1.4534 (PH13-8Mo) Open-Die Forgings: Rings, Bars, Flanges and Shafts
Maintained by Jiangyin Jiangnan Metal Co., Ltd. Last reviewed .
EN 1.4534 is a martensitic precipitation-hardening stainless steel. It is designated X3CrNiMoAl13-8-2 in EN 10088-3 and is known internationally as PH13-8Mo, UNS S13800 and ASTM Type XM-13. The alloy contains roughly 13% chromium, 8% nickel, 2.2% molybdenum and 1.1% aluminium, and is hardened by a single low-temperature ageing treatment that precipitates nano-scale NiAl particles. In the H950 condition it reaches a minimum tensile strength of 1,517 MPa (220 ksi) at 45 HRC, with better transverse toughness and stress-corrosion resistance than 17-4PH.
Jiangyin Jiangnan Metal Co., Ltd. supplies 1.4534 as open-die forgings and seamless rolled rings: forged rings, flanges, round bars, shafts, discs, sleeves, bushings, tube sheets and hollow forgings. Parts are delivered solution annealed, or aged to H950, H1000, H1025, H1050, H1100 or H1150, with ultrasonic testing to EN 10228-3, SEP 1921 or ASTM A388 and EN 10204 3.1 or 3.2 certification.
- EN number
- 1.4534
- EN name
- X3CrNiMoAl13-8-2
- UNS number
- S13800
- Common trade name
- PH13-8Mo (also written 13-8 PH, 13-8Mo)
- ASTM type
- XM-13
- Steel family
- Martensitic precipitation-hardening (PH) stainless steel
- Strengthening mechanism
- NiAl intermetallic precipitation during ageing
- Product standards
- EN 10088-3; ASTM A705/A705M Type XM-13 (forgings); ASTM A564 Type XM-13 (bars); AMS 5629 (bars, forgings, rings); ASTM A693 (sheet and plate)
- Strength range
- 931 to 1,517 MPa (135 to 220 ksi) minimum UTS, depending on ageing condition
- Hardness range
- 30 to 45 HRC minimum, H1150 through H950
- Density
- 7.76 g/cm³ (0.280 lb/in³)
- Magnetic response
- Ferromagnetic in all conditions
- Forms we forge
- Seamless rolled rings, flanges, round bars, shafts, discs, sleeves, bushings, tube sheets, hollow forgings
- Supplier
- Jiangyin Jiangnan Metal Co., Ltd., Jiangyin City, Jiangsu Province, China
What is 1.4534 steel?
1.4534 is the European material number for X3CrNiMoAl13-8-2, a martensitic precipitation-hardening stainless steel developed as a cleaner and tougher alternative to 17-4PH. Carbon is held to 0.05% maximum, sulphur and phosphorus are kept very low, and aluminium and molybdenum take the place of the copper and niobium used in 17-4PH.
Strength does not come from carbon. The steel is solution treated at about 927 °C and cooled below 16 °C, which turns austenite into a soft, low-carbon martensite that machines reasonably well. Ageing between 510 °C and 621 °C then precipitates coherent NiAl particles a few nanometres across, raising yield strength by 400 to 800 MPa without a quench and with very little distortion.
For a forging buyer this means one grade covers a wide strength band. The same forged ring can be supplied at 1,517 MPa and 45 HRC (H950), or at 931 MPa and 30 HRC with much higher ductility (H1150), by changing only the ageing temperature. Ageing happens below the tempering range of most steels, so finish-machined parts can be aged with little dimensional change, typically a linear contraction of about 0.05% to 0.10%.
1.4534 grade equivalents and cross-references
| System | Designation | Notes |
|---|---|---|
| EN / Werkstoff | 1.4534 | Material number used across EN 10088 and EN 10222 |
| EN name | X3CrNiMoAl13-8-2 | EN 10088-3 chemical-symbol designation |
| UNS | S13800 | North American unified numbering |
| ASTM type | XM-13 | Used in A564, A693, A705 and ASME SA-705 |
| Trade name | PH13-8Mo | Most common commercial name worldwide |
| SAE / aerospace | AMS 5629 | Bars, forgings, rings, wire, extrusions |
| Proprietary | Böhler N709; ATI 13-8 | Mill-specific brands of the same grade |
Naming note: 1.4534 and PH13-8Mo are two names for one steel, not two grades. If your drawing calls out either designation, or UNS S13800 or XM-13, the same forging satisfies it, provided the melt route and ageing condition on the order match your specification.
