PH 13-8Mo stainless steel PH 13-8Mo

Iron-based precipitation-hardening stainless steel: iron with chromium, nickel, molybdenum and aluminium as the main alloying elements (limits in the recipe parts)

Also known as UNS S13800, EN 1.4534, AMS 5629, PH 13-8 Mo

PH 13-8 Mo (UNS S13800, EN 1.4534, AMS 5629) is a precipitation-hardening stainless steel.

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

Evidence level

2 of 5

Lab-measured

Carry load

1449 MPa yield (H 950, typical)

Resist impact

41 J Charpy (H 1000, typical)

Carry heat

14.0 W/m-K at 100 °C

Weight

7.76 g/cm3

Melting

1404 °C

Recipe, share of the weight

  • Fe balance (Bibus prints Rest)Iron
  • Cr 12.25 to 13.25%Chromium
  • Ni 7.5 to 8.5%Nickel
  • Mo 2 to 2.5%Molybdenum
  • Al 0.9 to 1.35%Aluminium

Best for

Strong stainless parts for marine or humid air: a typical yield strength of 1449 MPa in condition H 950 and a high level of stress-corrosion resistance in marine tests

Weakest at

Strength falls as the ageing temperature rises, and toughness rises with it; no space-environment data (outgassing, atomic oxygen or radiation) for this alloy were found in any source read

Risk at a glance

  • People Low. Nickel hazard codes only, not the alloy's own SDS
  • If it fails Moderate. Stress-corrosion cracking of under-aged parts
  • Corrosion Low. The datasheet reports a high level of resistance to stress-corrosion cracking in marine tests.

Quick facts: PH 13-8Mo

Key properties of PH 13-8Mo
PropertyValueBasis
Density7.76 g/cm³1 sourced value
Yield strength1,138 to 1,449 MPa5 sourced values across conditions
Tensile strength1,207 to 1,551 MPa5 sourced values across conditions
Thermal conductivity12.8 W/(m·K)1 sourced value
Thermal expansion (CTE)13 ppm/K2 sourced values across conditions
Melting point1,404 °C1 sourced value
Electrical resistivity1,020 microhm-mm1 sourced value

What is the density of PH 13-8Mo stainless steel?

PH 13-8Mo stainless steel has a density of 7.76 g/cm³. The source and test conditions are listed in the properties table on this page.

What is the thermal conductivity of PH 13-8Mo stainless steel?

PH 13-8Mo stainless steel has a thermal conductivity of 12.8 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 PH 13-8Mo stainless steel?

PH 13-8Mo stainless steel has a coefficient of thermal expansion of 13 ppm/K. The range covers 2 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.

What is the melting point of PH 13-8Mo stainless steel?

PH 13-8Mo stainless steel has a melting point of 1,404 °C. The source and test conditions are listed in the properties table on this page.

What is the yield strength of PH 13-8Mo stainless steel?

PH 13-8Mo stainless steel has a yield strength of 1,138 to 1,449 MPa. The range covers 5 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 PH 13-8Mo stainless steel?

PH 13-8Mo stainless steel is also written as UNS S13800, EN 1.4534, AMS 5629, PH 13-8 Mo. Each code is printed in the source listed beside it in the designations table.

What is PH 13-8Mo stainless steel used for?

Uses recorded in the sources include Valve parts, fittings and shafts; Aircraft components, nuclear reactor components and petrochemical parts.

Why it exists

Precipitation hardening, also called age hardening, is a heat treatment that raises the yield strength of malleable materials (Wikipedia). PH 13-8 Mo is a precipitation-hardening stainless steel, chosen where a stainless part needs high strength and toughness together. The Bibus datasheet gives a minimum yield strength of 1413 MPa in condition H950 and a minimum tensile strength of 1517 MPa. The HiTemp Metals datasheet gives a typical yield strength of 1449 MPa for the same condition. Its aerospace and valve uses rest on the combination: a Charpy V-notch energy of 27 J in H 950 and 41 J in H 1000.

Where it's used

Valve parts, fittings and shafts

The HiTemp Metals datasheet says the alloy has been used for valve parts, fittings, cold-headed and machined fasteners, and shafts.

Aircraft and reactor parts

The same datasheet lists aircraft components, nuclear reactor components and petrochemical applications.

