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.
Evidence level
2 of 5
Lab-measured
- 0Predicted only. No one has made it, or no measurement exists.
- 1Calculated. Only calculated or predicted values from sources.
- 2Lab-measured. Measured properties with their conditions stated.
- 3Space-relevant tests. Measured in conditions relevant to space, such as vacuum or atomic oxygen.
- 4Ground-qualified. Qualified for an application on the ground.
- 5Flown or field-proven. Flight or field results exist.
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
| Property | Value | Basis |
|---|---|---|
| Density | 7.76 g/cm³ | 1 sourced value |
| Yield strength | 1,138 to 1,449 MPa | 5 sourced values across conditions |
| Tensile strength | 1,207 to 1,551 MPa | 5 sourced values across conditions |
| Thermal conductivity | 12.8 W/(m·K) | 1 sourced value |
| Thermal expansion (CTE) | 13 ppm/K | 2 sourced values across conditions |
| Melting point | 1,404 °C | 1 sourced value |
| Electrical resistivity | 1,020 microhm-mm | 1 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.
| Ingredient | Share of the weight | What 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.
| Measurement | PH 13-8Mo | 304 (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) | 302 | 304L (UNS S30403) | 309 | 310S (UNS S31008, EN 1.4845) | 317L | 321 | 347 | 347H | 904L (UNS N08904, EN 1.4539) | Nitronic 60 | 2101 | 430F (UNS S43020) | 410S (UNS S41008) | 416 | 420 | 431 (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 J18 | no data | no data | no data | > 27 J | no data | 20 J | no data | no data | no data | 70 J | no data | no data | > 40 J | no data | no data | no data | no data | no data | no data | 65 to 100 ft-lbf | no data | no data | no data | no data | 187.8 J | no data | no data | no data | no data | no data | no data | > 90 J | no data | no data |
| Charpy V-notch impact energy, H 950, typical longitudinal (HiTemp Metals datasheet) | 27 J19 | no data | no data | no data | > 27 J | no data | 20 J | no data | no data | no data | 70 J | no data | no data | > 40 J | no data | no data | no data | no data | no data | no data | 65 to 100 ft-lbf | no data | no data | no data | no data | 187.8 J | no data | no data | no data | no data | no data | no data | > 90 J | no data | no data |
| Thermal behavior and safety | |||||||||||||||||||||||||||||||||||
| Melting point, PH 13-8 Mo (Bibus datasheet)Single value printed in a supplier datasheet | 1404 °C | 1673 K | 1390 °C | 1390 °C | 2525 to 2625 °F | no data | 1404 °C | 2500 to 2700 °F | 1482 to 1532 °C | 1425 to 1510 °C | no data | 1399 to 1421 °C | 1455 °C | no data | no data | no data | 1420 °C | 1399 to 1421 °C | 2550 to 2650 °F | 1410 °C | 1390 to 1440 °C | 1398 to 1446 °C | 1398 to 1446 °C | 2550 to 2635 degF | 1300 to 1390 °C | no data | 2525 to 2630 °F | 1482 °C | 1480 to 1530 °C | 2714 °F | 2650 to 2750 °F | no data | no data | 1404 to 1440 °C | no data |
| Thermal conductivity at 20 °C, PH 13-8 Mo (Bibus datasheet)Value printed in a supplier datasheet | 12.8 W/m - °C | 14 W/m.K | 14.6 W/m.K | 14.6 W/m·K | 14 W/(m °C) | 14 W/m.K | 17.9 W/m.K | 24.2 W/m.K | 24.9 W/m-K | 23.86 W/m.K | 25 W/(m K) | 16.3 W/m.K | 15 W/m°C | 13 W/m.K | 25.8 W/m.K | 21.4 W/m.K | 16.2 W/(m·K) | 16.3 W/m·K | 15.6 W/m·K | 13 W/(m·K) | 14 W/(m·K) | 16.3 W/(m·K) | 16.3 W/(m·K) | 14 W/m.°C | 12 W/(m·K) | 9 Btu/ft hr °F | 16 W/(m·K) | 26.1 W/m.K | 26.9 W/m-K | 30 W/m K | 24.9 W/(m·K) | 25 W/(m·K) | 15 W/m K | 16.9 W/(m·K) | 16.2 W/m-K |
| Thermal conductivity at 100 °C, condition A (HiTemp Metals datasheet)Value printed in a supplier datasheet | 14 W/m-K1 | 14 W/m.K | 14.6 W/m.K | 14.6 W/m·K | 14 W/(m °C) | 14 W/m.K | 17.9 W/m.K | 24.2 W/m.K | 24.9 W/m-K | 23.86 W/m.K | 25 W/(m K) | 16.3 W/m.K | 15 W/m°C | 13 W/m.K | 25.8 W/m.K | 21.4 W/m.K | 16.2 W/(m·K) | 16.3 W/m·K | 15.6 W/m·K | 13 W/(m·K) | 14 W/(m·K) | 16.3 W/(m·K) | 16.3 W/(m·K) | 14 W/m.°C | 12 W/(m·K) | 9 Btu/ft hr °F | 16 W/(m·K) | 26.1 W/m.K | 26.9 W/m-K | 30 W/m K | 24.9 W/(m·K) | 25 W/(m·K) | 15 W/m K | 16.9 W/(m·K) | 16.2 W/m-K |
| Physical and electrical | |||||||||||||||||||||||||||||||||||
| Density, PH 13-8 Mo (Bibus datasheet)Value printed in a supplier datasheet | 7.76 g/cm³ | 7.85 Mg/m3 | 8.027 g/cm³ | 8.03 g/cm³ | 7.82 g/cm³ | 7.8 g/cm³ | 7.75 g/cm³ | 0.275 lb/in3 | 7.73 g/cm³ | 7.7 g/cm³ | 7.61 to 8.1 kg/dm3 | 8.03 g/cm³ | 7.9 kg/dm3 | 7.8 g/cm³ | 7.75 g/cm³ | 7.75 g/cm³ | 7.9 g/cm³ | 7.9 g/cm³ | 8.03 g/cm³ | 7.8 kg/dm3 | 8.027 g/cm³ | 7.92 g/cm³ | 7.96 g/cm³ | 7.98 kg/dm3 | 7.95 g/cm³ | 7.622 gm/cm³ | 7800 kg/m3 | 7700 kg/m3 | 7.73 g/cm³ | 7.7 kg/dm3 | 7.75 g/cm³ | 7800 kg/m3 | 7.7 kg/dm3 | 7.81 g/cm³ | 7.8 g/cm³ |
