7075-T73a,b Die forging: MIL-HDBK-5J Design Allowables
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| Material class | Aluminum |
| Alloy / temper / form | 7075 / T73a,b / Die forging |
| Specifications | AMS 4141; AMS 4141, AMS-A-22771, and AMS-QQ-A-367 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.7.6.0, Table 3.7.6.0(e) (pdf page 382 of the chapter file) |
| Dimension bands | 6 |
| 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 | 0–1 in | 1.001–2.000 in | 2.001–3.000 in | 3.001–4.000 in | 4.001–5.000 in | 5.001–6.000 in | |||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Specification | AMS 4141, AMS-A-22771, and AMS-QQ-A-367 | AMS 4141, AMS-A-22771, and AMS-QQ-A-367 | AMS 4141, AMS-A-22771, and AMS-QQ-A-367 | AMS 4141, AMS-A-22771, and AMS-QQ-A-367 | AMS 4141 | AMS 4141 | |||||
| Basis | A | B | A | B | A | B | A | B | S | S | |
| Ftu, ksi | L | 66 | 71 | 66 | 71 | 66 | 69 | 64 | 69 | 62 | 61 |
| LT | 62 | … | 62 | … | 62 | … | 61 | … | 59 | 58 | |
| Fty, ksi | L | 56 | 61 | 56 | 59 | 56 | 59 | 55 | 59 | 53 | 51 |
| LT | 53 | … | 53 | … | 53 | … | 52 | … | 51 | 50 | |
| Fcy, ksi | L | 58 | 63 | 58 | 61 | 58 | 61 | 57 | 61 | … | … |
| LT | 55 | 60 | 55 | 59 | 55 | 59 | 54 | 58 | … | … | |
| Fsu, ksi | L | 39 | 42 | 39 | 42 | 39 | 41 | 38 | 41 | … | … |
| LT | 39 | 42 | 39 | 42 | 39 | 41 | 38 | 41 | … | … | |
| Fbru (e/D = 1.5), ksi | L | 96 | 103 | 96 | 103 | 96 | 100 | 93 | 100 | … | … |
| LT | 96 | 103 | 96 | 103 | 96 | 100 | 93 | 100 | … | … | |
| Fbru (e/D = 2.0), ksi | L | 125 | 135 | 125 | 135 | 125 | 131 | 122 | 131 | … | … |
| LT | 125 | 135 | 125 | 135 | 125 | 131 | 122 | 131 | … | … | |
| Fbry (e/D = 1.5), ksi | L | 78 | 85 | 78 | 83 | 78 | 83 | 77 | 83 | … | … |
| LT | 78 | 85 | 78 | 83 | 78 | 83 | 77 | 83 | … | … | |
| Fbry (e/D = 2.0), ksi | L | 90 | 98 | 90 | 94 | 90 | 94 | 88 | 94 | … | … |
| LT | 90 | 98 | 90 | 94 | 90 | 94 | 88 | 94 | … | … | |
| e, % | L | 7 | 7 | 7 | 7 | 7 | 7 | 7 | 7 | 7 | 6 |
| LT | 3 | 3 | 3 | 3 | 3 | 3 | 2 | 2 | 2 | 2 | |
| E, Msi | 10 | 10 | 10 | 10 | 10 | 10 | 10 | 10 | 10 | 10 | |
| Ec, Msi | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | |
| G, Msi | 3.8 | 3.8 | 3.8 | 3.8 | 3.8 | 3.8 | 3.8 | 3.8 | 3.8 | 3.8 | |
| ν | 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 | |
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, T73510, T73511 Extrusion (rod, bars, and shapes) (Table 3.7.6.0(g))
- 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.