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17-4PHDownload

Precipitation-Hardening Martensitic Stainless Steel — UNS S17400 / ASTM Type 630 / EN 1.4542. Properties, heat treatment, condition selection, comparisons, and what HT PIPE supplies.

UNS NUMBER
S17400
ASTM / EN
630 / 1.4542
STRUCTURE
Martensitic (PH)
UTS MIN (H900)
1310 MPa
CONDITIONS
H900–H1150-M
DENSITY
7.80 g/cm³
Stainless Steel 17-4PH (UNS S17400) is a chromium-nickel-copper precipitation-hardening martensitic stainless steel. It is supplied in the solution-annealed Condition A and reaches its final properties through one low-temperature ageing treatment at 482–621°C, which precipitates copper-rich phases in the martensitic matrix. Proof strength rises from roughly 800 MPa before ageing to a specified minimum of 1170 MPa at H900. Because the ageing temperature decides everything, the heat-treatment condition belongs on the order line, not in a footnote. Mechanical and physical data on this page are taken from the mill product data bulletin (ARMCO 17-4 PH®, Cleveland-Cliffs, 2022) together with the governing ASTM, AMS and NACE documents listed under Section 11.
Supply at a glance. HT PIPE supplies 17-4PH as round bar and rod, plate and sheet, forged flanges, forgings and machined parts and fasteners, to ASTM A564, A693 and A705, in Condition A or aged to H900–H1150-M, with EN 10204 3.1/3.2 certification. See Section 12 for forms and sizes, and Section 13 for what to put on the enquiry.
Cr
15–17.5%
Passive film; corrosion base
Ni
3–5%
Martensite formation; toughness
Cu
3–5%
Precipitation-hardening driver
Nb + Ta
0.15–0.45%
Grain refinement; stabilisation
OVERVIEW  

What Is Stainless Steel 17-4PH?

17-4PH takes its name from a nominal 17% chromium and 4% nickel content, with about 4% copper added so the alloy can be age hardened. Mills ship it in the solution-annealed Condition A and the user brings it to final properties with a single ageing cycle. Since that cycle runs at only 482–621°C and cools in still air, there is no quench to distort the part and only a light heat tint to remove, which is why the grade is normally roughed out, aged, and then finished.

What makes 17-4PH unusual is that one chemistry covers a very wide property band. Aged at 482°C it is a 1310 MPa tensile material; aged at 621°C it is a 930 MPa material with roughly three times the impact energy and far better resistance to chloride cracking. The condition, not the grade name, is the specification.

In service it shows up wherever a rotating or loaded part needs strength that austenitic grades cannot give: pump shafts, valve stems, balls, gates, bushings and valve trim, fasteners, couplings, wear rings, hydraulic actuator components, load cells and aerospace hardware. It is magnetic in all conditions and, with a PREN of about 17 and no molybdenum, it is not the alloy to pick for a chloride-led design. Equivalent designations are ASTM Type 630, EN 1.4542 (X5CrNiCuNb16-4), JIS SUS630, AFNOR Z6CNU17-04 and GB 05Cr17Ni4Cu4Nb.

CHEMICAL COMPOSITION  

17-4PH Chemical Composition (Weight %)

Element Min (%) Max (%) Role in the Alloy
Chromium (Cr) 15.00 17.50 Passive film; corrosion base
Nickel (Ni) 3.00 5.00 Martensite formation; toughness
Copper (Cu) 3.00 5.00 Precipitation-hardening driver
Niobium + Tantalum (Nb+Ta) 0.15 0.45 Grain refinement; carbon stabilisation
Carbon (C) — 0.07 Kept low for weldability
Manganese (Mn) — 1.00 Deoxidiser
Silicon (Si) — 1.00 Deoxidiser
Phosphorus (P) — 0.040 Impurity
Sulfur (S) — 0.030 Impurity
Iron (Fe) Balance — Matrix

ASTM A693 sets the niobium plus tantalum band at 0.15–0.45%; most producers make no intentional tantalum addition, so the reported figure is effectively niobium. PREN works out at about 17, which is the number to quote when a client compares 17-4PH against a molybdenum-bearing grade.