| Electrical resistivity, condition A (HiTemp Metals datasheet) | 1020 microhm-mm4 | 65 10-8 ohm.m | 69 10-8 ohm.m | 74 μΩ·cm | 0.74 10-6 ohm.m | 0.83 μΩm | 98 microhm-cm | 0.6 10-6 ohm.m | 57 µohm-cm | 60 micro-ohm-cm | no data | 72 µΩ·cm | 72 microhm-cm | no data | 60 micro-ohm-cm | 800 µΩ.mm | 72 µΩ·cm | 72 microhm-cm | 78 µΩ·cm | 0.86 Ω·mm²/m | 475 Ohm-circ mil/ft | 72 microhm·cm | 72 µΩ·cm | no data | 95.2 µΩ·cm | 98.2 microhm-cm | no data | 600 nΩ.m | 60 µohm-cm | 0.6 Ω mm2/m | 0.55 µΩ·m | 0.7 ohm mm2/m | no data | 80 µΩ·cm | 82 microhm-cm |
| Hardness, Rockwell C, H 1000, typical longitudinal (HiTemp Metals datasheet) | 45 HRC17 | no data | no data | no data | no data | no data | 36 HRC | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | 26 to 32 RC | 48 HRC | no data | no data | no data | no data |
| Other measurements | |||||||||||||||||||||||||||||||||||
| Mean coefficient of thermal expansion, 20 to 100 °C (Bibus datasheet) | 13 μm/m - °C2 | no data | 16.5 10-6/K | 16.5 10-6 cm/cm/°C | 13 10-6/K | 13.5 10-6/K | 11.3 10-6/°C | 10.1 10-6/K | 9.9 µm/m-°C | 10.3 10-6/K | no data | 16.6 10-6/K | 16 10-6/°C | 13 10-6/K | 10.5 10-6/°C | 10.3 10-6/°C | 16.6 µm/(m·°C) | 16.6 10-6 cm/cm/°C | 15.6 µm/(m·K) | 16.5 ppm/K | 16.5 10^-6 cm/cm/°C | 16.6 ppm/K | 16.6 ppm/K | 9.2 in/in.degF x 10^-6 | 15.8 ppm/K | 15.8 µm/m/°C | 13 µm/m/°C | 10.4 um/m/C | 10.8 µm/m·K | 10.5 10^-6/K | 10.3 10^-6/K | 10 ppm/K | 10.8 10-6 K-1 | 17.3 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 datasheet | 10.8 10⁻⁶/K3 | no data | 16.5 10-6/K | 16.5 10-6 cm/cm/°C | 13 10-6/K | 13.5 10-6/K | 11.3 10-6/°C | 10.1 10-6/K | 9.9 µm/m-°C | 10.3 10-6/K | no data | 16.6 10-6/K | 16 10-6/°C | 13 10-6/K | 10.5 10-6/°C | 10.3 10-6/°C | 16.6 µm/(m·°C) | 16.6 10-6 cm/cm/°C | 15.6 µm/(m·K) | 16.5 ppm/K | 16.5 10^-6 cm/cm/°C | 16.6 ppm/K | 16.6 ppm/K | 9.2 in/in.degF x 10^-6 | 15.8 ppm/K | 15.8 µm/m/°C | 13 µm/m/°C | 10.4 um/m/C | 10.8 µm/m·K | 10.5 10^-6/K | 10.3 10^-6/K | 10 ppm/K | 10.8 10-6 K-1 | 17.3 µm/(m·°C) | 14.4 10^-6/C |
| Yield strength 0.2 % offset, H 950, typical longitudinal (HiTemp Metals datasheet) | 1449 MPa5 | > 205 MPa | 205 MPa | 170 MPa | > 450 MPa | > 550 MPa | 1262 MPa | 1896 MPa | 205 to 290 MPa | > 30 ksi | > 520 MPa | 205 MPa | > 172 MPa | > 400 MPa | > 170 MPa | 345 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa | > 450 MPa | 379 MPa | > 30 ksi | > 450 MPa | 51.5 ksi | 600 MPa | > 550 MPa | 310 MPa | 380 MPa |
| Yield strength, H 950, minimum (Bibus datasheet) | 1413 MPa6 | > 205 MPa | 205 MPa | 170 MPa | > 450 MPa | > 550 MPa | 1262 MPa | 1896 MPa | 205 to 290 MPa | > 30 ksi | > 520 MPa | 205 MPa | > 172 MPa | > 400 MPa | > 170 MPa | 345 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa | > 450 MPa | 379 MPa | > 30 ksi | > 450 MPa | 51.5 ksi | 600 MPa | > 550 MPa | 310 MPa | 380 MPa |
| Yield strength 0.2 % offset, H 1000, typical longitudinal (HiTemp Metals datasheet)Typical value printed in a supplier datasheet | 1413 MPa7 | > 205 MPa | 205 MPa | 170 MPa | > 450 MPa | > 550 MPa | 1262 MPa | 1896 MPa | 205 to 290 MPa | > 30 ksi | > 520 MPa | 205 MPa | > 172 MPa | > 400 MPa | > 170 MPa | 345 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa | > 450 MPa | 379 MPa | > 30 ksi | > 450 MPa | 51.5 ksi | 600 MPa | > 550 MPa | 310 MPa | 380 MPa |
| Yield strength, H 1000, minimum (Bibus datasheet) | 1310 MPa8 | > 205 MPa | 205 MPa | 170 MPa | > 450 MPa | > 550 MPa | 1262 MPa | 1896 MPa | 205 to 290 MPa | > 30 ksi | > 520 MPa | 205 MPa | > 172 MPa | > 400 MPa | > 170 MPa | 345 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa | > 450 MPa | 379 MPa | > 30 ksi | > 450 MPa | 51.5 ksi | 600 MPa | > 550 MPa | 310 MPa | 380 MPa |
| Yield strength, H 1050, minimum (Bibus datasheet) | 1138 MPa9 | > 205 MPa | 205 MPa | 170 MPa | > 450 MPa | > 550 MPa | 1262 MPa | 1896 MPa | 205 to 290 MPa | > 30 ksi | > 520 MPa | 205 MPa | > 172 MPa | > 400 MPa | > 170 MPa | 345 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa | > 450 MPa | 379 MPa | > 30 ksi | > 450 MPa | 51.5 ksi | 600 MPa | > 550 MPa | 310 MPa | 380 MPa |
| Tensile strength, H 950, typical longitudinal (HiTemp Metals datasheet)Typical value printed in a supplier datasheet | 1551 MPa10 | > 515 MPa | 515 MPa | 485 MPa | > 655 MPa | 800 to 1000 MPa | 1365 MPa | 1965 MPa | 450 to 510 MPa | > 65 ksi | < 1100 MPa | 515 MPa | > 517 MPa | > 600 MPa | > 380 MPa | 517 MPa | 655 MPa | > 485 MPa | 621 MPa | 610 MPa | > 515 MPa | > 515 MPa | > 515 MPa | > 75 ksi | 530 to 730 MPa | > 655 MPa | > 650 MPa | 552 MPa | > 60 ksi | 650 to 850 N/mm2 | 85.8 ksi | 862 MPa | 760 to 960 MPa | 827 MPa | 860 MPa |
| Tensile strength, H 950, minimum (Bibus datasheet) | 1517 MPa11 | > 515 MPa | 515 MPa | 485 MPa | > 655 MPa | 800 to 1000 MPa | 1365 MPa | 1965 MPa | 450 to 510 MPa | > 65 ksi | < 1100 MPa | 515 MPa | > 517 MPa | > 600 MPa | > 380 MPa | 517 MPa | 655 MPa | > 485 MPa | 621 MPa | 610 MPa | > 515 MPa | > 515 MPa | > 515 MPa | > 75 ksi | 530 to 730 MPa | > 655 MPa | > 650 MPa | 552 MPa | > 60 ksi | 650 to 850 N/mm2 | 85.8 ksi | 862 MPa | 760 to 960 MPa | 827 MPa | 860 MPa |
