Martensitic precipitation-hardening stainless steel. The part is machined in the solution-annealed state (Condition A), then brought to the required strength by a single aging cycle between 482 and 621 °C.
Forms
Round bar · Flat bar · Plate · Sheet · Pipe · Forging
Standards
AMS 5643 (bars, wire, forgings, mechanical tubing, rings) · AMS 5622 (same forms, consumable-electrode remelted) · AMS 5604 (sheet, strip, plate) · AMS 5825 (welding wire) · AMS 5827 (covered welding electrodes) · ASTM A564 / ASME SA-564 Type 630 (bars, wire, shapes) · ASTM A693 / ASME SA-693 Grade 630 (plate, sheet, strip) · ASTM A705 / ASME SA-705 Grade 630 (forgings) · EN 10088-3 1.4542 AMS 5643 and AMS 5622 cover the same UNS S17400 alloy; the difference is the melting route — AMS 5622 requires consumable-electrode remelted (ESR/VAR) material. AMS 5827G appears in the SAE catalogue as cancelled in September 2000;
Advantage
Strength is set by a single low-temperature cycle that requires no high-temperature quench. A part machined to finished size in Condition A is aged for 1-4 hours between 482 and 621 °C and air cooled, giving six different minimum yield levels from one alloy: 1170 MPa at H900 down to 725 MPa at…
Welding
Filler metal: for matching filler, AWS A5.9 ER630 (wire) / AWS A5.4 E630 (covered electrode); AMS equivalents are AMS 5825 and AMS 5827. Where base-metal strength is not required, austenitic AWS 308L is used — this filler does not respond to aging. Preheat: not normally required;
Limits
Continuous service temperature is limited to roughly 300-315 °C; prolonged exposure above this reduces toughness in the precipitation-hardened conditions. The H900 condition is markedly susceptible to chloride stress corrosion cracking;
Compiled from manufacturer data sheets · confirm against the current specification before ordering
On this page · click to jump
Standards by Product FormWelding, Heat Treatment and MachiningWhich Ageing Condition Should I Choose?Frequently Asked Questions
Corrosion resistance: 17-4 PH stands out for its superior corrosion resistance and offers resistance to rusting similar to that of grade 304 stainless steel. Although it is attracted by a magnet, that does not mean its corrosion resistance is low. It delivers long service life particularly in demanding environmental conditions.
Weldability: It can be welded readily by conventional methods and does not require preheating during welding. Care should be taken to avoid stresses in the design and welding of high strength steels.
Machinability: The hard internal and external structure of 1.4542 (17-4 PH) stainless steel can create some difficulties during machining. Post-production treatments improve the machinability of this steel. If heat treatment is to be applied, it is recommended that it be carried out after machining.
Heat treatment: It is produced and stocked in different heat treatment conditions depending on the application. Heat treatment options include PS800, P930, P960 and P1070 to European standards, and H1025, H1075, H1100 and H1150 to American standards.
Applications. Defence industry: chosen for its mechanical strength and long service life. Petrochemical industry: notable for its durability in chemical plants. Kitchen equipment: used for its corrosion resistance. Pump and valve shafts: its durable structure is ideal for producing parts of this kind.
1.4542 (17-4 PH / AISI 630) stainless steel is an indispensable material for many industries thanks to its wide range of applications and superior properties. Its durability, machinability and corrosion resistance make it a preferred solution.
Chemical Composition
DEFENCE METAL
C
Max. 0.070
Mn
Max. 1.00
Si
Max. 1.00
P
Max. 0.040
S
Max. 0.030
Cr
Min. 15.00 · Max. 17.50
Ni
Min. 3.00 · Max. 5.00
Cu
Min. 3.00 · Max. 5.00
Nb+Ta
Min. 0.15 · Max. 0.45
Mechanical Properties
DEFENCE METAL
Tensile Strength (MPa)
1070-1270
Proof Stress (MPa)
1000
Elongation A50 mm
10
Hardness Brinell
363 Max HB
Density
7.75 g/cm3
Melting Point
1400-1440 °C
Modulus of Elasticity
197 GPa
Electrical Resistivity
800 nΩ.m
Thermal Conductivity
18.4 W/m-K
Thermal Expansion
10.8 µm/m°C
Standards and Equivalents · 17-4Ph
DEFENCE METAL
Trade name
17-4Ph
UNS
S17400
W.Nr (DIN/EN)
1.4542
AMS
5604 · 5622 · 5642 · 5643
ASTM
A484 · A564 · A693
Available forms
Round bar · Flat bar · Plate · Sheet · Tube · Forgings All forms are supplied to order.