Chemical composition of 1.4534 / PH13-8Mo
1.4534 contains 12.25% to 13.25% chromium, 7.50% to 8.50% nickel, 2.00% to 2.50% molybdenum and 0.90% to 1.35% aluminium, with carbon at 0.05% maximum. Sulphur is limited to 0.008%, phosphorus to 0.010%, silicon to 0.10% and manganese to 0.20%. Those tight limits are what give the grade its transverse toughness, because they suppress the inclusion stringers that would otherwise act as crack initiation sites across the grain flow of a forging.
| Element | Symbol | Weight % | Function in the alloy |
|---|---|---|---|
| Chromium | Cr | 12.25 – 13.25 | Passive film, corrosion resistance |
| Nickel | Ni | 7.50 – 8.50 | Forms NiAl precipitates; stabilises austenite before quench |
| Molybdenum | Mo | 2.00 – 2.50 | Pitting and crevice corrosion resistance |
| Aluminium | Al | 0.90 – 1.35 | Primary hardening element (NiAl precipitation) |
| Carbon | C | 0.05 max | Held low to protect toughness and weldability |
| Manganese | Mn | 0.20 max | Residual, restricted for cleanliness |
| Silicon | Si | 0.10 max | Residual, restricted for cleanliness |
| Phosphorus | P | 0.010 max | Impurity, restricted |
| Sulphur | S | 0.008 max | Impurity, restricted for transverse toughness |
| Nitrogen | N | 0.010 max | Impurity, restricted |
| Iron | Fe | Balance | Matrix |
Mechanical properties of 1.4534 by ageing condition
The mechanical properties of 1.4534 are set by the ageing temperature. Each condition is named after that temperature in degrees Fahrenheit, so H950 means aged at 950 °F (510 °C). Lower ageing temperatures give higher strength and hardness. Higher temperatures over-age the NiAl precipitates and trade strength for ductility, toughness and better stress-corrosion performance.
| Condition | Ageing temp. | Tensile strength min. | 0.2% yield min. | Elongation min. | Reduction of area min. | Hardness min. |
|---|---|---|---|---|---|---|
| H950 | 510 °C / 950 °F | 1,517 MPa (220 ksi) | 1,413 MPa (205 ksi) | 10% | 45% | 45 HRC |
| H1000 | 538 °C / 1000 °F | 1,413 MPa (205 ksi) | 1,310 MPa (190 ksi) | 10% | 50% | 43 HRC |
| H1025 | 552 °C / 1025 °F | 1,310 MPa (190 ksi) | 1,207 MPa (175 ksi) | 11% | 50% | 41 HRC |
| H1050 | 566 °C / 1050 °F | 1,207 MPa (175 ksi) | 1,138 MPa (165 ksi) | 12% | 50% | 40 HRC |
| H1100 | 593 °C / 1100 °F | 1,034 MPa (150 ksi) | 931 MPa (135 ksi) | 14% | 50% | 34 HRC |
| H1150 | 621 °C / 1150 °F | 931 MPa (135 ksi) | 621 MPa (90 ksi) | 14% | 50% | 30 HRC |
H900 and H925 do not exist for this grade. Those conditions belong to 17-4PH (1.4542) and 15-5PH. The lowest standard ageing condition for 1.4534 and PH13-8Mo is H950. If a drawing calls for 1.4534 in H900, query it with the design authority before ordering, because the two grades are often confused on older drawings.