| Tensile strength, H 1000, typical longitudinal (HiTemp Metals datasheet)Typical value printed in a supplier datasheet | 1482 MPa12 | > 515 MPa | 515 MPa | 485 MPa | > 655 MPa | 800 to 1000 MPa | 1365 MPa | 1965 MPa | 450 to 510 MPa | > 65 ksi | < 1100 MPa | 515 MPa | > 517 MPa | > 600 MPa | > 380 MPa | 517 MPa | 655 MPa | > 485 MPa | 621 MPa | 610 MPa | > 515 MPa | > 515 MPa | > 515 MPa | > 75 ksi | 530 to 730 MPa | > 655 MPa | > 650 MPa | 552 MPa | > 60 ksi | 650 to 850 N/mm2 | 85.8 ksi | 862 MPa | 760 to 960 MPa | 827 MPa | 860 MPa |
| Tensile strength, H 1000, minimum (Bibus datasheet) | 1413 MPa13 | > 515 MPa | 515 MPa | 485 MPa | > 655 MPa | 800 to 1000 MPa | 1365 MPa | 1965 MPa | 450 to 510 MPa | > 65 ksi | < 1100 MPa | 515 MPa | > 517 MPa | > 600 MPa | > 380 MPa | 517 MPa | 655 MPa | > 485 MPa | 621 MPa | 610 MPa | > 515 MPa | > 515 MPa | > 515 MPa | > 75 ksi | 530 to 730 MPa | > 655 MPa | > 650 MPa | 552 MPa | > 60 ksi | 650 to 850 N/mm2 | 85.8 ksi | 862 MPa | 760 to 960 MPa | 827 MPa | 860 MPa |
| Tensile strength, H 1050, minimum (Bibus datasheet) | 1207 MPa14 | > 515 MPa | 515 MPa | 485 MPa | > 655 MPa | 800 to 1000 MPa | 1365 MPa | 1965 MPa | 450 to 510 MPa | > 65 ksi | < 1100 MPa | 515 MPa | > 517 MPa | > 600 MPa | > 380 MPa | 517 MPa | 655 MPa | > 485 MPa | 621 MPa | 610 MPa | > 515 MPa | > 515 MPa | > 515 MPa | > 75 ksi | 530 to 730 MPa | > 655 MPa | > 650 MPa | 552 MPa | > 60 ksi | 650 to 850 N/mm2 | 85.8 ksi | 862 MPa | 760 to 960 MPa | 827 MPa | 860 MPa |
| Elongation in 2 in., H 1000, typical longitudinal (HiTemp Metals datasheet)Typical value printed in a supplier datasheet | 13 %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.
| System | Codes |
|---|---|
| UNS | S13800 |
| EN | 1.4534 |
| AMS | 5629 |
| Trade name | PH 13-8 Mo |
Notes
The method, full conditions and any caveat for the numbered rows above.
| # | Measurement | Method | Conditions | Caveat |
|---|---|---|---|---|
| 1 | Thermal conductivity at 100 °C, condition A (HiTemp Metals datasheet) | — | temperature 100 °C (212 °F)condition printed Condition Aunit in source W/m-K | — |
| 2 | Mean 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 | — |
| 3 | Mean 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 | — |
| 4 | Electrical 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 | — |
| 5 | Yield 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 minimum | condition H 950form typical longitudinal, center or intermediate locationtemperature room temperaturebasis typical | — |
| 6 | Yield strength, H 950, minimum (Bibus datasheet) | Minimum value printed under the heading Typical mechanical properties (room temperature) | condition H950basis minimum, room temperature | — |
| 7 | Yield strength 0.2 % offset, H 1000, typical longitudinal (HiTemp Metals datasheet) | — | condition H 1000form typical longitudinal, center or intermediate locationtemperature room temperaturebasis typical | — |
| 8 | Yield strength, H 1000, minimum (Bibus datasheet) | Minimum value printed under the heading Typical mechanical properties (room temperature) | condition H1000basis minimum, room temperature | — |
| 9 | Yield strength, H 1050, minimum (Bibus datasheet) | Minimum value printed under the heading Typical mechanical properties (room temperature) | condition H1050basis minimum, room temperature | — |
| 10 | Tensile strength, H 950, typical longitudinal (HiTemp Metals datasheet) | — | condition H 950form typical longitudinal, center or intermediate locationtemperature room temperaturebasis typical | — |
| 11 | Tensile strength, H 950, minimum (Bibus datasheet) | Minimum value printed under the heading Typical mechanical properties (room temperature) | condition H950basis minimum, room temperature | — |
| 12 | Tensile strength, H 1000, typical longitudinal (HiTemp Metals datasheet) | — | condition H 1000form typical longitudinal, center or intermediate locationtemperature room temperaturebasis typical | — |
| 13 | Tensile strength, H 1000, minimum (Bibus datasheet) | Minimum value printed under the heading Typical mechanical properties (room temperature) | condition H1000basis minimum, room temperature | — |
| 14 | Tensile strength, H 1050, minimum (Bibus datasheet) | Minimum value printed under the heading Typical mechanical properties (room temperature) | condition H1050basis minimum, room temperature | — |
| 15 | Elongation in 2 in., H 1000, typical longitudinal (HiTemp Metals datasheet) | — | condition H 1000gauge length 2 in.form typical longitudinalbasis typical | — |
| 16 | Elongation, H 1000, minimum (Bibus datasheet) | Minimum value printed under the heading Typical mechanical properties (room temperature) | condition H1000basis minimum, room temperature | — |
| 17 | Hardness, 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 | — |
| 18 | Charpy 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 | — |
| 19 | Charpy 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.