HEAT TREATMENT  

17-4PH Heat Treatment — Solution Annealing and Ageing (H-Codes)

Condition A is produced by solution treating at 1038 ± 14°C for half an hour and cooling below 32°C, which completes the martensite transformation. Ageing then sets the final properties. Anything that has been hot worked, forged or cast has to be solution annealed again first, or it will not respond correctly to ageing.

Condition Treatment Temperature Hold Cooling
A Solution anneal 1038 ± 14°C 0.5 h Oil, water+polymer or air to <32°C
H900 Age 482 ± 9°C 1 h Air
H925 Age 496°C 4 h Air
H1025 Age 552°C 4 h Air
H1075 Age 579°C 4 h Air
H1100 Age 593°C 4 h Air
H1150 Age 621°C 4 h Air
H1150-D Double age 621°C + 621°C 4 h + 4 h Air / air
H1150-M Condition + age 760°C then 621°C 2 h + 4 h Air / air
Two rules that cause most shop problems. Material has to be cooled to at least 32°C before ageing, because the martensite finish temperature sits near 32°C and ageing warm material leaves low ductility. And material ordered to AMS 5643 is aged in a tighter window, 482 ± 6°C for 1 hour ± 5 minutes, which is not the same as commercial ASTM A564 practice.
MECHANICAL PROPERTIES  

17-4PH Mechanical Properties by Condition

Minimum values below apply to bar up to 75 mm section tested longitudinally, per ASTM A564 / AMS 5643. Condition A is normally bought on hardness rather than strength: the specification maximum is 363 HB (38 HRC), with tensile strength typically around 1030 MPa.

Condition UTS min, MPa (ksi) YS 0.2% min, MPa (ksi) Elong. min % RA min % Hardness min (HB / HRC) Charpy V, typical J
H900 1310 (190) 1170 (170) 10 40 388 / 40 20
H925 1170 (170) 1070 (155) 10 44 375 / 38 34
H1025 1070 (155) 1000 (145) 12 45 331 / 35 47
H1075 1000 (145) 860 (125) 13 45 311 / 32 54
H1100 965 (140) 795 (115) 14 45 302 / 31 61
H1150 930 (135) 725 (105) 16 50 277 / 28 68
H1150-D 860 (125) 725 (105) 16 50 255 / 24 108
H1150-M 795 (115) 520 (75) 18 55 255 / 24 135

Hardness figures are specification minima, so production material usually runs 2–4 HRC above them. Sections over 75 mm carry reduced elongation and reduction of area, and transverse ductility in H900 and H925 is markedly lower than longitudinal, which is the point at which a remelted 15-5 PH starts to look attractive.

CONDITION SELECTION  

How to Choose Between H900, H1025 and H1150

Most 17-4PH headaches come from choosing the condition by strength alone. Work the other way round: fix the environment first, then check how much strength you can still afford.

Factor H900 H1025 H1150
Ageing temperature 482°C, 1 h 552°C, 4 h 621°C, 4 h
UTS / YS minimum 1310 / 1170 MPa 1070 / 1000 MPa 930 / 725 MPa
Elongation / hardness 10% / 40 HRC min 12% / 35 HRC min 16% / 28 HRC min
Typical Charpy V 20 J 47 J 68 J
Chloride SCC resistance Poor. Not for chloride service Good, the usual threshold Best of the three
Sour (H2S) service Not acceptable Not acceptable Still needs H1150-D or H1150-M
Machining rate Slowest, carbides advised Medium Fast
Contraction on ageing 0.00045 mm/mm 0.00053 mm/mm 0.0022 mm/mm
Typical duty Fasteners, wear parts, dry structural parts Pump shafts, valve stems, general oilfield parts Marine hardware, subsea valve stems, impact-loaded parts

H900 earns its place where strength is the whole point and the environment is clean and dry. Fasteners, wear rings, actuator pins and aerospace fittings mostly fall here. Move to H1025 when the part sees plant atmospheres, condensate or mildly corrosive process fluids and you still want four-digit tensile strength; it is the default for pump shafts and valve stems.

H1150 is the answer when chlorides, seawater or impact loading enter the picture, and it is the starting point rather than the end point for sour service: NACE compliance needs the double-aged H1150-D or H1150-M condition on top. If H900-level strength is genuinely required in a chloride or H2S environment, 17-4PH is the wrong alloy and the conversation should move to a duplex or a nickel alloy.

