15-5 PH stainless steel 15-5 PH (UNS S15500, AMS 5659)

Fe balance, 14.00 to 15.50 Cr, 3.50 to 5.50 Ni, 2.50 to 4.50 Cu, 0.15 to 0.45 Nb plus Ta, max 0.07 C, max 1.00 Mn, max 1.00 Si, max 0.040 P, max 0.030 S (wt%)

Also known as UNS S15500, EN 1.4545, AMS 5659, ASTM A564, PH15-5

15-5 PH is a precipitation-hardening stainless steel (UNS S15500) with 14.00 to 15.50 percent chromium, 3.50 to 5.50 percent nickel and 2.50 to 4.50 percent copper.

8 sources · Updated 2026-11-01 · CC BY 4.0

Evidence level

2 of 5

Lab-measured

Recipe, share of the weight

  • Fe balanceIron
  • Cr 14 to 15.5%Chromium
  • Ni 3.5 to 5.5%Nickel
  • Cu 2.5 to 4.5%Copper
  • Nb+Ta 0.15 to 0.45%Niobium plus tantalum
  • C 0 to 0.07%Carbon

Best for

Fittings, shafts, gears and valve parts that need high strength from one aging step and moderate corrosion resistance

Weakest at

Ductility at the highest strength (elongation of 6 % at H900), and no chloride, stress-corrosion or sour-service data in the sources read

Risk at a glance

  • People None found. Nickel is the hazard in the record
  • If it fails Moderate. Loss of strength at a higher aging temperature
  • Corrosion Low. Corrosion resistance is comparable to Types 302 and 304 in many environments.

Quick facts: 15-5 PH (UNS S15500, AMS 5659)

Key properties of 15-5 PH (UNS S15500, AMS 5659)
PropertyValueBasis
Density7.8 g/cm³1 sourced value
Yield strength724 to 1,172 MPa4 sourced values across conditions
Tensile strength931 to 1,310 MPa4 sourced values across conditions
Young's modulus200 GPa1 sourced value
Hardness (Brinell)388 Bhn1 sourced value
Thermal conductivity17.8 W/(m·K)1 sourced value
Thermal expansion (CTE)10.8 ppm/K1 sourced value
Melting point1,404 to 1,440 °C1 sourced value

What is the density of 15-5 PH stainless steel?

15-5 PH stainless steel has a density of 7.8 g/cm³. The source and test conditions are listed in the properties table on this page.

What is the thermal conductivity of 15-5 PH stainless steel?

15-5 PH stainless steel has a thermal conductivity of 17.8 W/(m·K). The source and test conditions are listed in the properties table on this page.

What is the coefficient of thermal expansion of 15-5 PH stainless steel?

15-5 PH stainless steel has a coefficient of thermal expansion of 10.8 ppm/K. The source and test conditions are listed in the properties table on this page.

What is the melting point of 15-5 PH stainless steel?

15-5 PH stainless steel has a melting point of 1,404 to 1,440 °C. The source and test conditions are listed in the properties table on this page.

What is the yield strength of 15-5 PH stainless steel?

15-5 PH stainless steel has a yield strength of 724 to 1,172 MPa. The range covers 4 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.

What are the other names and codes for 15-5 PH stainless steel?

15-5 PH stainless steel is also written as UNS S15500, EN 1.4545, AMS 5659, ASTM A564, PH15-5. Each code is printed in the source listed beside it in the designations table.

What is 15-5 PH stainless steel used for?

Uses recorded in the sources include Aerospace structural components; Valves, gears and shafts.

Why it exists

15-5 PH is chosen when a stainless steel must reach high strength from a single low-temperature heat treatment, with corrosion resistance close to Types 302 and 304 in many environments. The SSA table gives a yield strength of 170,000 psi at H900 and 105,000 psi at H1150, and the choice of aging condition is the main design decision.

Where it's used

Aerospace structural components

The SSA product page lists aerospace structural components among the typical applications of 15-5 PH, and Titanium.com says the alloy meets requirements for aerospace and nuclear applications.

