Designations and equivalents
One alloy, five names. Buyers reach it through whichever system their drawing uses, which is why the same steel turns up on enquiries as S15500, as XM-12 and as 1.4545.
| System | Designation |
|---|---|
| UNS, United States | S15500 |
| ASTM type | XM-12 |
| Werkstoff-Nr., Germany | 1.4545 |
| EN name | X5CrNiCu15-5 |
| Trade and common names | 15-5PH, 15-5 PH, Alloy 15-5 |
S17400, 1.4542, X5CrNiCuNb16-4, AISI 630 and SUS 630 are not equivalents. Those designate 17-4PH, a separate alloy with higher chromium and a different melt practice.
Specifications by product form
For a forging, the governing document is A705. A564 is frequently quoted instead, because buyers work from bar practice, and the chemistry is the same in both, but the testing and sampling clauses differ. State which one applies on the order.
| Product form | Specification | Type or grade |
|---|---|---|
| Forgings | ASTM A705 / A705M | XM-12 |
| Forgings, pressure equipment | ASME SA-705 | XM-12 |
| Bar and shapes | ASTM A564 / A564M | XM-12 |
| Sheet, strip, plate | ASTM A693 | XM-12 |
| Aerospace bar, forgings, rings | AMS 5659 | Type 1 vacuum melt, Type 2 ESR |
| Aerospace sheet, strip, plate | AMS 5862 | — |
| Welding wire | AMS 5826 | — |
| General requirements | ASTM A484 | — |
ASTM B564 covers nickel alloy forgings. It is sometimes quoted for S15500 in error and does not apply to this steel.
Chemical composition
AMS 5659 is the tighter of the two documents on residuals, holding sulphur to 0.015 % against 0.030 % in the ASTM grades, and it caps molybdenum where ASTM does not list the element at all. Where a part is bought to A705 but destined for fatigue-critical service, it is worth writing the AMS sulphur limit into the order.
| Element | ASTM A705 / A564, XM-12 | AMS 5659 |
|---|---|---|
| Carbon, C | 0.07 max | 0.07 max |
| Manganese, Mn | 1.00 max | 1.00 max |
| Silicon, Si | 1.00 max | 1.00 max |
| Phosphorus, P | 0.040 max | 0.030 max |
| Sulphur, S | 0.030 max | 0.015 max |
| Chromium, Cr | 14.00 to 15.50 | 14.00 to 15.50 |
| Nickel, Ni | 3.50 to 5.50 | 3.50 to 5.50 |
| Copper, Cu | 2.50 to 4.50 | 2.50 to 4.50 |
| Niobium plus tantalum, Nb+Ta | 0.15 to 0.45 | 0.15 to 0.45 |
| Molybdenum, Mo | not specified | 0.50 max |
| Iron, Fe | balance | balance |
Heat treatment
Solution annealing and ageing are both carried out here, so parts leave the works in the condition stated on the order rather than needing treatment elsewhere. Ageing temperatures sit between 482 and 621 °C, low enough that scale and distortion during hardening stay small, which is why many customers rough machine first and age afterwards.
| Condition | Temperature | Soak | Cooling |
|---|---|---|---|
| A, solution annealed | 1038 °C / 1900 °F | 0.5 h | Air |
| H900 | 482 °C / 900 °F | 1 h | Air |
| H925 | 496 °C / 925 °F | 4 h | Air |
| H1025 | 552 °C / 1025 °F | 4 h | Air |
| H1075 | 579 °C / 1075 °F | 4 h | Air |
| H1100 | 593 °C / 1100 °F | 4 h | Air |
| H1150 | 621 °C / 1150 °F | 4 h | Air |
| H1150M | 760 °C / 1400 °F, then 621 °C / 1150 °F | 2 h, then 4 h | Air after each |
H1000 and H1050 are not recognised conditions for this alloy and appear on enquiries from time to time through confusion with other PH grades. If a drawing calls for one of them, the intended condition is usually H925 or H1075 and we will ask before proceeding. Annealing after hot work is at 1038 °C for one hour with rapid cooling, so that the material responds correctly to ageing.