Bottom line. H900 for maximum strength in clean, dry service; H1025 where strength and moderate corrosion resistance have to coexist; H1150, or H1150-D / H1150-M for sour gas, whenever chlorides, seawater, impact loading or H2S are part of the duty. Never leave the condition off the order.
DIMENSIONAL & THERMAL  

Dimensional Change on Ageing and Long-Term Thermal Exposure

17-4PH contracts as it ages, by an amount fixed by the condition. That is the reason parts are roughed out in Condition A, aged, and then finished: the treatment adds no scale and no quench distortion, so contraction is the only allowance to plan for.

Condition H900 H925 H1025 H1100 H1150 H1150-M
Contraction from Condition A, mm/mm 0.00045 0.00051 0.00053 0.0009 0.0022 0.00243

Over a 500 mm length that is roughly 0.22 mm at H900 and about 1.1 mm at H1150. Long-term exposure between 371°C and 482°C is a separate problem: it cuts room-temperature impact strength even when the part is never loaded at temperature. Izod results after exposure show the size of the effect.

Condition No exposure, J 371°C, 1000 h, J 371°C, 2000 h, J 427°C, 1000 h, J
H900 18.8 9.4 5.4 2.7
H1100 75.2 9.4 5.4 4.0
PHYSICAL PROPERTIES  

17-4PH Physical Properties

Property Value Note
Density 7.80 g/cm³ 7.78 in Condition A to 7.82 at H1150
Modulus of elasticity (tension) 200 GPa Torsional modulus 77 GPa; Poisson's ratio 0.291
Thermal conductivity 17.9 W/m·K At 149°C; 22.6 W/m·K at 482°C
Mean coefficient of thermal expansion 10.8 ×10-6/K 21–93°C; 11.7 ×10-6/K over 21–427°C
Specific heat 460 J/kg·K Over 0–100°C
Electrical resistivity 80 µΩ·cm 0.80 µΩ·m; 100 µΩ·cm in Condition A
Transformation temperatures Ms 132°C / Mf 32°C Ac1 627°C, Ac3 704°C
Magnetic response Magnetic In all conditions; H1150 differs measurably from H900
PREN ≈17 No molybdenum; modest chloride resistance
CORROSION RESISTANCE  

17-4PH Corrosion Resistance

General Corrosion

Across most media 17-4PH sits close to Type 304 and clearly above the hardenable martensitics such as 410, 420 and 431, which is what the mill corrosion tables show in sulfuric, phosphoric and organic acids. Rural and mild industrial atmospheres give the same picture. Seacoast atmosphere is harder on it: light overall rusting and pitting will appear in every heat-treated condition, and stagnant seawater brings the usual crevice-attack risk, so equipment that does not run continuously should be cathodically protected.

Chloride Stress-Corrosion Cracking

Condition selection stops being a strength question here. Smooth bent-beam specimens stressed to 90–100% of the 0.2% proof strength and exposed on a marine test lot failed within 68 days in Condition H900, welded or not. Specimens aged at 552°C and above showed no failures after more than 25 years. Welds follow the same pattern, with welded specimens aged to H1025, H1075 and H1150 showing no cracking after a year in quiet seawater.

So the practical rule is to age at the highest temperature that still gives the required properties, and never below 552°C, for anything that will see chlorides, marine atmosphere or sour gas. Below that threshold the copper precipitates stay fine and the matrix around them is locally depleted in chromium, which is what drives the cracking.

Sour Service — NACE MR0175 / ISO 15156 and NACE MR0103

Testing in synthetic sour well solution (5% NaCl plus 0.5% acetic acid saturated with H2S, per NACE TM-01-77) shows that 17-4PH should be aged to H1150-D or H1150-M for the best resistance to sulfide stress cracking. Only in those double-aged conditions is the grade treated by NACE as acceptable for sour service and carried in NACE MR0175 / ISO 15156 and NACE MR0103. H900, H925 and H1025 do not qualify. Background on the standard itself is on our NACE MR0175 comparison page.

What to write on the enquiry. "17-4PH, UNS S17400, condition H1150-D (or H1150-M), maximum hardness 33 HRC on the finished component, 100% hardness testing per ASTM E18, certified to NACE MR0175 / ISO 15156." Confirm the cap against the current edition of the standard and the governing equipment specification, because that is where the hardness limit and the permitted component categories are set.