Standards by Product Form
STANDARDS BY PRODUCT FORM
DEFENCE METAL
Product form
Standards
Round bar, flat bar
AMS 5643 · AMS 5622 (consumable-electrode remelted) · ASTM A564 / ASME SA-564 Type 630 · EN 10088-3 1.4542
Plate, sheet
AMS 5604 · ASTM A693 / ASME SA-693 Grade 630
Forging
AMS 5643 · ASTM A705 / ASME SA-705 Grade 630
Pipe, mechanical tubing
AMS 5643 (mechanical tubing scope) · ASTM has no seamless pressure pipe specification specific to 17-4 PH
The SAE catalogue shows AMS 5827G as cancelled in September 2000; confirm the current revision for aerospace orders. AMS 7474 (bolts) and ASTM F899 (surgical instrument steels) were found in only 2 sources and are not included in the map.
The most common mistake when ordering 17-4 PH is quoting the specification without reference to the product form. The chemistry is identical in all three standards (Type 630, UNS S17400) and the condition codes are shared, but the mechanical minimums differ — the elongation minimum for sheet is markedly lower than for bar. “AISI 630” or “1.4542” alone is not an acceptance criterion; the product standard and the condition code must be stated together.
Standards by Product Form · 17-4 PH (S17400)
DEFENCE METAL
Sheet · Plate · Strip
ASTM A693 Gr. 630 / ASME SA-693 · AMS 5604
Bar · Shapes
ASTM A564 Type 630 / ASME SA-564 · AMS 5643
Forgings
ASTM A705 / ASME SA-705 · AMS 5643
Wire
ASTM A564 (wire) · AMS 5643
Rings · Discs
AMS 5643
Seamless pipe · tube
AMS 5643 (there is no dedicated ASTM tubing standard)
Welding wire
AWS A5.9 ER630 · AMS 5825
Covered electrode
AWS A5.4 E630
Aerospace work uses AMS instead of ASTM: AMS 5604 for sheet and plate, AMS 5643 for bar, forgings, tubing and rings.
Ageing conditions and ASTM A564 / A705 minimum values (all air cooled, standard temperature tolerance ±8 °C):
Ageing Conditions · ASTM A564 / A705 Minimums
DEFENCE METAL
Condition A (solution annealed)
1038 ± 14 °C · ~30 min · rapid cool — a delivery condition, not a service condition
760 °C / 2 h + 621 °C / 4 h — yield ≥ 520 MPa · tensile ≥ 795 MPa · elong. ≥ 18% · ≥ 24 HRC
These are ASTM A564 / A705 (bar and forgings) minimums, not typical values. For sheet and plate use the ASTM A693 table, where the elongation minimum is considerably lower.
Welding, Heat Treatment and Machining
HEAT TREATMENT — SCHEMATIC
1 · SOLUTION TREATMENT
1040 °C ± 15 °C (1900 °F ± 25 °F) minimum 30 minutes (after the centre reaches temperature)
2 · COOL
air, oil or water+polymer to below 32 °C (90 °F)
3 · AGEING
see the table below
DEFENCE METAL
Solution treatment
Step
Condition A (solution treated)
Temperature
1040 °C ± 15 °C (1900 °F ± 25 °F)
Time
minimum 30 minutes (after the centre reaches temperature)
Cooling
air, oil or water+polymer to below 32 °C (90 °F)
DEFENCE METAL
H900
Step
H900
Temperature
482 °C (900 °F)
Time
1 hour
Cooling
air
DEFENCE METAL
H925
Step
H925
Temperature
496 °C (925 °F)
Time
4 hours
Cooling
air
DEFENCE METAL
H1025
Step
H1025
Temperature
552 °C (1025 °F)
Time
4 hours
Cooling
air
DEFENCE METAL
H1075
Step
H1075
Temperature
579 °C (1075 °F)
Time
4 hours
Cooling
air
DEFENCE METAL
H1100
Step
H1100
Temperature
593 °C (1100 °F)
Time
4 hours
Cooling
air
DEFENCE METAL
H1150
Step
H1150
Temperature
621 °C (1150 °F)
Time
4 hours
Cooling
air
DEFENCE METAL
H1150-M
Step
H1150-M
Temperature
760 °C (1400 °F) → 621 °C (1150 °F)
Time
2 hours + 4 hours
Cooling
air cool after each cycle
DEFENCE METAL
H1150-D
Step
H1150-D
Temperature
621 °C (1150 °F), two separate cycles
Cooling
air cool after each cycle
This is a cycle schematic; no published TTT/CCT curve was used. The time axis is not to scale. Aging temperatures are Fahrenheit-based (H900 = 900 °F). Celsius equivalents differ by 1-2 °C between sources because of rounding: for example 550 °C (ASTM A564) versus 552 °C (manufacturer data sheets) for H1025. ATI and Jacquet give 1040-1065 °C for the solution treatment; ARMCO, ASTM A564, North American Stainless and Rolled Alloys state 1040 °C ± 15 °C. The H1150-D cycle time (4 hours + 4 hours) is stated explicitly in only 2 sources (ARMCO, Rolled Alloys), so it is not entered in the table; confirm it from the order specification. The Sandmeyer Steel page gives the H900 time as 4 hours and shows H1150D with the same cycle as H1150M; it conflicts with the other six sources and was not used.