Recipe

Iron-based precipitation-hardening stainless steel: iron with chromium, nickel, molybdenum and aluminium as the main alloying elements (limits in the recipe parts)

PH 13-8 Mo is an iron-based precipitation-hardening stainless steel. Chromium, nickel, molybdenum and aluminium are the main alloying elements, and carbon, manganese, silicon, nitrogen and phosphorus are kept low. Precipitation hardening is a heat treatment that raises strength by forming fine particles in the metal (Wikipedia). The Bibus limits are in the identity block.

What PH 13-8Mo is made of
IngredientShare of the weightWhat it does
Iron Fe balance (Bibus prints Rest) The matrix that the other elements are added to.
Chromium Cr 12.25 to 13.25% Gives the stainless corrosion resistance; Wikipedia says 10.5% or more forms the passive film.
Nickel Ni 7.5 to 8.5% Alloying element printed in the composition table; its role in this grade is not described in the sources read.
Molybdenum Mo 2 to 2.5% Alloying element printed in the composition table; its role in this grade is not described in the sources read.
Aluminium Al 0.9 to 1.35% Alloying element printed in the composition table; the datasheets do not say how it forms the hardening particles.

Weight shares are as printed in the sources.

What it can do

Carry load

1449 MPa yield (H 950, typical)

measured

The typical yield strength is 1449 MPa in condition H 950 (HiTemp Metals). The Bibus minimum for the same condition is 1413 MPa.

Resist impact

41 J Charpy (H 1000, typical)

measured

Charpy V-notch energy is 41 J in condition H 1000 and 27 J in condition H 950 (HiTemp Metals, typical longitudinal values).

Carry heat

14.0 W/m-K at 100 °C

measured

Thermal conductivity is 14.0 W/m-K at 100 °C in condition A (HiTemp Metals), and 12.8 W/m - °C at 20 °C (Bibus). The two sources test at different temperatures.

Weight

7.76 g/cm3

measured

Density is 7.76 g/cm3 in the Bibus datasheet, with no condition printed.

Melting

1404 °C

measured

The Bibus datasheet gives a single melting point of 1404 °C, with no range.

Marine stress-corrosion

high resistance, qualitative

The HiTemp Metals datasheet reports a high level of resistance to stress-corrosion cracking in marine tests, without a numeric threshold.

How it compares

Against Type 304 stainless steel, the HiTemp Metals datasheet says PH 13-8 Mo's general-corrosion resistance approaches that of Type 304, and that its rusting resistance in 5 weight percent salt fog is similar to Type 304 in condition H 950. The reason to choose PH 13-8 Mo is strength: its typical yield strength is 1449 MPa in H 950, against the Bibus minimum of 1413 MPa for the same condition. The two datasheets use different bases, so read the table rows as examples, not a ranking.