| Environment | Concern | What 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 |
| # | Environment | Details | Test 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 | Trigger and consequence |
|---|---|
| Stress-corrosion cracking of under-aged partsmoderate severity | Ageing 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 severity | Choosing 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 severity | Welding 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
| Affects | Effect |
|---|---|
| Use near magnetometers or other magnetic sensors | The 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%
Documents
Datasheets, safety data sheets, papers and standards you can open.
| Document | Type | Year |
|---|---|---|
| PH 13-8 Mo technical data, HiTemp Metals | datasheet | |
| PH 13-8 Mo | 1.4534 technical data, Bibus Metals | datasheet | |
| USGS Mineral Commodity Summaries 2026: Nickel | report | 2026 |
| USGS Mineral Commodity Summaries 2026: Chromium | report | 2026 |
| USGS Mineral Commodity Summaries 2026: Molybdenum | report | 2026 |
| PubChem compound record: Nickel (CID 935), GHS classification | database | |
| Wikipedia: Stainless steel | database | |
| Wikipedia: Precipitation hardening | database |
Full record
The complete spore, as stored. Free to reuse under CC-BY-4.0. Images keep the licence shown with each one.
Show the full YAML
spore: profile
id: stainless-13-8mo
spore_version: 0.2
family: stainless-steels
name: PH 13-8Mo stainless steel
abbreviation: PH 13-8Mo
role: high-toughness precipitation-hardening stainless steel for aerospace fasteners, shafts and hardware
category: metals
type: steels-and-stainless
summary: |
PH 13-8 Mo (UNS S13800, EN 1.4534, AMS 5629) is a precipitation-hardening stainless steel. Its typical yield strength is 1449 MPa in condition H 950 (longitudinal, per the HiTemp Metals datasheet), and the Bibus datasheet gives a minimum of 1413 MPa for the same condition. Its marine stress-corrosion resistance is described as high, and its Charpy V-notch energy is 41 J in condition H 1000 and 27 J in condition H 950.
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
identity:
formula: 'Iron-based precipitation-hardening stainless steel: iron with chromium, nickel, molybdenum and aluminium as the main alloying elements (limits in the recipe parts)'
designations:
- system: UNS
code: S13800
source: bibus
where: Header line printed as 1.4534.9 | UNS S13800 | AMS 5629
- system: AMS
code: '5629'
source: bibus
where: Header line printed as 1.4534.9 | UNS S13800 | AMS 5629
- system: EN
code: '1.4534'
source: bibus
where: Header line printed as 1.4534.9, and page title PH 13-8 Mo | 1.4534
- system: Trade name
code: PH 13-8 Mo
source: hightempmetals
where: 'Page title and trademark note: PH 13-8 Mo stainless is a registered trademark of Armco Inc.'
source: bibus
where: 'Chemical composition limits in % from the Bibus table, with decimal commas written as points: Fe rest; Cr 12.25 to 13.25; Ni 7.50 to 8.50; Mo 2.00 to 2.50; Al 0.90 to 1.35; Mn max 0.20; N max 0.10; Si max 0.10; C max 0.05; P max 0.01. The HiTemp Metals type analysis differs for two elements: Mn max 0.10 and N max 0.01. Both are recorded here and the two sources disagree.'
tags:
environments: []
stresses: []
applications:
- structures
- mechanisms
properties:
- benchmark: density
label: Density, PH 13-8 Mo (Bibus datasheet)
value: 7.76
unit: g/cm3
scope: material
conditions:
condition: not stated on the page
unit_in_source: g/cm³
method: Value printed in a supplier datasheet
status: ground
source: bibus
where: Physical constants and thermal properties table, row Density
- benchmark: melting_point
label: Melting point, PH 13-8 Mo (Bibus datasheet)
value: 1404
unit: °C
scope: material
conditions:
note: single value printed, no range
method: Single value printed in a supplier datasheet
status: ground
source: bibus
where: Physical constants and thermal properties table, row Melting point
- benchmark: thermal_conductivity
label: Thermal conductivity at 20 °C, PH 13-8 Mo (Bibus datasheet)
value: 12.8
unit: W/m - °C
scope: material
conditions:
temperature: 20 °C
unit_in_source: W/m - °C
method: Value printed in a supplier datasheet
status: ground
source: bibus
where: Physical constants and thermal properties table, row Thermal conductivity at 20°C
- benchmark: thermal_conductivity
label: Thermal conductivity at 100 °C, condition A (HiTemp Metals datasheet)
value: 14
unit: W/m-K
scope: material
conditions:
temperature: 100 °C (212 °F)
condition_printed: Condition A
unit_in_source: W/m-K
method: Value printed in a supplier datasheet
status: ground
source: hightempmetals
where: Thermal Conductivity section, Condition A at 212°F / 100°C, printed as 97.2 Btu-in/ft²-h-°F (14.0 W/m-K)
- benchmark: cte
label: Mean coefficient of thermal expansion, 20 to 100 °C (Bibus datasheet)
value: 13
unit: μm/m - °C
scope: material
conditions:
temperature: 20 to 100 °C
unit_in_source: μm/m - °C
method: Value printed in a supplier datasheet; it differs from the HiTemp Metals value at a different temperature range (see gaps)
status: ground
source: bibus
where: Physical constants and thermal properties table, row Coefficient of expansion at 20-100°C
- benchmark: cte
label: Mean coefficient of thermal expansion, condition H 1000, 21 to 204 °C (HiTemp Metals datasheet)
value: 10.8
unit: 10⁻⁶/K
scope: material
conditions:
condition: H 1000
temperature: 21 to 204 °C (70 to 400 °F)
unit_in_source: 10⁻⁶/K