Transverse properties in heavy forgings
The values in Table 3 are longitudinal, measured along the grain flow. In heavy open-die forgings the transverse and short-transverse directions usually matter more in service. 1.4534 is specified for that reason: controlled sulphur and the absence of coarse carbides mean transverse reduction of area retains a larger fraction of the longitudinal value than in 17-4PH. If your part is loaded across the grain flow, say so at the enquiry stage and we will plan the upsetting and drawing sequence, and the test-piece orientation, around it.
Physical properties of 1.4534
| Property | Metric | Imperial |
|---|---|---|
| Density | 7.76 g/cm³ | 0.280 lb/in³ |
| Modulus of elasticity | 203 GPa | 29.4 × 10⁶ psi |
| Thermal conductivity | approx. 14 W/m·K | approx. 8.1 Btu/hr·ft·°F |
| Mean thermal expansion (20–100 °C) | approx. 10.6 µm/m·K | approx. 5.9 µin/in·°F |
| Specific heat | approx. 460 J/kg·K | approx. 0.11 Btu/lb·°F |
| Electrical resistivity | approx. 1.02 µΩ·m | approx. 613 Ω·circ mil/ft |
| Melting range | 1,404 – 1,440 °C | 2,560 – 2,625 °F |
| Magnetic permeability | Ferromagnetic in all heat-treated conditions | |
| Practical max. service temperature | About 425 °C (800 °F). Do not exceed the ageing temperature of the condition supplied. | |
Heat treatment of 1.4534 forgings
1.4534 is heat treated in two stages: solution treatment, followed by a single ageing cycle. We carry out both in house on forged parts, and can also supply in Condition A for customers who prefer to age after machining.
Solution treatment, Condition A
- Heat to 927 °C ± 15 °C (1,700 °F ± 25 °F) and hold, typically one hour per 25 mm of ruling section.
- Cool in air or oil to below 16 °C (60 °F) and hold to complete the transformation to martensite. Heavy sections normally need a refrigeration step, since any retained austenite left in the part will not respond to ageing.
- Hardness after solution treatment is usually in the low to mid 30s HRC. That is soft enough for rough machining, which is why most buyers order Condition A for parts with heavy metal removal.
Ageing, conditions H950 to H1150
- Heat to the temperature given in Table 3, hold 4 hours at temperature, then cool in air.
- Dimensional change is small and predictable. Allow for a slight linear contraction in your finish-machining stock.
- No quench is involved, so the risk of distortion on long or thin-walled forgings is much lower than for a quench-and-temper steel.
Choosing a condition. H950 gives maximum strength and wear resistance. H1000 and H1025 are the usual compromise for shafts and pump components. H1050 suits general engineering. H1100 and H1150 are used where toughness, weldability and resistance to stress-corrosion cracking matter more than strength, for example in sour service and subsea hardware.
Forging practice and melting route
Melting
Our standard production route for 1.4534 is EAF plus VOD refining, followed by ESR (electroslag remelting). The VOD stage brings carbon, sulphur and phosphorus down to the limits the grade requires. ESR then produces a directionally solidified ingot with low segregation and a clean, homogeneous structure suitable for heavy forgings and ultrasonic acceptance.
Melt route: please confirm it at RFQ. Aerospace specifications written to AMS 5629 normally require double melting by VIM plus VAR, with ESR accepted only where the purchaser permits it. Industrial, oil and gas and general engineering orders to EN 10088-3 or ASTM A705 are routinely satisfied by EAF + VOD + ESR. Tell us which specification governs your part and we will confirm the route before quoting.
Hot working
- Forging temperature: heat uniformly to 1,150 °C to 1,200 °C (2,100 °F to 2,190 °F). Soak thoroughly, because the alloy does not tolerate an unevenly heated ingot.
- Finishing temperature: stop forging above about 925 °C (1,700 °F). Working below that risks cracking and leaves residual stress.
- After forging: cool, then solution treat. Forgings are not supplied as forged, because the solution treatment establishes the martensite that ageing later hardens.
- Grain flow: for rings and discs we use upsetting and ring rolling, so that continuous circumferential grain flow lies where the hoop stress acts, instead of machining the part from solid bar.