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
MeasurementPH 13-8Mo304 (UNS S30400)316 (UNS S31600)316L (UNS S31603)2205 (UNS S32205)2507 (UNS S32750)17-4 PH (UNS S17400, Type 630)440C (UNS S44004)410 (UNS S41000)430 (UNS S43000)S41500 (F6NM forged, CA6NM cast)301 (UNS S30100)303 (UNS S30300)2304 (UNS S32304, EN 1.4362)409 (UNS S40900, EN 1.4512)444 (UNS S44400)302304L (UNS S30403)309310S (UNS S31008, EN 1.4845)317L321347347H904L (UNS N08904, EN 1.4539)Nitronic 602101430F (UNS S43020)410S (UNS S41008)416420431 (UNS S43100, EN 1.4057)1.4418 (X4CrNiMo16-5-1)17-7 PH (UNS S17700, EN 1.4568, Type 631)15-7 PH
Capacity and energy
Charpy V-notch impact energy, H 1000, typical longitudinal (HiTemp Metals datasheet)41 J18no datano datano data> 27 Jno data20 Jno datano datano data70 Jno datano data> 40 Jno datano datano datano datano datano data65 to 100 ft-lbfno datano datano datano data187.8 Jno datano datano datano datano datano data> 90 Jno datano data
Charpy V-notch impact energy, H 950, typical longitudinal (HiTemp Metals datasheet)27 J19no datano datano data> 27 Jno data20 Jno datano datano data70 Jno datano data> 40 Jno datano datano datano datano datano data65 to 100 ft-lbfno datano datano datano data187.8 Jno datano datano datano datano datano data> 90 Jno datano data
Thermal behavior and safety
Melting point, PH 13-8 Mo (Bibus datasheet)Single value printed in a supplier datasheet1404 °C1673 K1390 °C1390 °C2525 to 2625 °Fno data1404 °C2500 to 2700 °F1482 to 1532 °C1425 to 1510 °Cno data1399 to 1421 °C1455 °Cno datano datano data1420 °C1399 to 1421 °C2550 to 2650 °F1410 °C1390 to 1440 °C1398 to 1446 °C1398 to 1446 °C2550 to 2635 degF1300 to 1390 °Cno data2525 to 2630 °F1482 °C1480 to 1530 °C2714 °F2650 to 2750 °Fno datano data1404 to 1440 °Cno data
Thermal conductivity at 20 °C, PH 13-8 Mo (Bibus datasheet)Value printed in a supplier datasheet12.8 W/m - °C14 W/m.K14.6 W/m.K14.6 W/m·K14 W/(m °C)14 W/m.K17.9 W/m.K24.2 W/m.K24.9 W/m-K23.86 W/m.K25 W/(m K)16.3 W/m.K15 W/m°C13 W/m.K25.8 W/m.K21.4 W/m.K16.2 W/(m·K)16.3 W/m·K15.6 W/m·K13 W/(m·K)14 W/(m·K)16.3 W/(m·K)16.3 W/(m·K)14 W/m.°C12 W/(m·K)9 Btu/ft hr °F16 W/(m·K)26.1 W/m.K26.9 W/m-K30 W/m K24.9 W/(m·K)25 W/(m·K)15 W/m K16.9 W/(m·K)16.2 W/m-K
Thermal conductivity at 100 °C, condition A (HiTemp Metals datasheet)Value printed in a supplier datasheet14 W/m-K114 W/m.K14.6 W/m.K14.6 W/m·K14 W/(m °C)14 W/m.K17.9 W/m.K24.2 W/m.K24.9 W/m-K23.86 W/m.K25 W/(m K)16.3 W/m.K15 W/m°C13 W/m.K25.8 W/m.K21.4 W/m.K16.2 W/(m·K)16.3 W/m·K15.6 W/m·K13 W/(m·K)14 W/(m·K)16.3 W/(m·K)16.3 W/(m·K)14 W/m.°C12 W/(m·K)9 Btu/ft hr °F16 W/(m·K)26.1 W/m.K26.9 W/m-K30 W/m K24.9 W/(m·K)25 W/(m·K)15 W/m K16.9 W/(m·K)16.2 W/m-K
Physical and electrical
Density, PH 13-8 Mo (Bibus datasheet)Value printed in a supplier datasheet7.76 g/cm³7.85 Mg/m38.027 g/cm³8.03 g/cm³7.82 g/cm³7.8 g/cm³7.75 g/cm³0.275 lb/in37.73 g/cm³7.7 g/cm³7.61 to 8.1 kg/dm38.03 g/cm³7.9 kg/dm37.8 g/cm³7.75 g/cm³7.75 g/cm³7.9 g/cm³7.9 g/cm³8.03 g/cm³7.8 kg/dm38.027 g/cm³7.92 g/cm³7.96 g/cm³7.98 kg/dm37.95 g/cm³7.622 gm/cm³7800 kg/m37700 kg/m37.73 g/cm³7.7 kg/dm37.75 g/cm³7800 kg/m37.7 kg/dm37.81 g/cm³7.8 g/cm³