method: Value printed in a supplier datasheet
status: ground
source: hightempmetals
where: Mean Coefficient of Thermal Expansion table, row 70-400°F (21-204°C), column H 1000, second value of 6.0 / 10.8
- benchmark: electrical_resistivity
label: Electrical resistivity, condition A (HiTemp Metals datasheet)
value: 1020
unit: microhm-mm
scope: material
conditions:
temperature: 100 °C (212 °F)
condition_printed: Condition A
unit_in_source: microhm-mm
method: Value printed in a supplier datasheet; the same page also prints 613 ohms c/mf (not recorded here)
status: ground
source: hightempmetals
where: Electrical Resistivity section, Condition A at 212°F / 100°C, second line
- benchmark: yield_strength
label: Yield strength 0.2 % offset, H 950, typical longitudinal (HiTemp Metals datasheet)
value: 1449
unit: MPa
scope: material
conditions:
condition: H 950
form: typical longitudinal, center or intermediate location
temperature: room temperature
basis: typical
method: Typical value printed in a supplier datasheet; this is a typical value, not a minimum
status: ground
source: hightempmetals
where: Typical Longitudinal Room-Temperature Mechanical Properties table, row H 950, column 0.2% Yield (ksi / MPa), printed as 210 / 1449
- benchmark: yield_strength
label: Yield strength, H 950, minimum (Bibus datasheet)
value: 1413
unit: MPa
scope: material
conditions:
condition: H950
basis: minimum, room temperature
method: Minimum value printed under the heading Typical mechanical properties (room temperature)
status: ground
source: bibus
where: Typical mechanical properties table, row H950, column Yield strength, printed as min. 1413 MPa
- benchmark: yield_strength
label: Yield strength 0.2 % offset, H 1000, typical longitudinal (HiTemp Metals datasheet)
value: 1413
unit: MPa
scope: material
conditions:
condition: H 1000
form: typical longitudinal, center or intermediate location
temperature: room temperature
basis: typical
method: Typical value printed in a supplier datasheet
status: ground
source: hightempmetals
where: Typical Longitudinal Room-Temperature Mechanical Properties table, row H 1000, column 0.2% Yield (ksi / MPa), printed as 205 / 1413
- benchmark: yield_strength
label: Yield strength, H 1000, minimum (Bibus datasheet)
value: 1310
unit: MPa
scope: material
conditions:
condition: H1000
basis: minimum, room temperature
method: Minimum value printed under the heading Typical mechanical properties (room temperature)
status: ground
source: bibus
where: Typical mechanical properties table, row H1000, column Yield strength, printed as min. 1310 MPa
- benchmark: yield_strength
label: Yield strength, H 1050, minimum (Bibus datasheet)
value: 1138
unit: MPa
scope: material
conditions:
condition: H1050
basis: minimum, room temperature
method: Minimum value printed under the heading Typical mechanical properties (room temperature)
status: ground
source: bibus
where: Typical mechanical properties table, row H1050, column Yield strength, printed as min. 1138 MPa
- benchmark: ultimate_tensile_strength
label: Tensile strength, H 950, typical longitudinal (HiTemp Metals datasheet)
value: 1551
unit: MPa
scope: material
conditions:
condition: H 950
form: typical longitudinal, center or intermediate location
temperature: room temperature
basis: typical
method: Typical value printed in a supplier datasheet
status: ground
source: hightempmetals
where: Typical Longitudinal Room-Temperature Mechanical Properties table, row H 950, column UTS (ksi / MPa), printed as 225 / 1551
- benchmark: ultimate_tensile_strength
label: Tensile strength, H 950, minimum (Bibus datasheet)
value: 1517
unit: MPa
scope: material
conditions:
condition: H950
basis: minimum, room temperature
method: Minimum value printed under the heading Typical mechanical properties (room temperature)
status: ground
source: bibus
where: Typical mechanical properties table, row H950, column Tensile strength, printed as min. 1517 MPa
- benchmark: ultimate_tensile_strength
label: Tensile strength, H 1000, typical longitudinal (HiTemp Metals datasheet)
value: 1482
unit: MPa
scope: material
conditions:
condition: H 1000
form: typical longitudinal, center or intermediate location
temperature: room temperature
basis: typical
method: Typical value printed in a supplier datasheet
status: ground
source: hightempmetals
where: Typical Longitudinal Room-Temperature Mechanical Properties table, row H 1000, column UTS (ksi / MPa), printed as 215 / 1482
- benchmark: ultimate_tensile_strength
label: Tensile strength, H 1000, minimum (Bibus datasheet)
value: 1413
unit: MPa
scope: material
conditions:
condition: H1000
basis: minimum, room temperature
method: Minimum value printed under the heading Typical mechanical properties (room temperature)
status: ground
source: bibus
where: Typical mechanical properties table, row H1000, column Tensile strength, printed as min. 1413 MPa
- benchmark: ultimate_tensile_strength
label: Tensile strength, H 1050, minimum (Bibus datasheet)
value: 1207
unit: MPa
scope: material
conditions:
condition: H1050
basis: minimum, room temperature
method: Minimum value printed under the heading Typical mechanical properties (room temperature)
status: ground
source: bibus
where: Typical mechanical properties table, row H1050, column Tensile strength, printed as min. 1207 MPa
- benchmark: elongation
label: Elongation in 2 in., H 1000, typical longitudinal (HiTemp Metals datasheet)
value: 13
unit: '%'
scope: material
conditions:
condition: H 1000
gauge_length: 2 in.