Mechanical properties
The figures below are specification minimums, not typical results. Hardness bands are from AMS 5659.
| Condition | Tensile, MPa | Tensile, ksi | Yield 0.2 %, MPa | Yield 0.2 %, ksi | Elong. % | R of A % | Hardness HB |
|---|---|---|---|---|---|---|---|
| A | — | — | — | — | — | — | 363 max |
| H900 | 1310 | 190 | 1170 | 170 | 10 | 35 | 388 to 444 |
| H925 | 1170 | 170 | 1070 | 155 | 10 | 38 | 375 to 429 |
| H1025 | 1070 | 155 | 1000 | 145 | 12 | 45 | 331 to 401 |
| H1075 | 1000 | 145 | 860 | 125 | 13 | 45 | 311 to 375 |
| H1100 | 965 | 140 | 790 | 115 | 14 | 45 | 302 to 363 |
| H1150 | 930 | 135 | 725 | 105 | 16 | 50 | 277 to 352 |
H1150M is supplied against properties agreed at enquiry, since the double-overaged values are not listed uniformly across the ASTM and AMS documents. Transverse properties are lower than longitudinal and cannot be determined where the section measures under about 76 mm in the test direction; rounds, squares and hexagons have no short-transverse direction. In heavy forgings the result depends on section size and test position, so the ruling section and the sampling location are fixed at enquiry stage and testing is carried out on prolongations taken from the forging itself.
Charpy requirements, where the order carries them, are agreed as a separate line rather than taken from the grade tables. Impact testing down to minus 60 °C runs in the works laboratory on a JBN-300 pendulum with a DWC-60 bath; below that temperature the test is placed with an accredited laboratory.
Physical properties
| Property | Metric | Imperial |
|---|---|---|
| Density | 7.80 g/cm³ | 0.282 lb/in³ |
| Melting range | 1404 to 1440 °C | 2560 to 2625 °F |
| Modulus of elasticity | 196 GPa | 28.4 × 10&sup6; psi |
| Poisson's ratio | 0.27 to 0.30 | 0.27 to 0.30 |
| Thermal conductivity, 150 °C | 17.8 W/m·K | 124 BTU·in/hr·ft²·°F |
| Coefficient of thermal expansion | 10.4 µm/m·°C | 5.78 µin/in·°F |
| Magnetic response | Ferromagnetic in all conditions | Ferromagnetic in all conditions |
Expansion and conductivity figures vary a little between published datasheets according to the temperature interval used, so take them as design guidance rather than acceptance values.
Melting and forging route
The steel for an S15500 forging is melted on site rather than bought as billet. Carbon, alloy and stainless heats run through a 25 t electric arc furnace, are refined in 25 t and 50 t ladle furnaces, and go through vacuum oxygen decarburisation in 30 t or 60 t units where carbon and nitrogen need holding down. Maximum heat size is 60 tonnes.
Because S15500 is a remelted grade by definition, the second stage matters. Protective-atmosphere electroslag remelting in 3 t and 6 t furnaces satisfies AMS 5659 Type 2. Where Type 1 vacuum melt is called for, the route is 3 t vacuum induction melting followed by 6 t vacuum arc remelting. Having both in house is the reason this grade does not need subcontracting out, which is the usual bottleneck for Chinese forging shops working to AMS documents.
From ingot the part is cogged or upset on 6300 t, 4000 t or 2000 t hydraulic presses, or ring rolled on radial-axial mills at 6 m, 3 m and 1 m. Five hammers between 750 kg and 5 t cover drawing out and smaller batch work. Heat treatment follows in one of 14 furnaces, including two 15 m well-type furnaces that let long shafts hang vertically through quench instead of distorting on a hearth. Machining, inspection and certification close out the route, all under the same roof, so the certificate traces back to a melt number rather than stopping at a purchased billet.
Forged forms and size limits
Everything below is forged from a single piece of steel melted here. No welding, no casting, no bought-in billet of unknown origin.
Rings
Seamless rolled rings, contoured rolled rings, forged rings, gear ring blanks, retaining rings, valve seat rings, slewing rings.
Shafts
Step shafts, pump and plunger shafts, eccentric shafts, crankshafts, spindles, rolls, rotors, tie rods.
Flat and hollow
Flanges, tube sheets, discs, blocks, covers, hubs, nozzles, hollow bars, sleeves, bushings, cylinders, forged pipe and tube sections.
Bar
Round, square, rectangular, flat and hex forged bar, plus near-net contoured preforms for finish machining.
Valve and wellhead
Valve stems, seat rings, bodies, bonnets, blocks, spools and manifolds.