Electrical resistivity, condition A (HiTemp Metals datasheet)1020 microhm-mm465 10-8 ohm.m69 10-8 ohm.m74 μΩ·cm0.74 10-6 ohm.m0.83 μΩm98 microhm-cm0.6 10-6 ohm.m57 µohm-cm60 micro-ohm-cmno data72 µΩ·cm72 microhm-cmno data60 micro-ohm-cm800 µΩ.mm72 µΩ·cm72 microhm-cm78 µΩ·cm0.86 Ω·mm²/m475 Ohm-circ mil/ft72 microhm·cm72 µΩ·cmno data95.2 µΩ·cm98.2 microhm-cmno data600 nΩ.m60 µohm-cm0.6 Ω mm2/m0.55 µΩ·m0.7 ohm mm2/mno data80 µΩ·cm82 microhm-cm
Hardness, Rockwell C, H 1000, typical longitudinal (HiTemp Metals datasheet)45 HRC17no datano datano datano datano data36 HRCno datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano data26 to 32 RC48 HRCno datano datano datano data
Other measurements
Mean coefficient of thermal expansion, 20 to 100 °C (Bibus datasheet)13 μm/m - °C2no data16.5 10-6/K16.5 10-6 cm/cm/°C13 10-6/K13.5 10-6/K11.3 10-6/°C10.1 10-6/K9.9 µm/m-°C10.3 10-6/Kno data16.6 10-6/K16 10-6/°C13 10-6/K10.5 10-6/°C10.3 10-6/°C16.6 µm/(m·°C)16.6 10-6 cm/cm/°C15.6 µm/(m·K)16.5 ppm/K16.5 10^-6 cm/cm/°C16.6 ppm/K16.6 ppm/K9.2 in/in.degF x 10^-615.8 ppm/K15.8 µm/m/°C13 µm/m/°C10.4 um/m/C10.8 µm/m·K10.5 10^-6/K10.3 10^-6/K10 ppm/K10.8 10-6 K-117.3 µm/(m·°C)14.4 10^-6/C
Mean coefficient of thermal expansion, condition H 1000, 21 to 204 °C (HiTemp Metals datasheet)Value printed in a supplier datasheet10.8 10⁻⁶/K3no data16.5 10-6/K16.5 10-6 cm/cm/°C13 10-6/K13.5 10-6/K11.3 10-6/°C10.1 10-6/K9.9 µm/m-°C10.3 10-6/Kno data16.6 10-6/K16 10-6/°C13 10-6/K10.5 10-6/°C10.3 10-6/°C16.6 µm/(m·°C)16.6 10-6 cm/cm/°C15.6 µm/(m·K)16.5 ppm/K16.5 10^-6 cm/cm/°C16.6 ppm/K16.6 ppm/K9.2 in/in.degF x 10^-615.8 ppm/K15.8 µm/m/°C13 µm/m/°C10.4 um/m/C10.8 µm/m·K10.5 10^-6/K10.3 10^-6/K10 ppm/K10.8 10-6 K-117.3 µm/(m·°C)14.4 10^-6/C
Yield strength 0.2 % offset, H 950, typical longitudinal (HiTemp Metals datasheet)1449 MPa5> 205 MPa205 MPa170 MPa> 450 MPa> 550 MPa1262 MPa1896 MPa205 to 290 MPa> 30 ksi> 520 MPa205 MPa> 172 MPa> 400 MPa> 170 MPa345 MPa290 MPa> 170 MPa290 MPa290 MPa> 205 MPa> 205 MPa> 205 MPa> 30 ksi> 240 MPa> 345 MPa> 450 MPa379 MPa> 30 ksi> 450 MPa51.5 ksi600 MPa> 550 MPa310 MPa380 MPa
Yield strength, H 950, minimum (Bibus datasheet)1413 MPa6> 205 MPa205 MPa170 MPa> 450 MPa> 550 MPa1262 MPa1896 MPa205 to 290 MPa> 30 ksi> 520 MPa205 MPa> 172 MPa> 400 MPa> 170 MPa345 MPa290 MPa> 170 MPa290 MPa290 MPa> 205 MPa> 205 MPa> 205 MPa> 30 ksi> 240 MPa> 345 MPa> 450 MPa379 MPa> 30 ksi> 450 MPa51.5 ksi600 MPa> 550 MPa310 MPa380 MPa
Yield strength 0.2 % offset, H 1000, typical longitudinal (HiTemp Metals datasheet)Typical value printed in a supplier datasheet1413 MPa7> 205 MPa205 MPa170 MPa> 450 MPa> 550 MPa1262 MPa1896 MPa205 to 290 MPa> 30 ksi> 520 MPa205 MPa> 172 MPa> 400 MPa> 170 MPa345 MPa290 MPa> 170 MPa290 MPa290 MPa> 205 MPa> 205 MPa> 205 MPa> 30 ksi> 240 MPa> 345 MPa> 450 MPa379 MPa> 30 ksi> 450 MPa51.5 ksi600 MPa> 550 MPa310 MPa380 MPa