form: typical longitudinal
basis: typical
method: Typical value printed in a supplier datasheet
status: ground
source: hightempmetals
where: Typical Longitudinal Room-Temperature Mechanical Properties table, row H 1000, column Elong. in 2" (%)
- benchmark: elongation
label: Elongation, H 1000, minimum (Bibus datasheet)
value: 10
unit: '%'
scope: material
conditions:
condition: H1000
basis: minimum, room temperature
method: Minimum value printed under the heading Typical mechanical properties (room temperature)
status: ground
source: bibus
where: Typical mechanical properties table, row H1000, column Elongation, printed as min. 10 %
- benchmark: hardness_rockwell_c
label: Hardness, Rockwell C, H 1000, typical longitudinal (HiTemp Metals datasheet)
value: 45
unit: HRC
scope: material
conditions:
condition: H 1000
form: typical longitudinal
basis: typical
method: Typical value printed in a supplier datasheet; benchmark name is not in the canonical list (see gaps)
status: ground
source: hightempmetals
where: Typical Longitudinal Room-Temperature Mechanical Properties table, row H 1000, column Rockwell C
- benchmark: charpy_impact_energy
label: Charpy V-notch impact energy, H 1000, typical longitudinal (HiTemp Metals datasheet)
value: 41
unit: J
scope: material
conditions:
condition: H 1000
form: typical longitudinal
basis: typical
test: Charpy V-notch
unit_in_source: ft-lb / J
method: Typical value printed in a supplier datasheet; benchmark name is not in the canonical list (see gaps)
status: ground
source: hightempmetals
where: Typical Longitudinal Room-Temperature Mechanical Properties table, row H 1000, column Charpy V-Notch (ft-lb / J), printed as 30 / 41
- benchmark: charpy_impact_energy
label: Charpy V-notch impact energy, H 950, typical longitudinal (HiTemp Metals datasheet)
value: 27
unit: J
scope: material
conditions:
condition: H 950
form: typical longitudinal
basis: typical
test: Charpy V-notch
unit_in_source: ft-lb / J
method: Typical value printed in a supplier datasheet; benchmark name is not in the canonical list (see gaps)
status: ground
source: hightempmetals
where: Typical Longitudinal Room-Temperature Mechanical Properties table, row H 950, column Charpy V-Notch (ft-lb / J), printed as 20 / 27
corrosion:
- environment: Marine atmosphere, strip tested at the Kure Beach site
headline: The datasheet reports a high level of resistance to stress-corrosion cracking in marine tests.
effect: '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.'
rating: low
conditions:
specimen: strip
site: 80-ft lot, Kure Beach (as printed)
basis: qualitative statement and table title
source: hightempmetals
where: Corrosion Resistance section and the Stress-Corrosion-Cracking Table title
- environment: Salt fog, 5 weight percent
headline: In condition H 950, rusting resistance is said to be similar to Type 304 in salt fog.
effect: 'Quoted: ''rusting resistance similar to that of Type 304 Stainless in 5 weight percent salt fog'', for condition H 950.'
rating: low
conditions:
condition: H 950
test: 5 weight percent salt fog
source: hightempmetals
where: Corrosion Resistance section, first bullet
- environment: Strongly oxidizing and reducing acids, and atmospheric exposure
headline: General corrosion resistance approaches Type 304, and is greatest in the fully hardened condition.
effect: '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''.'
rating: low
conditions:
exposure: strongly oxidizing and reducing acids and atmospheric exposures
source: hightempmetals
where: Corrosion Resistance section, general-corrosion bullets
- environment: Air, passive film of chromium oxide
headline: Stainless steels in general resist corrosion through a chromium oxide film; the rule is not specific to this grade.
effect: 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.
rating: low
conditions:
basis: general account of stainless steels
source: wikipedia-stainless
where: Opening section of the Stainless steel article
- environment: Surfaces with scale or foreign particles
headline: Scale and foreign particles reduce corrosion resistance, so finished parts should be passivated.
effect: '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.'
rating: unknown
conditions:
basis: qualitative statement
source: hightempmetals
where: Corrosion Resistance section, last bullet
risks:
hazards:
- text: PubChem's record for nickel (CID 935) gives the GHS hazard statements H317 (may cause an allergic skin reaction), H351 (suspected of causing cancer), H372 (causes damage to organs through prolonged or repeated exposure) and H412 (harmful to aquatic life with long lasting effects) in its first notifier entries, with the signal word Danger and the pictograms GHS07 and GHS08. These codes are for nickel as an element, because no safety data sheet for PH 13-8 Mo was read.
ghs:
- H317
- H351
- H372
- H412
source: pubchem-nickel
where: GHS Classification section, first notifier entries (signal word, pictograms and hazard statements)
failure_risks:
- mode: Stress-corrosion cracking of under-aged parts
trigger: Ageing below 1000°F (538°C), which the datasheet says is the minimum for best resistance to stress-corrosion cracking
consequence: 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.
severity: moderate
source: hightempmetals
where: Corrosion Resistance section, aging recommendation
- mode: Lower impact toughness in the H 950 condition
trigger: Choosing condition H 950 over H 1000 where impact energy matters
consequence: Typical 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.
severity: low
source: hightempmetals
where: Typical Longitudinal Room-Temperature Mechanical Properties table, rows H 950 and H 1000
- mode: Welded joints in marine service
trigger: Welding without a suitable filler or aged condition
consequence: The 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.
severity: low
source: hightempmetals
where: Applications and Uses text, welding filler paragraph
side_effects:
- text: The 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.
affects: Use near magnetometers or other magnetic sensors
source: hightempmetals
where: Other Printed Values section, magnetic permeability
handling:
- text: Passivate finished parts and keep their surfaces free of scale and foreign particles (datasheet).
source: hightempmetals
where: Corrosion Resistance section, last bullet
- text: Age at a minimum of 1000°F (538°C) for the best stress-corrosion resistance (datasheet).
source: hightempmetals
where: Corrosion Resistance section, aging recommendation
- text: Where high weld strength is not needed, use a standard austenitic filler such as E/ER308L (datasheet).
source: hightempmetals
where: Applications and Uses text, welding filler paragraph
mitigations: []
uses:
- application: mechanisms
device: Valve parts, fittings and shafts
example: The datasheet says the alloy has been used for valve parts, fittings, cold-headed and machined fasteners, and shafts.
source: hightempmetals
where: Applications and Uses text
- application: structures
device: Aircraft components, nuclear reactor components and petrochemical parts
example: The datasheet lists aircraft components, nuclear reactor components and petrochemical applications, and says the alloy should be considered where high strength, toughness and corrosion resistance are needed.
source: hightempmetals
where: Applications and Uses text
supply:
- subject: Nickel (mine production)
producers:
- country: Indonesia
share_percent: 66.7
year: 2025
- country: Philippines
share_percent: 6.9
year: 2025
- country: Russia
share_percent: 5.1
year: 2025
- country: Canada
share_percent: 3.6
year: 2025
- country: New Caledonia
share_percent: 3.6
year: 2025
critical_lists: []
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.'
source: usgs-nickel-2026
where: World Mine Production and Reserves table, 2025e world total 3,900,000 (metric tons, nickel content); country shares calculated by Space Mushroom from the printed 2025e values; Recycling; Substitutes; Domestic Production and Use (stainless and alloy steel typically more than 85% of domestic consumption).