Temperature Limits

17-4PH is a strength grade, not a heat-resisting grade. Load-bearing use runs out near 300–315°C, and the impact figures above say why: 1000 hours at 371°C roughly halves the room-temperature toughness of H900 and takes H1100 from 75 J to under 10 J. Oxidation resistance is good to roughly 590°C, but that is a scaling limit rather than a strength limit. At the cold end, H925 is accepted to −18°C for general use, H1150 to −79°C and H1150-M to −196°C, while H900 should be treated with caution wherever toughness governs the design.

FABRICATION  

Fabrication — Machining, Welding and Forging

Machining

Machinability follows hardness, and hardness follows the ageing temperature. Rough-machine in Condition A, age, then finish, allowing for the contraction from Section 6. In Condition A the cutting rate and surface finish are comparable to Types 302 and 304; at H900 the rate falls to roughly 60% of that and carbide tooling pays for itself.

Condition Typical hardness, HRC Relative cutting rate, SFM Note
H1150-M 27 100–130 Best cutting rate; not the best for drilling or boring
H1150 33 80–100 Higher rate, slight sacrifice in finish
H1100 34 75–95 —
H1075 36 70–90 —
A (solution annealed) 34 60–80 Comparable to Type 302 / 304
H1025 38 50–70 —
H925 42 30–50 —
H900 44 20–30 Use carbides for production

Welding

The grade welds well and, thanks to low carbon, needs no preheat on sections up to about 100 mm. Matching filler is ER630 under AWS A5.9 for GTAW and GMAW, or E630 covered electrodes under AWS A5.4; HT PIPE also supplies welding wire and electrodes. The cleanest route is to weld in Condition A and then solution anneal and age the assembly, or at least re-age it, because weld toughness is best after a full heat treatment. Oxyacetylene welding is not recommended, interpass temperature is normally held to about 120°C, and weldment design should avoid square corners, unfused notches and sharp threads where residual stress collects.

Forging and Forming

Forge from 1177–1204°C, soak before working, cool to 32°C to refine the grain, then re-solution treat at 1024–1052°C before ageing. Severe cold working should not be attempted in Condition A; use H1100, H1150 or H1150-M and re-age afterwards to restore stress-corrosion resistance. One contamination warning belongs in every heat-treat shop: atmospheres containing carbon or nitrogen during solution treating or ageing leave a soft austenitic skin that will not age harden, or cause nitriding that costs corrosion resistance. Argon or helium should replace nitrogen.

MATERIAL COMPARISON

17-4PH vs 15-5PH, 316 and 410 — Where the Boundaries Are

These four comparisons cover most of the substitution questions that come up on a drawing. The short version first, then the detail.

Grade UNS YS 0.2%, MPa PREN Magnetic Choose it when
17-4PH H900 S17400 1170 min ~17 Yes Strength governs, environment is clean and dry
17-4PH H1150 S17400 725 min ~17 Yes Strength plus chlorides, seawater or impact loading
15-5PH S15500 1170 min (H900) ~17 Yes Heavy sections and transverse toughness matter
316 S31600 205 min ~26 No Corrosion, weldability or high temperature governs
410 S41000 205 min (annealed) ~12 Yes Low-cost hardenable wear parts in mild service

17-4PH vs 15-5PH

15-5PH (UNS S15500, ASTM A564 Type XM-12) was developed as the remelted, cleaner-toughness version of 17-4PH, and the minimum longitudinal mechanical properties at each H-code are essentially the same. The differences are in melting practice and in what happens across the grain.

Aspect 17-4PH 15-5PH
UNS / ASTM type S17400, Type 630 S15500, Type XM-12
Cr / Ni / Cu 15.0–17.5 / 3.0–5.0 / 3.0–5.0 14.0–15.5 / 3.5–5.5 / 2.5–4.5
Melting practice Air melted as standard; ESR / VAR optional Normally ESR or vacuum-arc remelted
H900 minimums 1310 / 1170 MPa, 10% elongation 1310 / 1170 MPa, 10% elongation
Transverse properties Weaker direction, the known limitation Better transverse ductility and toughness
Typical specifications ASTM A564, A693, A705; AMS 5643 ASTM A564 XM-12; AMS 5659 bar, AMS 5862 plate
Availability and cost Very widely stocked, lower cost Tighter supply, higher cost

Verdict: stay with 17-4PH unless the drawing calls out transverse or short-transverse properties, a remelt requirement, or a heavy section where consistency is the risk. Where 17-4PH has already failed on transverse ductility, 15-5PH is the intended fix rather than a trial substitute.