Yield strength, H 1000, minimum (Bibus datasheet)1310 MPa8> 205 MPa205 MPa170 MPa> 450 MPa> 550 MPa1262 MPa1896 MPa205 to 290 MPa> 30 ksi> 520 MPa205 MPa> 172 MPa> 400 MPa> 170 MPa345 MPa290 MPa> 170 MPa290 MPa290 MPa> 205 MPa> 205 MPa> 205 MPa> 30 ksi> 240 MPa> 345 MPa> 450 MPa379 MPa> 30 ksi> 450 MPa51.5 ksi600 MPa> 550 MPa310 MPa380 MPa
Yield strength, H 1050, minimum (Bibus datasheet)1138 MPa9> 205 MPa205 MPa170 MPa> 450 MPa> 550 MPa1262 MPa1896 MPa205 to 290 MPa> 30 ksi> 520 MPa205 MPa> 172 MPa> 400 MPa> 170 MPa345 MPa290 MPa> 170 MPa290 MPa290 MPa> 205 MPa> 205 MPa> 205 MPa> 30 ksi> 240 MPa> 345 MPa> 450 MPa379 MPa> 30 ksi> 450 MPa51.5 ksi600 MPa> 550 MPa310 MPa380 MPa
Tensile strength, H 950, typical longitudinal (HiTemp Metals datasheet)Typical value printed in a supplier datasheet1551 MPa10> 515 MPa515 MPa485 MPa> 655 MPa800 to 1000 MPa1365 MPa1965 MPa450 to 510 MPa> 65 ksi< 1100 MPa515 MPa> 517 MPa> 600 MPa> 380 MPa517 MPa655 MPa> 485 MPa621 MPa610 MPa> 515 MPa> 515 MPa> 515 MPa> 75 ksi530 to 730 MPa> 655 MPa> 650 MPa552 MPa> 60 ksi650 to 850 N/mm285.8 ksi862 MPa760 to 960 MPa827 MPa860 MPa
Tensile strength, H 950, minimum (Bibus datasheet)1517 MPa11> 515 MPa515 MPa485 MPa> 655 MPa800 to 1000 MPa1365 MPa1965 MPa450 to 510 MPa> 65 ksi< 1100 MPa515 MPa> 517 MPa> 600 MPa> 380 MPa517 MPa655 MPa> 485 MPa621 MPa610 MPa> 515 MPa> 515 MPa> 515 MPa> 75 ksi530 to 730 MPa> 655 MPa> 650 MPa552 MPa> 60 ksi650 to 850 N/mm285.8 ksi862 MPa760 to 960 MPa827 MPa860 MPa
Tensile strength, H 1000, typical longitudinal (HiTemp Metals datasheet)Typical value printed in a supplier datasheet1482 MPa12> 515 MPa515 MPa485 MPa> 655 MPa800 to 1000 MPa1365 MPa1965 MPa450 to 510 MPa> 65 ksi< 1100 MPa515 MPa> 517 MPa> 600 MPa> 380 MPa517 MPa655 MPa> 485 MPa621 MPa610 MPa> 515 MPa> 515 MPa> 515 MPa> 75 ksi530 to 730 MPa> 655 MPa> 650 MPa552 MPa> 60 ksi650 to 850 N/mm285.8 ksi862 MPa760 to 960 MPa827 MPa860 MPa
Tensile strength, H 1000, minimum (Bibus datasheet)1413 MPa13> 515 MPa515 MPa485 MPa> 655 MPa800 to 1000 MPa1365 MPa1965 MPa450 to 510 MPa> 65 ksi< 1100 MPa515 MPa> 517 MPa> 600 MPa> 380 MPa517 MPa655 MPa> 485 MPa621 MPa610 MPa> 515 MPa> 515 MPa> 515 MPa> 75 ksi530 to 730 MPa> 655 MPa> 650 MPa552 MPa> 60 ksi650 to 850 N/mm285.8 ksi862 MPa760 to 960 MPa827 MPa860 MPa
Tensile strength, H 1050, minimum (Bibus datasheet)1207 MPa14> 515 MPa515 MPa485 MPa> 655 MPa800 to 1000 MPa1365 MPa1965 MPa450 to 510 MPa> 65 ksi< 1100 MPa515 MPa> 517 MPa> 600 MPa> 380 MPa517 MPa655 MPa> 485 MPa621 MPa610 MPa> 515 MPa> 515 MPa> 515 MPa> 75 ksi530 to 730 MPa> 655 MPa> 650 MPa552 MPa> 60 ksi650 to 850 N/mm285.8 ksi862 MPa760 to 960 MPa827 MPa860 MPa
Elongation in 2 in., H 1000, typical longitudinal (HiTemp Metals datasheet)Typical value printed in a supplier datasheet13 %15> 40 %40 %40 %> 25 %> 25 %15 %2 %20 to 34 %> 22 %15 %40 %> 35 %> 25 %> 20 %30 %55 %> 40 %49 %42 %> 40 %> 35 %> 40 %> 40 %> 35 %> 35 %> 30 %> 25 %> 22 %> 12 %12 to 13 %20 %> 16 %35 %30 %
Elongation, H 1000, minimum (Bibus datasheet)10 %16> 40 %40 %40 %> 25 %> 25 %15 %2 %20 to 34 %> 22 %15 %40 %> 35 %> 25 %> 20 %30 %55 %> 40 %49 %42 %> 40 %> 35 %> 40 %> 40 %> 35 %> 35 %> 30 %> 25 %> 22 %> 12 %12 to 13 %20 %> 16 %35 %30 %