Valves, gears and shafts

The SSA page lists valves, gears and shafts among the typical applications. The Bibus page also lists valves, gears and pumps, and fasteners.

Recipe

Fe balance, 14.00 to 15.50 Cr, 3.50 to 5.50 Ni, 2.50 to 4.50 Cu, 0.15 to 0.45 Nb plus Ta, max 0.07 C, max 1.00 Mn, max 1.00 Si, max 0.040 P, max 0.030 S (wt%)

15-5 PH is an iron-based precipitation-hardening stainless steel, UNS S15500 (AMS 5659), made to the composition limits in the identity record with iron as the balance. Its strength is set by a low-temperature aging step to condition H900, H1025 or H1150 (SSA, Titanium.com).

What 15-5 PH (UNS S15500, AMS 5659) is made of
IngredientShare of the weightWhat it does
Iron Fe balance Matrix of the alloy.
Chromium Cr 14 to 15.5% Gives the passive film that resists general corrosion.
Nickel Ni 3.5 to 5.5% Part of the chromium-nickel-copper alloy that responds to aging.
Copper Cu 2.5 to 4.5% Forms the copper-rich phase that gives the strength on aging.
Niobium plus tantalum Nb+Ta 0.15 to 0.45% Alloying addition printed as Columbium plus Tantalum (SSA).
Carbon C 0 to 0.07% Kept low, maximum 0.07 percent.

Weight shares are as printed in the sources.

What it can do

Strength

yield strength of 170,000 psi and tensile strength of 190,000 psi at H900 (SSA). At H1025 the same table gives 145,000 psi and 155,000 psi.

Minimum strength

1000 MPa yield and 1070 MPa tensile at H1025, as printed as minimum values on the Bibus page.

Hardness and ductility

Brinell hardness of 388 Bhn at H900, and elongation of 6 % at H900 rising to 11 % at H1150 (SSA).

Stiffness

elastic modulus of 29000 ksi, printed without a temper on the Titanium.com page.

How it compares

Bibus says that in many corrosive environments the corrosion resistance of 15-5 PH is better than that of 410 stainless steel and comparable to that of Types 302 and 304. Titanium.com calls its corrosion resistance excellent but gives no test conditions. The SSA table gives separate strength rows for each aging condition, so the strength depends on which condition is ordered.

The same measurements for each material, so you can compare them. Each row names the key condition under the value; the full conditions and methods are in the numbered notes under Technical details. Other materials are shown beside it; each was measured under its own conditions, so open its page before comparing closely. Compare every grade in the family.

Benchmarks
Measurement15-5 PH (UNS S15500, AMS 5659)17-4 PH (UNS S17400, Type 630)17-7 PH (UNS S17700, EN 1.4568, Type 631)15-7 PH
Thermal behavior and safety
melting point1404 to 1440 °C21404 °C1404 to 1440 °Cno data
Thermal conductivity17.8 W/m-°C317.9 W/m.K16.9 W/(m·K)16.2 W/m-K
Physical and electrical
Density7.8 g/cm³17.75 g/cm³7.81 g/cm³7.8 g/cm³
brinell hardness388 Bhn12no datano datano data
Other measurements
Thermal expansion (CTE)10.8 μm/m-°C411.3 10-6/°C17.3 µm/(m·°C)14.4 10^-6/C
yield strength> 1000 MPa51262 MPa310 MPa380 MPa
ultimate tensile strength> 1070 MPa61365 MPa827 MPa860 MPa
elongation> 11 %715 %35 %30 %
yield strength1.7×10^5 psi81262 MPa310 MPa380 MPa
ultimate tensile strength1.9×10^5 psi91365 MPa827 MPa860 MPa
elongation6 %1015 %35 %30 %
reduction of area15 %11no datano datano data
yield strength1.45×10^5 psi131262 MPa310 MPa380 MPa
ultimate tensile strength1.55×10^5 psi141365 MPa827 MPa860 MPa
elongation8 %1515 %35 %30 %
yield strength1.05×10^5 psi161262 MPa310 MPa380 MPa
ultimate tensile strength1.35×10^5 psi171365 MPa827 MPa860 MPa
elongation11 %1815 %35 %30 %
elastic modulus29000 ksi19196 GPa200 GPa28 10^6 psi

Why choose it, and why not

Good for

  • Fittings, shafts, gears and valve parts that need high strength from a single low-temperature heat treatment (SSA).
  • Structural components that the SSA page lists as typical aerospace use.