17-4PH vs 316

This is not really an either-or, and most plants use both: 316 for wetted piping and vessels, 17-4PH for the shafts and stems that run inside them.

Aspect 17-4PH (H900) 316 (annealed)
Proof strength 1170 MPa min 205 MPa min
PREN / chloride resistance ~17, no molybdenum ~26, 2–3% molybdenum
Magnetic Yes, all conditions No, except after heavy cold work
Hardening route Age at 482–621°C, air cool Cannot be hardened by heat treatment
Welding Welds well; PWHT by re-ageing Welds readily; no PWHT normally needed
Service temperature Load-bearing to about 300°C Roughly −196 to 870°C

Verdict: pick 17-4PH when the part is strength-limited and the environment is controllable, and pick 316 when corrosion, weldability or temperature governs. If you need both high strength and 316-class corrosion resistance, neither is right; look at duplex 2205 instead.

17-4PH vs 410

Both are martensitic and magnetic, and both are chosen for strength rather than corrosion resistance, but they get there differently. 410 hardens by austenitising near 925–1010°C and quenching, then tempering; 17-4PH hardens by ageing at 482–621°C with no quench at all. That single difference drives distortion risk, cracking risk and dimensional control.

Aspect 410 17-4PH
Composition Cr 11.5–13.5, C 0.08–0.15, no nickel Cr 15–17.5, Ni 3–5, Cu 3–5
Hardening route Quench and temper Age, air cool
UTS / YS, annealed 450 / 205 MPa min Typically about 1030 MPa UTS
UTS after hardening Around 700–800 MPa, 30–40 HRC 1310 MPa min at H900, 40 HRC min
PREN ~12 ~17
Welding HAZ air-hardens; preheat and PWHT usual No preheat to 100 mm; re-age after welding
Cost position Lowest-cost hardenable stainless Higher alloy cost, lower machining and distortion cost

Verdict: 410 is the economical choice for wear parts, seats and general hardware in mild service where 12% chromium is enough. 17-4PH is the choice when the part needs 304-class corrosion resistance alongside high strength, when distortion from quenching cannot be tolerated, or when the assembly has to be welded without preheat. Full comparison: see all material comparisons.

17-4PH H900 vs H1150

Aspect H900 H1150
Ageing 482°C, 1 h, air 621°C, 4 h, air
Strength 1310 / 1170 MPa minimum 930 / 725 MPa minimum
Toughness About 20 J Charpy, 10% elongation About 68 J Charpy, 16% elongation
Chloride SCC Failures in marine testing within 68 days No failures in 25 years of exposure
Sour service Not acceptable Basis for H1150-D / H1150-M, which are acceptable
Machining 20–30 SFM, carbides 80–100 SFM

Verdict: H900 when nothing but strength matters, H1150 whenever the environment or the loading does. The 380 MPa of tensile strength given up buys six points of elongation, twelve points of hardness and roughly three times the impact energy.

STANDARDS  

17-4PH Standards and Equivalent Designations

Standard / Designation Scope
ASTM A564 / ASME SA-564, Type 630 Hot-rolled and cold-finished age-hardening bar and shapes
ASTM A693 / ASME SA-693, Type 630 Plate, sheet and strip
ASTM A705 / ASME SA-705, Grade 630 Age-hardening stainless forgings
AMS 5643 / AMS 5622 Aerospace bar, wire and billets; 5622 covers ESR / vacuum-arc remelted
AMS 5825 / AMS 5827 Welding wire and covered welding electrodes
AWS A5.4 E630 / AWS A5.9 ER630 Matching filler metal classification
NACE MR0175 / ISO 15156, NACE MR0103 Sour-service qualification; H1150-D and H1150-M conditions
AMS-QQ-S-763 Class 324 / MIL-DTL-24527C Federal bars and wire; forging stock
ASTM F899 / NF S94-090 Wrought stainless for surgical instruments
EN 10088-3 / EN 1.4542 (X5CrNiCuNb16-4) European delivery condition and grade number; 1.4548 also used
JIS SUS630 / AFNOR Z6CNU17-04 / GB 05Cr17Ni4Cu4Nb Japanese, French and Chinese equivalents
ASTM A747 / A747M CB7Cu-1, CB7Cu-2 Precipitation-hardening castings of the same family
SUPPLY  