Our capability for 1.4534
| Product form | Size range | Unit piece weight |
|---|---|---|
| Seamless rolled rings | OD 200 – 3,000 mm, wall 30 – 400 mm | up to 8,000 kg |
| Forged round bars and shafts | Ø 80 – 900 mm, length up to 6,000 mm | up to 8,000 kg |
| Discs and blanks | Ø 200 – 2,000 mm, thickness 40 – 600 mm | up to 6,000 kg |
| Sleeves, bushings, hollow forgings | OD 150 – 1,500 mm, ID from 80 mm | up to 5,000 kg |
Forgings are supplied rough-machined with agreed test and machining allowance as standard. Finish-machined and heat-treated parts are available to drawing.
1.4534 forged product forms we supply
- Seamless rolled ringsRing-rolled with circumferential grain flow for bearing races, pump casings and turbine components.
- Forged flangesWeld-neck, blind, slip-on and special profiles for pressure vessels and heat exchangers.
- Forged round barsSolid bar stock for onward machining, supplied in Condition A or aged.
- Forged shafts and spindlesPump shafts, plunger shafts, eccentric shafts and drive spindles.
- Discs and blanksSolid or bored discs for gears, valve components and compressor parts.
- Sleeves and bushingsHollow forgings with bored or trepanned centres.
- Tube sheetsForged and rough-machined plates for shell-and-tube heat exchangers.
- Valve bodies and stemsForged blanks for ball, gate, globe, check and plug valves.
Machining and welding 1.4534
Machining
Machine 1.4534 in Condition A, or in an over-aged condition, wherever the design allows. Machinability in the solution-annealed state is roughly comparable to 410 or 420 stainless, and sits at about one third of free-machining B1112 on the standard index. At H950 the part is at 45 HRC, and turning, drilling and tapping become slow and hard on tooling. Carbide tools, rigid setups, positive rake, plenty of coolant and low surface speeds are all needed.
A workable sequence for most parts is to rough machine in Condition A, leave finishing stock, age to the specified condition, then finish machine or grind to size. Because the contraction during ageing is predictable, this holds tight tolerances without having to cut a 45 HRC workpiece.
Welding
1.4534 welds readily by GTAW, GMAW, plasma and electron-beam processes. Its low carbon content means it does not suffer the sensitisation problems of higher-carbon martensitic stainless steels. Use matching filler where full strength is required across the joint. Preheat is generally unnecessary. To obtain full mechanical properties, solution treat and re-age after welding. Where a full post-weld solution treatment is not possible, ageing alone recovers a useful part of the strength, but the weld metal and heat-affected zone will not match parent-metal values.
Corrosion and environmental behaviour
General corrosion resistance is broadly comparable to 304 stainless steel. The 2% to 2.5% molybdenum gives 1.4534 better pitting and crevice resistance than 17-4PH or 15-5PH, neither of which contains a deliberate molybdenum addition. Resistance is best in the fully hardened conditions and with a clean, passivated surface.
Two points matter in service:
- Stress-corrosion cracking. Like all high-strength martensitic PH grades, 1.4534 becomes more susceptible as strength rises. For chloride-bearing or sour environments, over-aged conditions (H1050 and above) are considerably more resistant than H950. NACE MR0175 / ISO 15156 sets hardness limits for materials in sour service, so check the applicable clause before selecting a condition.
- Hydrogen embrittlement. The alloy is sensitive to hydrogen, particularly at high strength levels. Avoid hydrogen-charging processes such as acid pickling and electroplating on high-strength parts, or bake promptly afterwards to an agreed procedure. Cathodic protection systems in subsea service should be assessed against the selected ageing condition.
Typical applications for 1.4534 forgings
Oil, gas and subsea
Wellhead and Christmas-tree components, subsea connectors, valve bodies and stems, and pump shafts. The combination of 1,000 MPa class strength, molybdenum-bearing corrosion resistance and good transverse toughness is hard to obtain from a single grade.
