Materials/Metals and alloys/Stainless steels
Precipitation-hardening stainless steels
stainless-precipitation-hardeningAbout precipitation-hardening stainless steels
Precipitation-hardening stainless steels (17-4 PH): strength by heat-treatment condition, with sources.
Precipitation-hardening stainless steels gain strength from a low-temperature ageing treatment after solution annealing. Strength is set by the condition (A, H900, H1025, H1150), so values are listed by condition.
At a glance
- Highest density: 17-4 PH stainless steel reaches 7.86 g/cm³. Lowest: 17-7 PH stainless steel starts at 7.65 g/cm³. (3 of 3 grades have a sourced value.)
Ranges run across the conditions each source reports (temper, heat treatment, form), measured at room temperature where the source says so.
How they compare
The same measurements for every material in the collection. A range means the grade has values under several conditions; "at least" means the source gives a specified minimum. "no data" means no sourced value yet. For ranked tables, open a benchmark.
| Material | Yield strength | Tensile strength | Density | Young's modulus | Thermal conductivity | Melting point |
|---|---|---|---|---|---|---|
| 17-4 PH stainless steelprecipitation-hardening structural alloy | 725 to 1,262 MPa | 930 to 1,365 MPa | 7.75 to 7.86 g/cm³ | 196 to 201 GPa | 17.9 to 22.6 W/(m·K) | 1,404 to 1,440 °C |
| 17-7 PH stainless steelhigh-strength semi-austenitic precipitation-hardening stainless steel | 310 to 1,896 MPa | 827 to 2,034 MPa | 7.65 to 7.81 g/cm³ | 200 GPa | 16.9 W/(m·K) | 1,404 to 1,440 °C |
| PH 15-7 Mo stainless steel (15-7 PH)Semi-austenitic precipitation-hardening stainless steel for high-strength springs, rings and aircraft parts | 380 to 1,515 MPa | 860 to 1,690 MPa | 7.67 to 7.8 g/cm³ | 200 GPa | 16.2 W/(m·K) | no data |
What these materials are made of
Composition by weight, as printed in the sources for each grade (the first constituents listed).
| Material | Main constituents |
|---|---|
| 17-4 PH stainless steel | Fe balance · Cr 15 to 17.5% · Ni 3 to 5% · Cu 3 to 5% · Nb+Ta 0.15 to 0.45% · C up to 0.07% · Mn up to 1% |
| 17-7 PH stainless steel | Fe balance · Cr 16 to 18% · Ni 6.5 to 7.75% · Al 0.75 to 1.5% · C up to 0.09% · Mn, Si, P, S up to 1.00% |
Where they are used
| Use | Grades |
|---|---|
| Aircraft and missile fittings | 17-4 PH stainless steel |
| Bolts and fasteners | 17-4 PH stainless steel |
| Jet engine stator vanes | 17-4 PH stainless steel |
| Reaction-motor and support-equipment fittings for rocket-driven spacecraft | 17-7 PH stainless steel |
| Flat springs, Belleville (conical spring) washers and eyelets | 17-7 PH stainless steel |
| Aerospace bulkheads, retaining rings and tooling | 17-7 PH stainless steel |
| Springs and spring-type parts | PH 15-7 Mo stainless steel (15-7 PH) |
| Seal rings and retaining rings | PH 15-7 Mo stainless steel (15-7 PH) |
| Aircraft components | PH 15-7 Mo stainless steel (15-7 PH) |
When each grade fits
| Material | Best for | Weakest at |
|---|---|---|
| 17-4 PH stainless steel | High-strength fittings, fasteners, shafts and valve parts that need more strength than 304 and moderate corrosion resistance | Stress corrosion cracking and pitting in peak-aged (H900) material, and crevice corrosion in stagnant salt water |
| 17-7 PH stainless steel | Springs, Belleville washers, eyelets and flat springs that need high strength and stainless corrosion resistance, with formability in the soft state | Stress corrosion cracking in chloride and in nitrogen tetroxide/hydrazine propellant, in every heat-treated condition except CH 900; ductility in CH 900 (2 % elongation) |
| PH 15-7 Mo stainless steel (15-7 PH) | Springs, retaining rings and seal rings that need high strength with a low-distortion hardening heat treatment (ATI and Ulbrich list these uses) | Stress corrosion cracking in salt water: the 1969 NASA test found the alloy cracked in all conditions except CH 900, and corrosion resistance is below Type 304 (ATI) |