17-4PH Supplier — Product Forms, Standards and Capabilities

HT PIPE supplies 17-4PH across the forms that buying teams actually order: round bar and rod for shafts and fasteners, plate and sheet for machined components, forged flanges and forged fittings, and custom forgings and machined parts made to drawing. Material is delivered in Condition A ready for your own ageing, or aged to the specified H-code with the heat-treatment chart recorded on the certificate.

Product Form Specification Conditions supplied HT PIPE
Round bar / rod ASTM A564 Type 630, AMS 5643 Condition A or aged H900–H1150-M Stock and made to order
Plate / sheet ASTM A693 Type 630 Condition A, aged on request Made to order
Forged flanges ASTM A705 Grade 630, ASME B16.5 dimensions H1025, H1150 typical Made to order
Forged fittings ASTM A705, to drawing Per drawing Made to order
Forgings, rings, discs, shafts ASTM A705 / A564, to drawing Per drawing, with ageing Made to order
Fasteners ASTM A564, to drawing H900 typical Made to order
Welding consumables AWS A5.9 ER630, AWS A5.4 E630 As supplied On request

Quality and documentation. Every order ships with mill certification to EN 10204 3.1, with 3.2 or third-party inspection (SGS, BV, TÜV) available where the project requires it. Routine verification covers PMI on chemistry, hardness testing per ASTM E18, and ultrasonic examination on bar and forgings; Charpy testing can be added where the specification calls for it. Sour-service orders are heat treated to H1150-D or H1150-M and hardness tested on the finished component.

Bar is the fastest route: it is the form most often held in Condition A, so a shaft order can be cut, aged and certified without waiting on a mill rolling. Plate, flanges and custom forgings are quoted against your drawing or size list, and we will state on the quotation whether the size is ex-stock or made to order, and what the ageing step adds to the lead time.

ENQUIRY  

How to Specify 17-4PH on a Purchase Order

An enquiry that only says "17-4PH round bar" will come back as a question, because the condition alone can move the yield strength by 450 MPa. Eight lines are enough to make it quotable:

# Line What to write
1 Condition H900, H1025, H1150, H1150-D or H1150-M. Mandatory, never optional
2 Specification ASTM A564 / A693 / A705, or AMS 5643 for aerospace work
3 Size and quantity Diameter or thickness, length, piece count; drawing for machined parts
4 Hardness ceiling For sour service: maximum 33 HRC on the finished component, per NACE MR0175 / ISO 15156
5 Certification EN 10204 3.1 as standard, 3.2 or third-party witness if required
6 Testing PMI, UT, hardness survey, Charpy if the specification calls for it
7 Heat-treat route Mill-aged and certified, or Condition A for ageing in your own shop
8 Finish and packing Peeled, turned or ground; export packing and marking requirements
Copy this into your RFQ: "17-4PH, UNS S17400, ASTM A564 Type 630 round bar, 60 mm dia × 3 m, 500 kg, condition H1150, EN 10204 3.1, PMI and hardness report, UT per ASTM A388." Add the NACE line and the 33 HRC ceiling if the service contains H2S.
Get a 17-4PH Quotation with the Condition You Can Certify
Send us the form, the size, the condition and the governing specification. We quote bar, plate, flanges and forgings to ASTM A564, A693 and A705, with ageing to H900–H1150-M and EN 10204 3.1 / 3.2 certification. Drawings welcome; trial quantities are quoted too.
Request a Quote
FAQ  

