AISI 301and Relateda,b,c-Full Hard Sheet and strip: 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 | Steel |
| Alloy / temper / form | AISI 301and Relateda,b,c / Full Hard / Sheet and strip |
| Specifications | AMS 5519 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 2.7.1.0, Table 2.7.1.0(b) (pdf page 223 of the chapter file) |
| Dimension bands | 1 |
| Density | 7916 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 | all | ||
|---|---|---|---|
| Specification | AMS 5519 | ||
| Basis | A | B | |
| Ftu, MPa | L | 1200 | 1276 |
| LT | 1207 | 1282 | |
| Fty, MPa | L | 944.6 | 1055 |
| LT | 861.8 | 979.1 | |
| Fcy, MPa | L | 572.3 | 648.1 |
| LT | 979.1 | 1131 | |
| Fsu, MPa | L | 655 | 689.5 |
| LT | 655 | 689.5 | |
| Fbru (e/D = 2.0), MPa | L | 2386 | 2489 |
| LT | 2386 | 2489 | |
| Fbry (e/D = 2.0), MPa | L | 1531 | 1717 |
| LT | 1531 | 1717 | |
| e, % | L | … | … |
| LT | 25 | 25 | |
| E, GPa | 179.3 | 179.3 | |
| G, GPa | 72.39 | 72.39 | |
| ν | 0.27 | 0.27 | |
| ρ, kg/m³ | 7916 | 7916 | |
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
| °C | F_tu | F_ty | F_cy L | F_cy LT | F_su | F_bru | F_bry |
|---|---|---|---|---|---|---|---|
| 38 | 99.2 | 99.2 | 98.3 | 99.7 | 98.4 | 98.3 | 98.3 |
| 93 | 95.4 | 95.4 | 92.9 | 98.7 | 91.2 | 92 | 97 |
| 149 | 92.8 | 92.8 | 88.4 | 97.6 | 83.9 | 86.7 | 94.9 |
| 204 | 91.2 | 91.2 | 84.9 | 96.1 | 76.6 | 83 | 92.9 |
| 26 | 89.2 | 89.2 | 82.8 | 94.2 | 70.1 | 81.4 | 91.3 |
| 316 | 85.3 | 85.3 | 81.5 | 91.3 | 66.4 | 79.8 | 89.8 |
| 371 | 80.2 | 80.2 | 81 | 87.8 | 65.9 | 78.1 | 87.5 |
| 427 | 73.9 | 73.9 | 79.4 | 82.3 | 64.7 | 74.8 | 83.5 |
| 538 | 57.3 | 57.3 | 55.4 | 62.4 | 66.4 | ||
| 649 | 34.3 | 34.3 |
Factors in percent of the room-temperature allowable.
Other AISI 301and Relateda,b,c Tables
- AISI 301and Relateda,b,c-� Hard Sheet and strip (Table 2.7.1.0(b))
- AISI 301and Relateda,b,c-� Hard Sheet and strip (Table 2.7.1.0(b))
- AISI 301and Relateda,b,c-� Hard Sheet and strip (Table 2.7.1.0(b))
- AISI 301and Relateda,b,c-Annealed Sheet and strip (Table 2.7.1.0(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.