Delivery condition
As-forged with allowance, proof machined for volumetric inspection, or finish machined to drawing.
| Item | Limit | Set by |
|---|---|---|
| Seamless rolled rings | OD 50 to 6000 mm | 6 m radial-axial ring mill; upset and punch route below mill range |
| Forged shafts | to 14 000 mm turned length | C61160 horizontal lathe; 15 m well furnace for vertical quench |
| Discs, tube sheets, blocks | to 5000 mm machined diameter | 5000 mm vertical turning lathe |
| Bored cylinders, hollow shafts | to 1600 mm bore × 10 000 mm | CNC deep-hole drilling machine |
| Single-piece weight | to 30 000 kg | 60 t heat size; 6300 t press |
Machining, welding and forming
S15500 cuts in every condition it can be supplied in, and H1150M gives the longest tool life. The sequence most machine shops settle on is to rough out in Condition A or an overaged condition, age to the required H condition, then finish. Fully aged H900 material at 388 to 444 HB is hard going for turning, drilling and milling, and it is worth asking whether the design genuinely needs that strength before specifying it.
Welding is by shielded fusion or resistance methods with AWS E/ER630 filler. A weldment should be re-solution treated and aged afterwards, or at minimum re-aged, otherwise the heat-affected zone will not match the parent properties. The alloy is not suited to cold working and tolerates only mild forming, best attempted in the overaged condition. Nitriding can be arranged through qualified treaters; case hardness and depth depend on the process and the ageing condition and are confirmed against the treater's qualified procedure rather than quoted here.
Applications
The combination that drives selection is high strength with moderate corrosion resistance to roughly 316 °C, in a grade that behaves predictably through thickness.
- Chemical and plunger pump shafts, impeller and casing parts, compressor components.
- Valve stems, seat rings, bodies and blocks for ball, check, globe, gate and plug valves.
- Flanges, tube sheets, nozzles and covers for pressure vessels and shell-and-tube heat exchangers.
- Subsea and wellhead hardware, including Christmas tree and BOP components.
- Gear blanks, spindles and turbine parts where transverse loading rules out an air-melted grade.
- Aircraft components, pressure transducer bodies and nuclear parts bought to AMS 5659.
- Forged rolls, wheels, manifolds and crankshafts in paper, sugar and cement plant.
S15500 against S17400
These two come up side by side on almost every enquiry, so it is worth being plain about where the difference is real and where it is not.
| Attribute | UNS S15500 | UNS S17400 |
|---|---|---|
| Common name | 15-5PH | 17-4PH |
| Werkstoff-Nr. | 1.4545 | 1.4542 |
| ASTM type or grade | XM-12 | 630 |
| Chromium | 14.00 to 15.50 % | 15.5 to 17.5 % approx. |
| Melt practice | Consumable-electrode remelted, ESR or vacuum | Commonly air melted |
| Delta ferrite | Suppressed | Present |
| Transverse toughness | Higher | Lower in the short-transverse direction |
| Heavy sections | More even properties | Greater fall-off toward the centre |
| Forgeability | Better under severe upsetting | More prone to splitting |
| Strength in matching H condition | Comparable | Comparable |
Published data does not agree on whether S15500 holds a real corrosion advantage over S17400. Both sit above 410 and below 304 and 316 in general corrosion resistance, so corrosion alone is a weak reason to choose between them. The defensible reasons are section thickness, loading direction and whether the specification demands a remelted product.
Inspection and certification
Because the steel is melted here, chemistry is verified at the furnace rather than copied from a supplier's certificate. Release against an order runs melt analysis, mechanical testing on a representative prolongation, non-destructive examination, dimensional check, then certification.
| Item | Detail |
|---|---|
| Chemical analysis | Optical emission spectrometry to ASTM E415; carbon and sulphur by infrared to ASTM E1019; PMI by handheld analyser |
| Tensile | ASTM A370 or ISO 6892, on 600 kN and 300 kN machines |
| Impact | ASTM A370, to minus 60 °C in house; below that through an accredited laboratory |
| Ultrasonic | ASTM A388, EN 10228-3 or SEP 1921, acceptance class as nominated |
| Magnetic particle, penetrant | ASTM E709 and ASTM E165 on request |
| Grain size | ASTM E112 |
| Class approvals | CCS, BV, DNV, LR, NK |
| Standard certificate | EN 10204 3.1 mill test certificate |
| Witnessed certificate | EN 10204 3.2, witnessed by BV, DNV, LR, SGS, TÜV or the customer's own inspector |
| Marking | Grade, heat number and length stamped on each piece |
Corrosion testing to ASTM A262, G28 or G48 is placed with an accredited laboratory and the report is issued alongside the mill certificate. Flag it on the enquiry so it is scheduled before shipment rather than added to the delivery date afterwards.