- subject: Chromium (mine production, chromite ore)
producers:
- country: South Africa
share_percent: 45.1
year: 2025
- country: Turkey
share_percent: 17.6
year: 2025
- country: Kazakhstan
share_percent: 13.7
year: 2025
- country: India
share_percent: 5.9
year: 2025
- country: Zimbabwe
share_percent: 3.9
year: 2025
critical_lists: []
substitutes: []
source: usgs-chromium-2026
where: World Mine Production and Reserves table, 2025e world total 51,000 (gross weight, metric tons); shares calculated by Space Mushroom from South Africa 23,000, Turkey 9,000, Kazakhstan 7,000, India 3,000 and Zimbabwe 2,000. The text read here prints no critical-mineral list entry.
- subject: Molybdenum (mine production)
producers:
- country: China
share_percent: 37.3
year: 2025
- country: Chile
share_percent: 16.2
year: 2025
- country: United States
share_percent: 15.4
year: 2025
- country: Peru
share_percent: 15
year: 2025
- country: Mexico
share_percent: 6.5
year: 2025
critical_lists: []
substitutes: []
source: usgs-molybdenum-2026
where: 'World Mine Production and Reserves table, 2025e world total 260,000 (metric tons); shares calculated by Space Mushroom from the printed 2025e values. Events text: ''China, Chile, the United States, Peru, and Mexico, in descending order of production, accounting for 90% of total global production''.'
documents:
- title: PH 13-8 Mo technical data, HiTemp Metals
type: datasheet
url: https://www.hightempmetals.com/techdata/hitemp13-8MOdata.php
- title: PH 13-8 Mo | 1.4534 technical data, Bibus Metals
type: datasheet
url: https://sd-metals.bibus.com/de-en/materials/itm/PH-13-8-Mo-1-4534/
- title: 'USGS Mineral Commodity Summaries 2026: Nickel'
type: report
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-nickel.pdf
year: 2026
- title: 'USGS Mineral Commodity Summaries 2026: Chromium'
type: report
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-chromium.pdf
year: 2026
- title: 'USGS Mineral Commodity Summaries 2026: Molybdenum'
type: report
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-molybdenum.pdf
year: 2026
- title: 'PubChem compound record: Nickel (CID 935), GHS classification'
type: database
url: https://pubchem.ncbi.nlm.nih.gov/compound/Nickel
- title: 'Wikipedia: Stainless steel'
type: database
url: https://en.wikipedia.org/wiki/Stainless_steel
- title: 'Wikipedia: Precipitation hardening'
type: database
url: https://en.wikipedia.org/wiki/Precipitation_hardening
gaps:
- No EN steel name (the X5CrNiMo-style name) is printed on the Bibus page or the HiTemp Metals page, so no EN name is recorded; the EN number 1.4534 is recorded from the Bibus header.
- Modulus of elasticity and modulus of rigidity are printed only in exponent form (28.3 x 10³ ksi and 195 x 10³ MPa on the HiTemp Metals page), so they are left out.
- Specific heat, a melting range and fracture toughness are not printed on either datasheet that was read.
- 'The two datasheets differ on the coefficient of thermal expansion: 13 μm/m - °C at 20 to 100 °C (Bibus) and 10.8 10⁻⁶/K at 21 to 204 °C in condition H 1000 (HiTemp Metals). Both are recorded; neither is treated as the corrected value.'
- The two datasheets differ on the composition maxima for manganese (0.20 Bibus, 0.10 HiTemp Metals) and nitrogen (0.10 Bibus, 0.01 HiTemp Metals). Both are recorded in identity.where.
- Typical values (HiTemp Metals, longitudinal) and minimum values (Bibus) are on different bases. Both are recorded, side by side, under their own conditions.
- The HiTemp Metals stress-corrosion table could not be transcribed reliably from the extracted text, so its individual results (applied stresses and days to failure) are not recorded; only the qualitative statements and the aging minimum are.
- The datasheet's stress-corrosion note gives a solution-treatment step of 1700°F for 15 minutes for the H 950 rows; a full heat-treatment cycle was not opened, so only the aging minimum is recorded.
- Hardness and impact energy use benchmark names not in the canonical list (hardness_rockwell_c and charpy_impact_energy); the values are recorded under those names.
- No safety data sheet for PH 13-8 Mo was found or read. The hazard codes recorded are PubChem's codes for nickel as an element, not for this alloy.
- The chromium and molybdenum USGS texts read here print no critical-mineral list entry, so critical_lists is left empty for them. The nickel text also prints none.
- No atomic weights are recorded for the recipe parts; the composition is recorded as printed limits.
- No flight data, outgassing, atomic-oxygen or radiation results for this alloy were found in the sources read.
- The AMS 5629 specification text itself was not opened; the AMS number is recorded from the Bibus header only.
- Launch-vehicle hardware use, named in the project's plan entry, is not printed on either datasheet read, so it is not recorded as a use.