FAQ — 17-4PH Stainless Steel

What is the most important thing when ordering 17-4PH?
State the heat-treatment condition: H900, H1025, H1150, H1150-D or H1150-M. Properties come entirely from ageing, so an order reading only "17-4PH" can legitimately arrive anywhere between 795 MPa and 1310 MPa of tensile strength.
Should I specify H900, H1025 or H1150?
Decide on the environment first. H900 suits clean, dry, strength-limited parts such as fasteners and wear rings. H1025 is the general-purpose choice for pump shafts and valve stems where moderate corrosion resistance is needed alongside strength. H1150 is for chlorides, seawater, impact loading and marine hardware, and H1150-D or H1150-M is required for H2S service.
What is the difference between 17-4PH H900 and H1150?
H900 ages at 482°C and gives minimums of 1310 MPa tensile, 1170 MPa proof strength, 10% elongation and 40 HRC. H1150 ages at 621°C and gives 930 MPa, 725 MPa, 16% and 28 HRC. You give up 380 MPa of tensile strength and gain six points of elongation, twelve points of hardness and roughly three times the impact energy, plus far better chloride stress-corrosion resistance.
Is 17-4PH acceptable for sour service under NACE MR0175?
Only in the double-aged H1150-D or H1150-M condition, and only if the finished component stays at or below the hardness ceiling in the current edition of NACE MR0175 / ISO 15156, which is normally 33 HRC. H900, at 40 HRC minimum, does not qualify. Ask for 100% hardness testing per ASTM E18 on the finished part rather than relying on a mill certificate for the bar.
Does HT PIPE supply 17-4PH round bar and plate, and in which condition?
Yes. Round bar and rod to ASTM A564 Type 630 is the form most often held in stock and is supplied in Condition A or aged to the H-code you nominate. Plate and sheet to ASTM A693 is supplied in Condition A with ageing on request, and forged flanges, fittings and custom forgings to ASTM A705 are made to order. See Section 12 for the full list.
Can I order 17-4PH in Condition A and age it myself?
Yes, and it is common practice because ageing is a single low-temperature step in an ordinary furnace followed by air cooling. Say clearly on the order that the bar is required in Condition A for customer ageing, and agree what the certificate will report, since it will carry Condition A properties and the aged values become your responsibility to verify. Anything hot worked before ageing must be re-solution treated first.
What are the equivalents of 17-4PH in other standards?
UNS S17400, ASTM Type 630, EN 1.4542 (X5CrNiCuNb16-4, also written 1.4548), JIS SUS630, AFNOR Z6CNU17-04 and GB 05Cr17Ni4Cu4Nb. The cast equivalent is CB7Cu-1 or CB7Cu-2 under ASTM A747, and wrought property data should not be applied to castings without checking the casting specification.
Which should I buy, 17-4PH or 15-5PH?
Minimum longitudinal properties are the same at every H-code, so the decision is about the direction you are loading in. 15-5PH is remelted and was developed specifically to improve transverse and short-transverse toughness, which is where 17-4PH is weakest. Choose 15-5PH for heavy sections, aerospace work with remelt requirements, and parts stressed across the grain; choose 17-4PH otherwise, because it is more widely stocked and costs less.
Which is better, 17-4PH or 316 stainless steel?
Neither is universally better. 17-4PH gives roughly five times the proof strength, 1170 MPa against 205 MPa, and is the choice for shafts, stems and fasteners. 316 has a PREN of about 26 against 17, is non-magnetic, welds without post-weld heat treatment and works from cryogenic temperatures up to about 870°C, so it wins wherever corrosion, weldability or temperature governs. Many systems use both.
Is 17-4PH magnetic?
Yes, in every condition, because the structure is martensitic. Response is similar from H900 through H1075 and changes measurably at H1150, which can matter for parts located near instruments or sensors.
Can 17-4PH be used at high temperature?
Not as a heat-resisting grade. Load-bearing use ends near 300°C, and long exposure between 371°C and 482°C sharply reduces room-temperature impact strength, with H900 falling from about 19 J to 5 J after 2000 hours at 371°C. Oxidation resistance is good to roughly 590°C, but that is a scaling limit, not a strength limit.
What filler metal should be used to weld 17-4PH?
Matching filler is ER630 under AWS A5.9 for GTAW and GMAW, or E630 covered electrodes under AWS A5.4. No preheat is needed on sections up to about 100 mm, interpass temperature is normally limited to 120°C, and the best weld toughness comes from a full solution anneal and age after welding rather than ageing alone.
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