7075-T73a, T73510, T73511 Extrusion (rod, bars, and shapes): MIL-HDBK-5J Design Allowables
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| Material class | Aluminum |
| Alloy / temper / form | 7075 / T73a, T73510, T73511 / Extrusion (rod, bars, and shapes) |
| Specifications | AMS-QQ-A-200/11 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.7.6.0, Table 3.7.6.0(g) (pdf page 386 of the chapter file) |
| Dimension bands | 7 |
| 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 | 0.062–0.249 in, area 0–20 in2 | 0.250–0.499 in, area 0–25 in2 | 0.500–0.749 in, area 0–25 in2 | 0.750–1.499 in, area 0–25 in2 | 1.500–2.999 in, area 0–25 in2 | 3.000–4.499 in, area 0–20 in2 | 3.000–4.499 in, area 0–32 in2 | ||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Specification | AMS-QQ-A-200/11 | AMS-QQ-A-200/11 | AMS-QQ-A-200/11 | AMS-QQ-A-200/11 | AMS-QQ-A-200/11 | AMS-QQ-A-200/11 | AMS-QQ-A-200/11 | ||||||||
| Basis | A | B | A | B | A | B | A | B | A | B | A | B | A | B | |
| Ftu, ksi | L | 68 | 72 | 70 | 74 | 70 | 73 | 70 | 73 | 69 | 74 | 68 | 71 | 65 | 70 |
| LT | 66 | 70 | 68 | 72 | 67 | 70 | 66 | 69 | 62 | 67 | 58 | 61 | 56 | 60 | |
| Fty, ksi | L | 58 | 61 | 60 | 63 | 60 | 63 | 60 | 63 | 59 | 65 | 57 | 62 | 55 | 60 |
| LT | 56 | 59 | 57 | 60 | 57 | 60 | 56 | 58 | 51 | 56 | 46 | 50 | 44 | 48 | |
| Fcy, ksi | L | 58 | 61 | 60 | 63 | 60 | 63 | 60 | 63 | 59 | 65 | 57 | 62 | 55 | 60 |
| LT | 59 | 62 | 60 | 63 | 60 | 63 | 58 | 61 | 54 | 59 | 49 | 53 | 47 | 51 | |
| Fbru (e/D = 1.5), ksi | L | 101 | 107 | 104 | 110 | 103 | 108 | 103 | 107 | 99 | 106 | 95 | 99 | 91 | 98 |
| LT | 101 | 107 | 104 | 110 | 103 | 108 | 103 | 107 | 99 | 106 | 95 | 99 | 91 | 98 | |
| Fbru (e/D = 2.0), ksi | L | 129 | 137 | 133 | 141 | 133 | 139 | 132 | 138 | 128 | 138 | 124 | 130 | 119 | 128 |
| LT | 129 | 137 | 133 | 141 | 133 | 139 | 132 | 138 | 128 | 138 | 124 | 130 | 119 | 128 | |
| Fbry (e/D = 1.5), ksi | L | 82 | 86 | 84 | 89 | 84 | 88 | 83 | 87 | 79 | 87 | 72 | 79 | 70 | 76 |
| LT | 82 | 86 | 84 | 89 | 84 | 88 | 83 | 87 | 79 | 87 | 72 | 79 | 70 | 76 | |
| Fbry (e/D = 2.0), ksi | L | 97 | 102 | 100 | 105 | 100 | 105 | 98 | 103 | 93 | 103 | 86 | 94 | 83 | 91 |
| LT | 97 | 102 | 100 | 105 | 100 | 105 | 98 | 103 | 93 | 103 | 86 | 94 | 83 | 91 | |
| e, % | L | 7 | … | 8 | 8 | 8 | 8 | 8 | … | 8 | 8 | 7 | 7 | 7 | … |
| LT | … | … | … | … | … | … | … | … | … | … | … | … | … | … | |
| E, Msi | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | |
| Ec, Msi | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | |
| G, Msi | 4 | 4 | 4 | 4 | 4 | 4 | 4 | 4 | 4 | 4 | 4 | 4 | 4 | 4 | |
| 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 | 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 | 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-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,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.