Welding
GTAW (TIG), GMAW (MIG), SMAW, plasma, electron beam and resistance welding are all applicable; oxy-acetylene welding is not recommended because of carbon pick-up. The matching filler is AWS A5.9 ER630 / A5.4 E630; where weld strength is not critical a ductile austenitic filler such as 308L is used, and ERNiCr-3 / ENiCrFe-3 for dissimilar joints. Welding is carried out in Condition A; for heavy or restrained sections welding in the H1100 or H1150 condition is preferred. Welding in H900 to H1075 is not recommended. Preheat is generally unnecessary; 100–150 °C helps on restrained joints. Post-weld heat treatment is required: a single-pass weld on Condition A can be aged directly, while a multi-pass weld must be solution annealed first and then aged.
Heat treatment
The alloy combines two mechanisms: transformation to low-carbon martensite after solution annealing, and precipitation of copper-rich particles during ageing. Solution annealing is carried out at 1038 ± 14 °C for about 30 minutes followed by rapid cooling below 32 °C, producing Condition A (around 33 HRC). Ageing is a single step between 482 and 621 °C for 1–4 hours, air cooled. Condition A is a delivery and machining condition, not a service condition — untempered martensite is more susceptible to stress-corrosion cracking in chloride environments. Cold forming can only be carried out in Condition A.
Machining
Machinability in Condition A is similar to Type 302/304; the best machinability is in H1150-M. Typical single-point turning speeds: Condition A and H1150-M, 24–29 m/min with HSS and 90–137 m/min with carbide; H1075–H1150, 18 m/min HSS and 76–122 m/min carbide; H900–H925, 9 m/min HSS and 49–76 m/min carbide. The material work-hardens readily — maintain a steady, adequate feed and never let the tool dwell on the workpiece. The most efficient route is to rough and finish in Condition A and age afterwards; dimensional change during single-step, low-temperature ageing is small, so distortion risk on precision parts is low.
Which Ageing Condition Should I Choose?
STRENGTH BY AGEING CONDITION
DEFENCE METAL
Condition
Hardness
Yield MPa
Tensile MPa
Elongation
H900
≥ 40
1170
1310
10%
H925
≥ 38
1070
1170
10%
H1025
≥ 35
1000
1070
12%
H1075
≥ 32
860
1000
13%
H1100
≥ 31
795
965
14%
H1150
≥ 28
725
930
16%
All rows are ASTM A564/A564M Type 630 (ASME SA-564) STANDARD MINIMUM values — not manufacturer typical values. Values are for the bar product form. For sheet and strip (ASTM A693 / AMS 5604) the minimum elongation is lower — Ulbrich states 5% at H900 for sheet and strip. The hardness column is the ASTM A564 lower limit. Different publications vary by ±1-3 HRC at the lower limit (e.g. 34 HRC versus 35 HRC for H1025); the upper limit is set by the product form and the order specification. Manufacturer typical values are not included in this table; see the ‘atlananlar’ (omitted data) section for detail. The H1150-M and H1150-D rows are not in the table because the sources conflict; see the ‘celiskiler’ (conflicts) section.
With 17-4 PH the real choice is not the alloy but the ageing condition. The rule is simple: select the highest ageing temperature that still meets the required strength, and do not go below 552 °C (H1025) where corrosion is a factor.
Selection Guide · Ageing Condition
DEFENCE METAL
H900
Dry, atmospheric environments only; highest strength, most susceptible to stress-corrosion cracking
H1025
A good balance — high strength with markedly better stress-corrosion resistance
H1075 · H1100
Moderate strength, good toughness; preferred for welded parts
H1150 · H1150-M
Where toughness and corrosion resistance come first; best machinability
Chloride · seawater · H₂S
Do not use H900; age at 552 °C or above (H1025 and higher)
Where higher strength or a different balance is needed, 15-5 PH, 13-8 PH and Custom 455 are the other members of the same family.
Frequently Asked Questions
My material arrived in Condition A — can I use it as it is?
No. Condition A is a delivery and machining condition, not a service condition. The structure is untempered martensite: ductility is low and it is susceptible to stress-corrosion cracking in chloride environments. Machine the part in Condition A, then apply the ageing treatment (H900–H1150) appropriate to the service conditions.
Should I specify H900 or H1150?
If strength is the only requirement and the environment is dry and atmospheric, H900 (min. 1170 MPa yield). Where chlorides, seawater or H₂S are involved, do not use H900; manufacturers consistently recommend ageing at 552 °C or above. H1025 is a good balance (min. 1000 MPa yield with markedly better corrosion resistance); H1150 and H1150-M are chosen where toughness comes first. If the part is to be welded, the H1100 / H1150 class is required in any case.
Are ASTM A564, A693 and A705 interchangeable?
No — they cover different product forms: A564 bar, shapes and wire; A693 plate, sheet and strip; A705 forgings. The chemistry is the same in all three and the condition codes are shared, but the mechanical minimums differ. Quote the standard that matches the product form.