Why choose it, and why not

Good for

  • Strong stainless parts in marine or humid air: the datasheet reports a high level of resistance to stress-corrosion cracking in marine tests.
  • Fasteners and valve parts in conditions H 950 to H 1050, the uses the datasheet lists.
  • Tough high-strength parts: 41 J Charpy V-notch energy in condition H 1000.

Watch out for

  • Strength depends on condition: the Bibus minimum yield strength falls from 1413 MPa at H950 to 1138 MPa at H1050.
  • Under-aged parts are at risk of stress-corrosion cracking, since the datasheet suggests a minimum ageing temperature of 1000°F (538°C).
  • The two datasheets disagree on thermal expansion: 13 μm/m - °C at 20 to 100 °C (Bibus) against 10.8 at 21 to 204 °C in H 1000 (HiTemp Metals).
  • No flight, outgassing, atomic-oxygen or radiation data for this alloy were found in any source read.

PH 13-8 Mo is a precipitation-hardening stainless steel with a typical yield strength of 1449 MPa in condition H 950 (HiTemp Metals) and a Bibus minimum of 1413 MPa. Its toughness rises as the condition moves from H 950 to H 1000, while yield strength falls slightly. Its stress-corrosion resistance in marine tests is described qualitatively as high. This profile has no space-environment data for the alloy, and no stress-corrosion table values, because that table could not be transcribed reliably.

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
UNSS13800
EN1.4534
AMS5629
Trade namePH 13-8 Mo