Watch out for

  • Strength falls as the aging temperature rises: 170,000 psi yield at H900 against 105,000 psi at H1150 (SSA).
  • The sources read give no chloride, sea-water or stress-corrosion data, so check the data for the chosen condition in the environment.
  • Nickel, one of the alloying elements, is classified Danger in PubChem's elemental summary (CID 935).

15-5 PH is the strong stainless choice when a low-temperature aging step can set the strength. The aging condition sets the trade: H900 gives the most strength and H1150 gives the most elongation.

Technical details

For scientists and researchers. Everything above comes from the record below: every number with its method, its conditions and its source.

Other names and standards

The same grade under other systems, as datasheets and standards print them. Each code was checked against the page it comes from.

Other names and standards
SystemCodes
UNSS15500
EN1.4545
AMS5659
ASTMA564 (type XM-12)
Trade namePH15-5

Notes

The method, full conditions and any caveat for the numbered rows above.

Notes for the numbered rows
#MeasurementMethodConditionsCaveat
1DensityValue printed on the Bibus product page as Density 7.8 g/cm³condition not stated on the page (physical constants list)—
2melting pointRange printed on the Bibus product page as Melting point 1404 - 1440 °Cbasis melting range as printed—
3Thermal conductivityValue printed on the Bibus product page as Thermal conductivity at 150°temperature 150 (printed as 150° on the page)condition not stated—
4Thermal expansion (CTE)Value printed on the Bibus product page as Coefficient of expansion at 21-93 °Ctemperature range 21 to 93 °C (printed as 21-93 °C)—
5yield strengthRow printed under the Bibus heading for condition H1025 (Yield strength min. 1000 MPa)condition H1025 (AMS 5659)basis row printed as min.; the table heading says typical—
6ultimate tensile strengthRow printed under the Bibus heading for condition H1025 (Tensile strength min. 1070 MPa)condition H1025 (AMS 5659)basis row printed as min.; the table heading says typical—
7elongationRow printed under the Bibus heading for condition H1025 (Elongation min. 11 %)condition H1025 (AMS 5659)basis row printed as min.; the table heading says typical—
8yield strengthValue printed in the AMS 5659 mechanical properties table on the SSA pagecondition H900basis row printed as yield 0.2% offset; the page does not say minimum or typical—
9ultimate tensile strengthValue printed in the AMS 5659 mechanical properties table on the SSA pagecondition H900basis row printed as tensile; the page does not say minimum or typical—
10elongationValue printed in the AMS 5659 mechanical properties table on the SSA pagecondition H900gauge in 2 inch (as printed)—
11reduction of areaValue printed in the AMS 5659 mechanical properties table on the SSA page (name not in the canonical list)condition H900—
12brinell hardnessValue printed in the AMS 5659 mechanical properties table on the SSA page (name not in the canonical list)condition H900—
13yield strengthValue printed in the AMS 5659 mechanical properties table on the SSA pagecondition H1025basis row printed as yield 0.2% offset; the page does not say minimum or typical—
14ultimate tensile strengthValue printed in the AMS 5659 mechanical properties table on the SSA pagecondition H1025basis row printed as tensile; the page does not say minimum or typical—
15elongationValue printed in the AMS 5659 mechanical properties table on the SSA pagecondition H1025gauge in 2 inch (as printed)—
16yield strengthValue printed in the AMS 5659 mechanical properties table on the SSA pagecondition H1150basis row printed as yield 0.2% offset; the page does not say minimum or typical—
17ultimate tensile strengthValue printed in the AMS 5659 mechanical properties table on the SSA pagecondition H1150basis row printed as tensile; the page does not say minimum or typical—
18elongationValue printed in the AMS 5659 mechanical properties table on the SSA pagecondition H1150gauge in 2 inch (as printed)—
19elastic modulusValue read from the Modulus of Elasticity line of the Titanium.com mechanical properties table; the page gives no temper, and the pairing with its header was read from table layoutcondition not stated on the page—

Corrosion and compatibility

What happens when it meets other materials and environments.