Ordering
| Item | Detail |
|---|---|
| Minimum order | 10 kg, no minimum piece count |
| Lead time | 20 to 60 days; S15500 sits at the longer end because of the remelting step |
| Delivery condition | Condition A, or aged H900, H925, H1025, H1075, H1100, H1150, H1150M |
| Machining | As-forged, proof machined or finish machined to drawing |
| Pricing | Quoted per enquiry against grade, drawing, delivery condition and quantity |
| Payment | 30 % advance by T/T with balance against shipping documents, or irrevocable L/C at sight |
| Drawing formats | PDF, DWG, DXF, STEP |
Six items in the first email usually remove a round trip: grade or specification, dimensions or drawing, quantity and expected repeat volume, delivery condition, heat treatment and testing requirements, then certification and destination port.
Quotation for UNS S15500
Send the drawing with the condition, the ultrasonic class and the certificate type, and a price normally comes back within two working days.
Jiangyin Jiangnan Metal Co., Ltd.
No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province 214423, China
Telephone +86 189 2135 9659 · Email sales@steelforgepieces.com
Questions
Is UNS S15500 the same material as 15-5PH?
Yes. S15500 is the UNS number for the alloy sold as 15-5PH, which also appears as ASTM Type XM-12 and as W.Nr. 1.4545, name X5CrNiCu15-5. S17400, 1.4542 and AISI 630 are a different alloy, 17-4PH.
Which specification covers UNS S15500 forgings?
ASTM A705/A705M Type XM-12 for forgings, with ASME SA-705 as the pressure-equipment counterpart. A564/A564M covers bar and shapes, A693 covers sheet, strip and plate, and AMS 5659 covers consumable-electrode remelted bar, forgings and rings. ASTM B564 is a nickel alloy forging specification and does not apply.
What strength does S15500 reach in condition H900?
Minimum 1310 MPa tensile and 1170 MPa 0.2 % yield at 388 to 444 HB, with 10 % elongation and 35 % reduction of area. Toughness in H900 is the lowest of the range and the condition is the most sensitive to stress corrosion cracking, so it is specified only where the hardness is genuinely needed.
Why do H1000 and H1050 appear on some drawings?
They are not recognised conditions for this alloy. They turn up through confusion with other precipitation-hardening grades and with intermediate ageing practice. Where a drawing calls for H1000 or H1050, the intent is almost always H925 or H1075, and we ask for confirmation before heat treating.
Which condition suits a forged shaft?
Age at the highest temperature that still meets the design strength. H1075, H1100 and H1150 are the usual choices for shafts and impact-loaded parts, and H1150M where toughness and tool life matter more than strength. Reserve H900 for parts that need the hardness and are not loaded in impact.
Can you meet AMS 5659 Type 1, vacuum melt?
Yes. Type 2 runs through protective-atmosphere electroslag remelting in the 3 t or 6 t furnace. Type 1 runs 3 t vacuum induction melting followed by 6 t vacuum arc remelting. State the Type on the enquiry, because the route changes both price and lead time.
How large a ring can you roll in this grade?
Up to 6000 mm outside diameter on the 6 m radial-axial mill, with 3 m and 1 m mills for smaller sizes and an upset-and-punch route from 50 mm outside diameter. The heaviest single forging is 30 tonnes. Downstream capacity matters as much as the press: vertical lathes machine to 5000 mm swing and the deep-hole drill bores 1600 mm by 10 000 mm.
Can customers visit or send an inspector?
Yes. Audits and third-party inspections are welcome at the plant in Zhouzhuang Town, Jiangyin, between Shanghai and Nanjing on the south bank of the Yangtze. Wuxi airport is 30 km away, the Shanghai airports about 160 km. Email or call to arrange a date.
Data sources
Composition limits, heat-treatment cycles and minimum mechanical properties on this page are compiled from AMS 5659, ASTM A705/A705M, ASTM A564/A564M and published alloy datasheets, including the ARMCO 15-5 PH product data bulletin and the Rolled Alloys 15-5 datasheet. Where documents differ, the difference is noted in the text. Figures are given for guidance and carry no warranty; the purchase order and the governing specification revision take precedence, and nothing here replaces an engineering assessment of a particular application.
A plain-text version of this page is available at UNS-S15500.md.