Notes

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

Notes for the numbered rows
#MeasurementMethodConditionsCaveat
1Thermal conductivity at 100 °C, condition A (HiTemp Metals datasheet)—temperature 100 °C (212 °F)condition printed Condition Aunit in source W/m-K—
2Mean coefficient of thermal expansion, 20 to 100 °C (Bibus datasheet)Value printed in a supplier datasheet; it differs from the HiTemp Metals value at a different temperature range (see gaps)temperature 20 to 100 °Cunit in source μm/m - °C—
3Mean coefficient of thermal expansion, condition H 1000, 21 to 204 °C (HiTemp Metals datasheet)—condition H 1000temperature 21 to 204 °C (70 to 400 °F)unit in source 10⁻⁶/K—
4Electrical resistivity, condition A (HiTemp Metals datasheet)Value printed in a supplier datasheet; the same page also prints 613 ohms c/mf (not recorded here)temperature 100 °C (212 °F)condition printed Condition Aunit in source microhm-mm—
5Yield strength 0.2 % offset, H 950, typical longitudinal (HiTemp Metals datasheet)Typical value printed in a supplier datasheet; this is a typical value, not a minimumcondition H 950form typical longitudinal, center or intermediate locationtemperature room temperaturebasis typical—
6Yield strength, H 950, minimum (Bibus datasheet)Minimum value printed under the heading Typical mechanical properties (room temperature)condition H950basis minimum, room temperature—
7Yield strength 0.2 % offset, H 1000, typical longitudinal (HiTemp Metals datasheet)—condition H 1000form typical longitudinal, center or intermediate locationtemperature room temperaturebasis typical—
8Yield strength, H 1000, minimum (Bibus datasheet)Minimum value printed under the heading Typical mechanical properties (room temperature)condition H1000basis minimum, room temperature—
9Yield strength, H 1050, minimum (Bibus datasheet)Minimum value printed under the heading Typical mechanical properties (room temperature)condition H1050basis minimum, room temperature—
10Tensile strength, H 950, typical longitudinal (HiTemp Metals datasheet)—condition H 950form typical longitudinal, center or intermediate locationtemperature room temperaturebasis typical—
11Tensile strength, H 950, minimum (Bibus datasheet)Minimum value printed under the heading Typical mechanical properties (room temperature)condition H950basis minimum, room temperature—
12Tensile strength, H 1000, typical longitudinal (HiTemp Metals datasheet)—condition H 1000form typical longitudinal, center or intermediate locationtemperature room temperaturebasis typical—
13Tensile strength, H 1000, minimum (Bibus datasheet)Minimum value printed under the heading Typical mechanical properties (room temperature)condition H1000basis minimum, room temperature—
14Tensile strength, H 1050, minimum (Bibus datasheet)Minimum value printed under the heading Typical mechanical properties (room temperature)condition H1050basis minimum, room temperature—
15Elongation in 2 in., H 1000, typical longitudinal (HiTemp Metals datasheet)—condition H 1000gauge length 2 in.form typical longitudinalbasis typical—
16Elongation, H 1000, minimum (Bibus datasheet)Minimum value printed under the heading Typical mechanical properties (room temperature)condition H1000basis minimum, room temperature—
17Hardness, Rockwell C, H 1000, typical longitudinal (HiTemp Metals datasheet)Typical value printed in a supplier datasheet; benchmark name is not in the canonical list (see gaps)condition H 1000form typical longitudinalbasis typical—
18Charpy V-notch impact energy, H 1000, typical longitudinal (HiTemp Metals datasheet)Typical value printed in a supplier datasheet; benchmark name is not in the canonical list (see gaps)condition H 1000form typical longitudinalbasis typicaltest Charpy V-notchunit in source ft-lb / J—
19Charpy V-notch impact energy, H 950, typical longitudinal (HiTemp Metals datasheet)Typical value printed in a supplier datasheet; benchmark name is not in the canonical list (see gaps)condition H 950form typical longitudinalbasis typicaltest Charpy V-notchunit in source ft-lb / J—

Corrosion and compatibility

What happens when it meets other materials and environments.

Corrosion and compatibility
EnvironmentConcernWhat happens
Marine atmosphere, strip tested at the Kure Beach site low The datasheet reports a high level of resistance to stress-corrosion cracking in marine tests.1
Salt fog, 5 weight percent low In condition H 950, rusting resistance is said to be similar to Type 304 in salt fog.2
Strongly oxidizing and reducing acids, and atmospheric exposure low General corrosion resistance approaches Type 304, and is greatest in the fully hardened condition.3
Air, passive film of chromium oxide low Stainless steels in general resist corrosion through a chromium oxide film; the rule is not specific to this grade.4
Surfaces with scale or foreign particles not rated Scale and foreign particles reduce corrosion resistance, so finished parts should be passivated.5
Corrosion details
#EnvironmentDetailsTest conditions
1 Marine atmosphere, strip tested at the Kure Beach site Quoted from the datasheet: 'Numerous tests representing a marine environment have shown the alloy to have a high level of resistance to stress-corrosion cracking.' The datasheet's table of results is titled 'Typical Stress-Corrosion-Cracking Resistance in an Atmospheric Marine Environment'. Its individual values were not transcribed, because the extracted table text was not reliable. specimen stripsite 80-ft lot, Kure Beach (as printed)basis qualitative statement and table title
2 Salt fog, 5 weight percent Quoted: 'rusting resistance similar to that of Type 304 Stainless in 5 weight percent salt fog', for condition H 950. condition H 950test 5 weight percent salt fog
3 Strongly oxidizing and reducing acids, and atmospheric exposure Quoted: 'the general-corrosion resistance of PH 13-8 Mo stainless approaches that of Type 304' under strongly oxidizing and reducing acids and atmospheric exposures. The same section says the alloy's general-corrosion resistance is 'greatest in the fully hardened condition'. exposure strongly oxidizing and reducing acids and atmospheric exposures
4 Air, passive film of chromium oxide Wikipedia says stainless steel's resistance to corrosion comes from its chromium content of 10.5% or more, which forms a passive film of chromium oxide that blocks oxygen from reaching the steel. The article is a general account of stainless steels and does not give a value for this grade. basis general account of stainless steels
5 Surfaces with scale or foreign particles Quoted: 'For optimum corrosion resistance, surfaces must be free of scale and foreign particles and finished parts should be passivated.' The datasheet gives no rate for an unclean surface. basis qualitative statement