Chemical process and rotating equipment
Pump shafts and sleeves for chemical and plunger pumps, compressor components, valve internals, and forged rings and flanges for pressure vessels, columns, air receivers and shell-and-tube heat exchangers.
Aerospace and defence
Landing-gear components, actuator bodies, fittings and structural forgings. These are normally ordered to AMS 5629 with a VIM plus VAR melt route and full traceability.
Power generation and heavy machinery
Turbine and gas-compressor parts, gearbox shafts and gears, rolls, manifolds and forged wheels for marine and heavy-machinery service.
Tooling
Plastic injection-mould blocks and cavity inserts. The corrosion resistance protects against aggressive polymers, and the low ageing temperature avoids the distortion that comes with a hardening quench.
Testing, inspection and certification
| Item | Standard / scope |
|---|---|
| Chemical analysis | Heat analysis on every heat; product analysis on request |
| Mechanical testing | Tensile and hardness per ASTM A705 / EN 10088-3; Charpy impact on request, orientation to be specified |
| Ultrasonic testing | EN 10228-3, SEP 1921 or ASTM A388; acceptance class to be agreed at order |
| Surface NDT | Liquid penetrant (ASTM E165) or magnetic particle (ASTM E709) on request |
| Dimensional report | Issued for every rough- and finish-machined forging |
| Material certificate | EN 10204 3.1 as standard; EN 10204 3.2 with third-party witness (TÜV, BV, SGS, Lloyd's, ABS, DNV) on request |
| Traceability | Heat number hard-stamped and cross-referenced to the certificate on every piece |
How to request a quotation for 1.4534 forgings
Send a drawing or a dimensioned sketch to sales@steelforgepieces.com. To get a firm price and lead time in the first reply, include:
- Grade and governing standard, for example "1.4534 to ASTM A705 XM-13" or "PH13-8Mo to AMS 5629".
- Delivery condition: Condition A, or the ageing condition (H950 to H1150).
- Dimensions: OD, ID, length or thickness, and whether the price should be for as-forged, rough-machined or finish-machined.
- Quantity, and whether this is a prototype, a repeat order or a call-off.
- Testing and certification: UT class, impact requirements and test orientation, EN 10204 3.1 or 3.2.
- Melt route, if your specification restricts it (EAF+VOD+ESR or VIM+VAR).
- Destination port, for a delivered price.
Request a price for your 1.4534 forging
Jiangyin Jiangnan Metal Co., Ltd. is an open-die forging factory in Jiangyin, Jiangsu, producing rings, flanges, bars, shafts and discs in stainless, alloy, tool and carbon steel and in nickel alloys. Send a drawing and we will come back with a price, a lead time and the heat-treatment route we propose.
No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, ChinaTel: +86 189 2135 9659
Email: sales@steelforgepieces.com
Frequently asked questions about 1.4534
Is 1.4534 the same as PH13-8Mo?
Yes. 1.4534 is the European material number and PH13-8Mo is the common trade name for the same martensitic precipitation-hardening stainless steel. It is also designated X3CrNiMoAl13-8-2 in EN 10088-3, UNS S13800 in North America, and Type XM-13 in ASTM A564, A693 and A705. A forging made to any one of these designations satisfies the others, provided the melt route and heat-treatment condition match the specification.
What is the difference between 1.4534 and 17-4PH?
Both are martensitic precipitation-hardening stainless steels, but they harden by different mechanisms. 17-4PH (1.4542, UNS S17400) uses copper precipitation and contains niobium. 1.4534 uses NiAl intermetallic precipitation and adds 2% to 2.5% molybdenum. The result is that 1.4534 offers better transverse toughness, better pitting resistance from the molybdenum, and better resistance to stress-corrosion cracking, at a higher price. 17-4PH remains the more economical choice where those advantages are not needed. Note also that 17-4PH has H900 and H925 conditions, while 1.4534 starts at H950.
What is the hardness of 1.4534?
Hardness depends on the ageing condition. Minimum values are 45 HRC for H950, 43 HRC for H1000, 41 HRC for H1025, 40 HRC for H1050, 34 HRC for H1100 and 30 HRC for H1150. In the solution-annealed Condition A the hardness is usually in the low to mid 30s HRC, which is the state most parts are rough-machined in.
