17-4PH-H1150 Bar: MIL-HDBK-5J Design Allowables
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| Material class | Steel |
| Alloy / temper / form | 17-4PH / H1150 / Bar |
| Specifications | AMS 5643 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 2.6.9.0, Table 2.6.9.0(e) (pdf page 199 of the chapter file) |
| Dimension bands | 1 |
| Density | 0.284 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 | 0–8 in | ||
|---|---|---|---|
| Specification | AMS 5643 | ||
| Basis | A | B | |
| Ftu, ksi | L | 125 | 134 |
| Fty, ksi | L | 100 | 115 |
| Fcy, ksi | L | 90 | 104 |
| Fsu, ksi | L | 79 | 85 |
| Fbru (e/D = 1.5), ksi | L | 213 | 228 |
| Fbru (e/D = 2.0), ksi | L | 270 | 289 |
| Fbry (e/D = 1.5), ksi | L | 152 | 175 |
| Fbry (e/D = 2.0), ksi | L | 181 | 208 |
| e, % | L | 16 | 16 |
| E, Msi | 28.5 | 28.5 | |
| Ec, Msi | 30 | 30 | |
| G, Msi | 11.2 | 11.2 | |
| ν | 0.27 | 0.27 | |
| ρ, lb/in3 | 0.284 | 0.284 | |
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
| °F | F_tu | F_ty |
|---|---|---|
| 100 | 98.9 | 99.2 |
| 200 | 95.8 | 97.4 |
| 300 | 93 | 95.4 |
| 400 | 90.1 | 93.5 |
| 500 | 87.2 | 91.5 |
| 600 | 84.1 | 89.9 |
| 700 | 81.4 | 87.2 |
| 800 | 77.7 | 83.5 |
| 1000 | 65.8 | 68.7 |
Factors in percent of the room-temperature allowable.
Other 17-4PH Tables
- 17-4PH Investment Casting (Table 2.6.9.0(f))
- 17-4PH-H1000 Investment Casting (Table 2.6.9.0(f))
- 17-4PH-H1025 Bar (Table 2.6.9.0(e))
- 17-4PH-H1025 Forging, tubing, and rings (Table 2.6.9.0(d))
- 17-4PH-H1025 Sheet, strip, and plate (Table 2.6.9.0(b))
- 17-4PH-H1075 Bar (Table 2.6.9.0(e))
- 17-4PH-H1075 Forging, tubing, and rings (Table 2.6.9.0(d))
- 17-4PH-H1075 Sheet, strip, and plate (Table 2.6.9.0(b))
- 17-4PH-H1100 Bar (Table 2.6.9.0(e))
- 17-4PH-H1100 Forging, tubing, and rings (Table 2.6.9.0(d))
- 17-4PH-H1100 Investment Casting (Table 2.6.9.0(f))
- 17-4PH-H1100 Sheet, strip, and plate (Table 2.6.9.0(b))
- 17-4PH-H1150 Forging, tubing, and rings (Table 2.6.9.0(d))
- 17-4PH-H1150 Sheet, strip, and plate (Table 2.6.9.0(b))
- 17-4PH-H1150Ma Bar (Table 2.6.9.0(e))
- 17-4PH-H1150Ma Forging, tubing, and rings (Table 2.6.9.0(d))
- 17-4PH-H900 Bar (Table 2.6.9.0(e))
- 17-4PH-H900 Forging, tubing, and rings (Table 2.6.9.0(d))
- 17-4PH-H900 Sheet, strip, and plate (Table 2.6.9.0(b))
- 17-4PH-H925 Bar (Table 2.6.9.0(e))
- 17-4PH-H925 Forging, tubing, and rings (Table 2.6.9.0(d))
- 17-4PH-H925 Sheet, strip, and plate (Table 2.6.9.0(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.