95 | 97 | 100 | 99 | 102 | 97 | 101 | 93 | 99 | 89 | 96 | 89 | 88 | |
| e, % | L | … | … | … | … | … | … | … | … | … | … | … | … | … |
| LT | 7 | 7 | 7 | 6 | 6 | 6 | 6 | 6 | 6 | 6 | 6 | 6 | 6 | |
| ST | … | … | … | … | … | … | … | … | … | … | … | … | … | |
| E, Msi | 10.3 | 10.3 | 10.3 | 10.3 | 10.3 | 10.3 | 10.3 | 10.3 | 10.3 | 10.3 | 10.3 | 10.3 | 10.3 | |
| Ec, Msi | 10.6 | 10.6 | 10.6 | 10.6 | 10.6 | 10.6 | 10.6 | 10.6 | 10.6 | 10.6 | 10.6 | 10.6 | 10.6 | |
| G, Msi | 3.9 | 3.9 | 3.9 | 3.9 | 3.9 | 3.9 | 3.9 | 3.9 | 3.9 | 3.9 | 3.9 | 3.9 | 3.9 | |
| 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, lb/in3 | 0.101 | 0.101 | 0.101 | 0.101 | 0.101 | 0.101 | 0.101 | 0.101 | 0.101 | 0.101 | 0.101 | 0.101 | 0.101 | |
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.