Risks and side effects

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

For people

No safety data sheet for this alloy was read. The hazard codes in PubChem are for nickel as an element.

The alloy
The PubChem nickel record gives H317 (may cause an allergic skin reaction), H351 (suspected of causing cancer) and H372 (damage to organs with repeated exposure), with the signal word Danger.
Welding and surfaces
The datasheet suggests E/ER308L filler where high weld strength is not needed, and asks that finished parts be passivated.

If it fails

The failure routes in the sources are stress-corrosion cracking of under-aged parts and lower impact toughness in condition H 950.

Under-aged parts
The datasheet suggests a minimum ageing temperature of 1000°F (538°C) for best resistance to stress-corrosion cracking. It gives no failure rate for under-aged parts.
Toughness
Typical Charpy V-notch energy is 27 J in condition H 950 and 41 J in condition H 1000, so the higher-strength condition is the less tough one.

Handling and storage

Surfaces
Keep surfaces free of scale and foreign particles, and passivate finished parts (HiTemp Metals datasheet).
Condition
Specify the condition (H 950, H 1000 or H 1050) on every order, because strength and toughness change with it.

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

Failure risks

Failure risks
FailureTrigger and consequence
Stress-corrosion cracking of under-aged partsmoderate severityAgeing below 1000°F (538°C), which the datasheet says is the minimum for best resistance to stress-corrosion crackingThe datasheet suggests a minimum ageing temperature of 1000°F (538°C) for best resistance to stress-corrosion cracking. It gives no failure rate for under-aged parts.
Lower impact toughness in the H 950 conditionlow severityChoosing condition H 950 over H 1000 where impact energy mattersTypical Charpy V-notch energy is 27 J in condition H 950 against 41 J in condition H 1000 (datasheet). Yield strength in H 950 is also higher, so the choice is a trade-off.
Welded joints in marine servicelow severityWelding without a suitable filler or aged conditionThe datasheet suggests a standard austenitic filler such as E/ER308L where high weld strength is not needed. It does not report weld performance in marine tests in the text it gives.

Side effects on surrounding parts

Side effects on surrounding parts
AffectsEffect
Use near magnetometers or other magnetic sensorsThe datasheet prints magnetic permeability for condition H 950 of 52 at 10.5 Oe, rising to 127 at 54.7 Oe, so the alloy is magnetic in this condition.

Handling and storage

  • Passivate finished parts and keep their surfaces free of scale and foreign particles (datasheet).
  • Age at a minimum of 1000°F (538°C) for the best stress-corrosion resistance (datasheet).
  • Where high weld strength is not needed, use a standard austenitic filler such as E/ER308L (datasheet).

Supply and geography

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

Nickel (mine production)

Top producers (2025)
Indonesia 66.7%, Philippines 6.9%, Russia 5.1%, Canada 3.6%, New Caledonia 3.6%
Recycling
USGS: most secondary nickel was in the form of nickel content of stainless-steel scrap, and nickel recovered from scrap accounted for approximately 60% of apparent consumption in 2025.
Substitutes
USGS: low-nickel, duplex, or ultrahigh-chromium stainless steels have been substituted for austenitic grades in construction.

Chromium (mine production, chromite ore)

Top producers (2025)
South Africa 45.1%, Turkey 17.6%, Kazakhstan 13.7%, India 5.9%, Zimbabwe 3.9%

Molybdenum (mine production)

Top producers (2025)
China 37.3%, Chile 16.2%, United States 15.4%, Peru 15%, Mexico 6.5%

Updated