2024-T3, T3510, and T3511 Extruded bar, rod, and shapes: 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 | 2024 / T3, T3510, and T3511 / Extruded bar, rod, and shapes |
| Specifications | AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.2.3.0, Table 3.2.3.0(j) (pdf page 85 of the chapter file) |
| Dimension bands | 8 |
| Density | 0.1 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 | 0.000–0.249 in, area 0–20 in2 | 0.250–0.499 in, area 0–20 in2 | 0.500–0.749 in, area 0–20 in2 | 0.750–1.499 in, area 0–20 in2 | 1.500–2.999 in, area 0–25 in2 | 1.500–2.999 in, area 25– in2 | 3.000–4.499 in, area 0–25 in2 | 3.000–4.499 in, area 0–32 in2 | |||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Specification | AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3 | AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3 | AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3 | AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3 | AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3 | AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3 | AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3 | AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3 | |||||||
| Basis | A | B | A | B | A | B | A | B | A | B | S | A | B | S | |
| Ftu, ksi | L | 57 | 61 | 60 | 62 | 60 | 62 | 65 | 70 | 70 | 74 | 68 | 70 | 74 | 68 |
| LT | 54 | 58 | 56 | 57 | 54 | 56 | 56 | 60 | 55 | 58 | 53 | 54 | 57 | 52 | |
| Fty, ksi | L | 42 | 47 | 44 | 47 | 44 | 47 | 46 | 54 | 52 | 54 | 48 | 52 | 54 | 48 |
| LT | 37 | 41 | 38 | 40 | 37 | 39 | 37 | 43 | 39 | 41 | 36 | 39 | 41 | 36 | |
| Fcy, ksi | L | 34 | 38 | 37 | 39 | 38 | 40 | 41 | 48 | 49 | 50 | 45 | 49 | 51 | 45 |
| LT | 41 | 45 | 41 | 44 | 40 | 43 | 40 | 47 | 42 | 44 | 39 | 41 | 43 | 38 | |
| Fsu, ksi | L | 29 | 31 | 31 | 32 | 30 | 31 | 33 | 35 | 34 | 36 | 33 | 33 | 35 | 32 |
| LT | 29 | 31 | 31 | 32 | 30 | 31 | 33 | 35 | 34 | 36 | 33 | 33 | 35 | 32 | |
| Fbru (e/D = 1.5), ksi | L | 84 | 90 | 78 | 81 | 78 | 80 | 84 | 90 | 88 | 93 | 86 | 86 | 91 | 84 |
| LT | 84 | 90 | 78 | 81 | 78 | 80 | 84 | 90 | 88 | 93 | 86 | 86 | 91 | 84 | |
| Fbru (e/D = 2.0), ksi | L | 108 | 114 | 98 | 101 | 97 | 101 | 105 | 113 | 111 | 118 | 108 | 109 | 115 | 106 |
| LT | 108 | 114 | 98 | 101 | 97 | 101 | 105 | 113 | 111 | 118 | 108 | 109 | 115 | 106 | |
| Fbry (e/D = 1.5), ksi | L | 61 | 68 | 55 | 59 | 55 | 59 | 57 | 67 | 63 | 66 | 59 | 62 | 65 | 57 |
| LT | 61 | 68 | 55 | 59 | 55 | 59 | 57 | 67 | 63 | 66 | 59 | 62 | 65 | 57 | |
| Fbry (e/D = 2.0), ksi | L | 71 | 79 | 67 | 71 | 67 | 71 | 69 | 81 | 77 | 80 | 71 | 75 | 78 | 69 |
| LT | 71 | 79 | 67 | 71 | 67 | 71 | 69 | 81 | 77 | 80 | 71 | 75 | 78 | 69 | |
| e, % | L | 12 | 12 | 12 | … | 12 | … | 10 | … | 10 | … | 8 | 10 | … | 8 |
| LT | … | … | … | … | … | … | … | … | … | … | … | … | … | … | |
| E, Msi | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | |
| Ec, Msi | 11 | 11 | 11 | 11 | 11 | 11 | 11 | 11 | 11 | 11 | 11 | 11 | 11 | 11 | |
| G, Msi | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | |
| 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 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | |
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
| °F | F_tu | F_ty |
|---|---|---|
| -300 | 111.6 | 118.5 |
| -200 | 105.3 | 108.3 |
| -100 | 103 | 103.6 |
| 0 | 101.6 | 102 |
| 100 | 98.9 | 98.9 |
| 200 | 92.4 | 93.9 |
| 300 | 83.9 | 87.4 |
| 400 | 74.5 | 77.7 |
| 500 | 43.8 | 51.6 |
| 600 | 22.5 | 26.9 |
| 700 | 12 | 14 |
| 800 | 8 |
Factors in percent of the room-temperature allowable.