What is the tensile strength of 1.4534 in H1000?
In the H1000 condition, 1.4534 has a minimum tensile strength of 1,413 MPa (205 ksi) and a minimum 0.2% yield strength of 1,310 MPa (190 ksi), with 10% minimum elongation and 50% minimum reduction of area, per ASTM A705 and A564 Type XM-13. H1000 is one of the most commonly ordered conditions for pump shafts and valve components.
Can 1.4534 forgings be supplied in the H900 condition?
No. H900 and H925 are ageing conditions defined for 17-4PH and 15-5PH, not for 1.4534. The lowest standard ageing condition for 1.4534 and PH13-8Mo is H950, aged at 510 °C (950 °F). A drawing calling for 1.4534 in H900 usually reflects a carry-over from a 17-4PH drawing, and should be queried with the design authority before the order is placed.
How is 1.4534 heat treated?
In two stages. First a solution treatment at 927 °C ± 15 °C, followed by cooling below 16 °C to complete the transformation to martensite; heavy sections usually need refrigeration. Then a single ageing cycle: four hours at the temperature that names the condition, from 510 °C for H950 to 621 °C for H1150, followed by air cooling. There is no quench in the ageing step, so distortion is low and dimensional change is a small, predictable contraction.
Is 1.4534 weldable?
Yes. Its low carbon content (0.05% max) makes it readily weldable by GTAW, GMAW, plasma and electron-beam processes, usually without preheat, and it does not sensitise the way higher-carbon martensitic stainless steels do. To restore full mechanical properties, solution treat and re-age after welding. Where that is not practical, ageing alone recovers useful strength, but the weld and heat-affected zone will fall short of parent-metal values.
Is 1.4534 magnetic?
Yes. 1.4534 has a martensitic structure and is ferromagnetic in every heat-treated condition, including Condition A. That distinguishes it from austenitic stainless steels such as 304 and 316, which are essentially non-magnetic in the annealed condition.
Which melt route do you use for 1.4534, and does it meet AMS 5629?
Our standard route is EAF plus VOD refining, followed by ESR remelting, which suits industrial, oil and gas and general engineering orders written to EN 10088-3 or ASTM A705. AMS 5629 aerospace orders typically call for VIM plus VAR double melting, with ESR accepted only where the purchaser permits it. Please state the governing specification with your enquiry so we can confirm the melt route before quoting.
What certification do you supply with 1.4534 forgings?
EN 10204 3.1 certification is standard on every order, covering chemical analysis, mechanical test results, heat-treatment record and dimensional report, with the heat number hard-stamped on each piece. EN 10204 3.2 certification witnessed by a third party (TÜV, BV, SGS, Lloyd's, ABS or DNV) is available on request. Ultrasonic testing is reported to EN 10228-3, SEP 1921 or ASTM A388, to the acceptance class agreed at order.
What sizes of 1.4534 forgings can you produce?
We produce seamless rolled rings, flanges, round bars, shafts, discs, sleeves, bushings and tube sheets in 1.4534, in the size ranges shown in the capability table on this page, as forged, rough-machined or finish-machined. Non-standard geometries are made to drawing. Send the drawing and the governing standard and we will confirm feasibility and price.
Related precipitation-hardening and stainless grades
- PH13-8Mo forgings, the same grade under its trade name
- 17-4PH (1.4542) forgings, the economical copper-hardened alternative
- 17-7PH forgings, semi-austenitic PH grade for spring and sheet applications
- All stainless steel forging grades
- Nickel alloy forgings: Inconel 625, 718, 690, 617 and Incoloy 800/800H/825
Jiangyin Jiangnan Metal Co., Ltd. is an open-die forging factory at No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China. Property data on this page is taken from ASTM A705/A705M, ASTM A564/A564M Type XM-13 and EN 10088-3. Contact: +86 189 2135 9659, sales@steelforgepieces.com. Last reviewed .