- Strength at elevated temperature, and the effect of cold work, were not found in the sources read.
sources:
hightempmetals:
title: PH 13-8 Mo technical data, HiTemp Metals (supplier datasheet)
url: https://www.hightempmetals.com/techdata/hitemp13-8MOdata.php
kind: datasheet
license: Supplier technical data page (cited, not reproduced)
bibus:
title: PH 13-8 Mo | 1.4534 technical data, Bibus Metals (supplier datasheet)
id: EN 1.4534, UNS S13800, AMS 5629
url: https://sd-metals.bibus.com/de-en/materials/itm/PH-13-8-Mo-1-4534/
kind: datasheet
license: Supplier technical data page (cited, not reproduced)
usgs-nickel-2026:
title: 'Mineral Commodity Summaries 2026: Nickel (USGS)'
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-nickel.pdf
year: 2026
kind: report
license: public domain (USGS)
usgs-chromium-2026:
title: 'Mineral Commodity Summaries 2026: Chromium (USGS)'
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-chromium.pdf
year: 2026
kind: report
license: public domain (USGS)
usgs-molybdenum-2026:
title: 'Mineral Commodity Summaries 2026: Molybdenum (USGS)'
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-molybdenum.pdf
year: 2026
kind: report
license: public domain (USGS)
pubchem-nickel:
title: 'PubChem compound record: Nickel, CID 935, including GHS classification'
id: CID 935
url: https://pubchem.ncbi.nlm.nih.gov/compound/Nickel
kind: database
license: PubChem (NCBI), public domain; classification sections attributed to notifiers
wikipedia-stainless:
title: Stainless steel (Wikipedia)
url: https://en.wikipedia.org/wiki/Stainless_steel
kind: web
license: CC BY-SA 4.0 (cited, not reproduced)
wikipedia-precipitation-hardening:
title: Precipitation hardening (Wikipedia)
url: https://en.wikipedia.org/wiki/Precipitation_hardening
kind: web
license: CC BY-SA 4.0 (cited, not reproduced)
license: CC-BY-4.0
updated: '2026-11-01'
review:
status: draft
method: assistant
checked_values: 22
unreachable: 0
caveats: 5
note: 'Values were read by an AI assistant on 2026-11-01 from the two supplier datasheets and the USGS 2026 summaries named in each entry. Caveats: the two datasheets give typical and minimum strengths on different bases; their thermal expansion values differ; the stress-corrosion table could not be transcribed reliably; the hazard codes are for nickel, not for the alloy; the Charpy and hardness benchmark names are not canonical.'
story:
risk_groups:
- title: For people
lead: No safety data sheet for this alloy was read. The hazard codes in PubChem are for nickel as an element.
level: 1
verdict: Nickel hazard codes only, not the alloy's own SDS
points:
- label: The alloy
line: 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.
- label: Welding and surfaces
line: The datasheet suggests E/ER308L filler where high weld strength is not needed, and asks that finished parts be passivated.
- title: If it fails
lead: The failure routes in the sources are stress-corrosion cracking of under-aged parts and lower impact toughness in condition H 950.
points:
- label: Under-aged parts
line: 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.
- label: Toughness
line: 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.
- title: Handling and storage
points:
- label: Surfaces
line: Keep surfaces free of scale and foreign particles, and passivate finished parts (HiTemp Metals datasheet).
- label: Condition
line: Specify the condition (H 950, H 1000 or H 1050) on every order, because strength and toughness change with it.
why: '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.'
uses:
- where: Valve parts, fittings and shafts
line: The HiTemp Metals datasheet says the alloy has been used for valve parts, fittings, cold-headed and machined fasteners, and shafts.
- where: Aircraft and reactor parts
line: The same datasheet lists aircraft components, nuclear reactor components and petrochemical applications.
can_do:
- label: Carry load
value: 1449 MPa yield (H 950, typical)
benchmark: yield_strength
line: The typical yield strength is 1449 MPa in condition H 950 (HiTemp Metals). The Bibus minimum for the same condition is 1413 MPa.
- label: Resist impact
value: 41 J Charpy (H 1000, typical)
benchmark: charpy_impact_energy
line: Charpy V-notch energy is 41 J in condition H 1000 and 27 J in condition H 950 (HiTemp Metals, typical longitudinal values).
- label: Carry heat
value: 14.0 W/m-K at 100 °C
benchmark: thermal_conductivity
line: 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.
- label: Weight
value: 7.76 g/cm3
benchmark: density
line: Density is 7.76 g/cm3 in the Bibus datasheet, with no condition printed.
- label: Melting
value: 1404 °C
benchmark: melting_point
line: The Bibus datasheet gives a single melting point of 1404 °C, with no range.
- label: Marine stress-corrosion
value: high resistance, qualitative
line: The HiTemp Metals datasheet reports a high level of resistance to stress-corrosion cracking in marine tests, without a numeric threshold.
compare: '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.'
compare_rows:
- label: Yield strength
benchmark: yield_strength
- label: Thermal conductivity
benchmark: thermal_conductivity
- label: Density
benchmark: density
handling:
- Passivate finished parts and keep their surfaces free of scale and foreign particles (HiTemp Metals datasheet).
- Age at a minimum of 1000°F (538°C) for the best stress-corrosion resistance (HiTemp Metals datasheet).
- Where high weld strength is not needed, use a standard austenitic filler such as E/ER308L (HiTemp Metals datasheet).
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:
- '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.
verdict: 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.
recipe:
line: 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.
parts:
- name: Iron
symbol: Fe
share_note: balance (Bibus prints Rest)
role: The matrix that the other elements are added to.
- name: Chromium
symbol: Cr
share_percent: 12.25
share_high: 13.25
role: Gives the stainless corrosion resistance; Wikipedia says 10.5% or more forms the passive film.
- name: Nickel
symbol: Ni
share_percent: 7.5
share_high: 8.5
role: Alloying element printed in the composition table; its role in this grade is not described in the sources read.
- name: Molybdenum
symbol: Mo
share_percent: 2
share_high: 2.5
role: Alloying element printed in the composition table; its role in this grade is not described in the sources read.
- name: Aluminium
symbol: Al
share_percent: 0.9
share_high: 1.35
role: Alloying element printed in the composition table; the datasheets do not say how it forms the hardening particles.
References
Every number above carries a reference number. Click one to see the source and where in it the value comes from.
| # | Source | Type | Year | Used for |
|---|---|---|---|---|
| PH 13-8 Mo technical data, HiTemp Metals (supplier datasheet) | datasheet | 24 values | ||
| PH 13-8 Mo | 1.4534 technical data, Bibus Metals (supplier datasheet) | datasheet | 12 values | ||
| Mineral Commodity Summaries 2026: Nickel (USGS) | report | 2026 | 1 value | |
| Mineral Commodity Summaries 2026: Chromium (USGS) | report | 2026 | 1 value | |
| Mineral Commodity Summaries 2026: Molybdenum (USGS) | report | 2026 | 1 value | |
| PubChem compound record: Nickel, CID 935, including GHS classification | database | 1 value | ||
| Stainless steel (Wikipedia) | web | 1 value | ||
| Precipitation hardening (Wikipedia) | web | 0 values |
Updated