Corrosion and compatibility
EnvironmentConcernWhat happens
Corrosive environments in general (no test conditions given) low Corrosion resistance is comparable to Types 302 and 304 in many environments.1
General corrosion (no test conditions given) low The Titanium.com page calls its corrosion resistance excellent.2
Corrosion details
#EnvironmentDetailsTest conditions
1 Corrosive environments in general (no test conditions given) The Bibus page says that in many corrosive environments its resistance is better than that of 410 stainless steel and comparable to that of 302 and 304 stainless steels. The page gives no test conditions. basis manufacturer-style product statement; no test conditions printed
2 General corrosion (no test conditions given) The stockist page says the alloy exhibits excellent corrosion resistance. The page gives no chloride, sea-water or stress-corrosion test data. basis product statement only; no test conditions printed

Risks and side effects

Hazards to people, what happens when a cell overheats, and how the material is handled and stored.

For people

The hazard entry is for elemental nickel. No safety data sheet for the alloy was opened in this run.

Nickel
PubChem's GHS summary for elemental nickel (CID 935) gives the signal word Danger with H317, H351 and H372.
Workshop
Check the supplier safety data sheet before cutting, grinding or welding this alloy.

In service

The strongest condition is the least ductile.

Aging
On the SSA table, yield strength is 170,000 psi at H900 and 105,000 psi at H1150, while elongation rises from 6 % to 11 %.
Corrosion
Bibus says its corrosion resistance is comparable to Types 302 and 304 in many corrosive environments. The sources read give no chloride or stress-corrosion data.

Handling and fabrication

Welding
The SSA page says the alloy is readily weldable.
Machining
The SSA page says it can be machined in any of the several thermal conditions available to this grade.

Test details
The original wording and numbers from the sources, for readers who want them.

Failure risks

Failure risks
FailureTrigger and consequence
Loss of strength at a higher aging temperaturemoderate severityAging to H1150 instead of H900Yield strength falls from 170,000 psi at H900 to 105,000 psi at H1150 on the SSA table, and elongation rises from 6 % to 11 %.

Handling and storage

  • The SSA page says the alloy is readily weldable, and that it can be machined in any of the several thermal conditions available to this grade.

Mitigations

  • Choose the aging condition for the load: the SSA table prints separate H900, H1025 and H1150 rows, so the condition sets both strength and elongation.

Supply and geography

How common the raw materials are and where they come from.

Chromium

Top producers (2025)
South Africa 45.1%, Turkey 17.6%, Kazakhstan 13.7%, India 5.9%
Recycling
USGS: in 2025 recycled chromium, contained in reported stainless-steel scrap receipts, accounted for 21% of apparent consumption.
Substitutes
USGS: chromium has no substitute in stainless steel, the leading end use.

Nickel

Top producers (2025)
Indonesia 66.7%, Philippines 6.9%, Russia 5.1%, Canada 3.6%
Recycling
USGS: in 2025 nickel recovered from scrap accounted for approximately 60% of apparent consumption.

Niobium (columbium)

Top producers (2025)
Brazil 92.9%, Canada 5.4%
Recycling
USGS: niobium was recycled when niobium-bearing steels and superalloys were recycled.
Substitutes
USGS: substitutes for niobium carry a performance loss or higher cost, as the chapter states.

Copper

Top producers (2025)
Chile 23%, Congo (Kinshasa) 13.9%, Peru 11.7%, China 7.8%

Updated