Other 2024 Tables
- 2024-T3 Clad flat sheet and plate (Table 3.2.3.0(e))
- 2024-T3 Drawn tubing (Table 3.2.3.0(g))
- 2024-T3 Sheet (Table 3.2.3.0(b))
- 2024-T351 Bar and rod; rolled, drawn, or cold-finished (Table 3.2.3.0(i))
- 2024-T351 Clad flat sheet and plate (Table 3.2.3.0(e))
- 2024-T351 Plate (Table 3.2.3.0(b))
- 2024-T361 Bar and rod; rolled, drawn, or cold-finished (Table 3.2.3.0(i))
- 2024-T361 Clad flat sheet and plate (Table 3.2.3.0(e))
- 2024-T361 Plate (Table 3.2.3.0(b))
- 2024-T361 Sheet (Table 3.2.3.0(b))
- 2024-T4 Bar and rod; rolled, drawn, or cold-finished (Table 3.2.3.0(i))
- 2024-T4 Clad coiled sheet (Table 3.2.3.0(e))
- 2024-T4 Coiled Sheet (Table 3.2.3.0(b))
- 2024-T42 Bar and rod; rolled, drawn, or cold-finished (Table 3.2.3.0(i))
- 2024-T42 Clad flat sheet and plate (Table 3.2.3.0(e))
- 2024-T42 Drawn tubing (Table 3.2.3.0(g))
- 2024-T42 Extruded bar, rod, and shapes (Table 3.2.3.0(j))
- 2024-T42 Flat Sheet and Plate (Table 3.2.3.0(b))
- 2024-T6 Bar and rod; rolled, drawn, or cold finished (Table 3.2.3.0(i))
- 2024-T62 Bar and rod; rolled, drawn, or cold finished (Table 3.2.3.0(i))
- 2024-T62 Clad flat sheet and plate (Table 3.2.3.0(e))
- 2024-T62 Flat Sheet and Plate (Table 3.2.3.0(b))
- 2024-T72 Clad flat sheet and plate (Table 3.2.3.0(e))
- 2024-T72 Flat Sheet and Plate (Table 3.2.3.0(b))
- 2024-T81 Clad flat sheet and plate (Table 3.2.3.0(e))
- 2024-T81 Drawn tubing (Table 3.2.3.0(g))
- 2024-T81 Sheet (Table 3.2.3.0(b))
- 2024-T81, T8510, and T8511 Extruded bar, rod, and shapes (Table 3.2.3.0(j))
- 2024-T851 Bar and rod; rolled, drawn, or cold finished (Table 3.2.3.0(i))
- 2024-T851 Clad flat sheet and plate (Table 3.2.3.0(e))
- 2024-T851 Plate (Table 3.2.3.0(b))
- 2024-T861 Clad flat sheet and plate (Table 3.2.3.0(e))
- 2024-T861 Plate (Table 3.2.3.0(b))
- 2024-T861 Sheet (Table 3.2.3.0(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.