Hastelloy X-Solution treated (annealed) Sheet and plate: MIL-HDBK-5J Design Allowables
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| Material class | Heat-Resistant |
| Alloy / temper / form | Hastelloy X / Solution treated (annealed) / Sheet and plate |
| Specifications | AMS 5536 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 6.3.1.0, Table 6.3.1.0(b) (pdf page 22 of the chapter file) |
| Dimension bands | 6 |
| Density | 0.297 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 | 0.000–0.010 in | 0.010–0.019 in | 0.020–0.100 in | 0.101–0.187 in | 0.188–2.000 in | 2– in | ||
|---|---|---|---|---|---|---|---|---|
| Specification | AMS 5536 | AMS 5536 | AMS 5536 | AMS 5536 | AMS 5536 | AMS 5536 | ||
| Basis | S | S | A | B | S | S | S | |
| Ftu, ksi | LT | 105 | 105 | 102 | 106 | 105 | 100 | 95 |
| Fty, ksi | LT | 45 | 45 | 44 | 47 | 45 | 40 | 40 |
| e, % | LT | … | 29 | 35 | 35 | 35 | 35 | 35 |
| E, Msi | 29.8 | 29.8 | 29.8 | 29.8 | 29.8 | 29.8 | 29.8 | |
| Ec, Msi | 29.8 | 29.8 | 29.8 | 29.8 | 29.8 | 29.8 | 29.8 | |
| G, Msi | 11.3 | 11.3 | 11.3 | 11.3 | 11.3 | 11.3 | 11.3 | |
| ν | 0.32 | 0.32 | 0.32 | 0.32 | 0.32 | 0.32 | 0.32 | |
| ρ, lb/in3 | 0.297 | 0.297 | 0.297 | 0.297 | 0.297 | 0.297 | 0.297 | |
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
| °F | F_tu | F_ty |
|---|---|---|
| 100 | 98.6 | 98.6 |
| 200 | 99.3 | 95.9 |
| 300 | 97.9 | 93.6 |
| 400 | 96.4 | 91.7 |
| 500 | 94.8 | 89.8 |
| 600 | 93 | 87.9 |
| 700 | 90.6 | 86.4 |
| 800 | 87.7 | 85 |
| 1000 | 80 | 80 |
| 1200 | 66.6 | 71.5 |
Factors in percent of the room-temperature allowable.
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.