A semi-austenitic precipitation hardening stainless steel. Its structural difference from 17-4 PH and 15-5 PH is this: as delivered in Condition A the structure is AUSTENITIC (about HRB 85, ≥ 20% elongation) and it is cut, bent and drawn like 301/304.
Forms
Round bar · Flat bar · Plate · Sheet · Tube · Forging (all forms supplied to order)
Standards
AMS 5528 (sheet, strip and plate — solution heat treated, Condition A; current revision K/2024) · AMS 5529 (sheet and strip — solution heat treated and cold rolled, Condition C; 0.038-2.54 mm nominal thickness) · AMS 5568 (WELDED tubing — solution heat treated) · AMS 5644 (bars and forgings; current revision E/2017) · AMS 5678 (wire — cold drawn) · AMS 5824 (welding wire, 17Cr-7.1Ni-1.0Al) · ASTM A693 / ASME SA-693 Type 631 (plate, sheet, strip) · ASTM A564 / ASME SA-564 Type 631 (bars and shapes) · ASTM A705 / ASME SA-705 Type 631 (forgings) · ASTM A313 Type 631 (spring wire) · W.Nr. 1.4568 / X7CrNiAl17-7 1) AMS 5824 BELONGS TO A DIFFERENT UNS: it is a welding wire specification and its material is UNS S17780, not S17700. Do not write AMS 5824 on a sheet or bar order.
Advantage
The part is formed soft and gains its strength AFTERWARDS, with no quench from a high temperature in the process. In numbers: in Condition A the sheet/strip specification limits are ≤ 1034 MPa tensile, ≤ HRB 92, ≥ 20% elongation;
Welding
Filler metal: the matching filler is AMS 5824 welding wire (17Cr-7.1Ni-1.0Al, UNS S17780). Where matching strength is not required, austenitic fillers are used; Hobart Brothers recommends the 309 type (preferably low-carbon 309L or stabilized 309Cb) when matching filler is not required.
Limits
Service temperature: the sources do not agree on a single ceiling. The statement that mechanical properties are retained up to 482 °C (900 °F) in the heat-treated condition is common to Cleveland-Cliffs, Ulbrich and METALCOR (480 °C); AZoM gives 427 °C (800 °F).
Compiled from manufacturer data sheets · confirm against the current specification before ordering
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Standards by Product FormWhat the Condition Letters MeanForming, Welding and MachiningApplications and LimitsFrequently Asked Questions
Corrosion resistance: 17-7 PH is an age-hardened precipitation hardening stainless steel with the highest chromium (17%) and nickel (7%) content of the PH grades compared with 15-5 PH and 17-4 PH. 1.4568 offers excellent strength properties, high hardness and elasticity, good corrosion resistance and resistance to high temperatures and to deformation.
Weldability: 17-7 PH steel presents certain difficulties and points to observe in terms of weldability. Although this steel alloy is high strength, stainless and hardenable by heat treatment, it requires some particular precautions during welding.
Machinability: In terms of chemical composition its corrosion resistance is equal to that of AISI 301 / 1.4310 steel, while in terms of mechanical properties it is a much better choice for critical parts and components subject to fatigue. 1.4568 has an austenitic structure in the annealed condition and transforms to martensite after the ageing heat treatment, increasing its strength properties while also acquiring magnetic properties.
Heat treatment: 17-7 PH steel is processed by solution treatment and ageing. These treatments raise the hardness of the steel and give it the required mechanical properties.
Solution treatment: The steel is heated to approximately 1040-1065 °C (approximately 1900-1950 °F). It is held at this temperature for a sufficient period and is then cooled rapidly, generally in water or air. This treatment softens the steel and stabilises the martensitic phase in its internal structure.
Ageing: After solution treatment, the steel is aged for a set period at elevated temperature, between 480 and 620 °C. This temperature range is the stage that raises the hardness of the steel and develops the required mechanical properties. The ageing time and temperature directly affect the final hardness and durability of the steel, and the ageing time can generally be between 1 and 4 hours. This treatment gives the steel high strength and hardness, but its brittleness must not be increased at the same time, which is why careful control of the ageing parameters is important.
Applications: 1.4568 is used in valve components, tanks, springs, spring washers, food-industry blades, diaphragms, low and high temperature parts, heat exchangers, special fittings and installations, and machine structures and components. The steel is produced as strip, wire, plate and bar for the aerospace, oil, chemical and petrochemical industries and for the energy, food and cryogenic industries.
Chemical Composition
DEFENCE METAL
C
Max. 0.080
Mn
Max. 1.00
Si
Max. 0.70
P
Max. 0.040
S
Max. 0.015
Cr
Min. 16.00 · Max. 18.00
Ni
Min. 6.50 · Max. 7.80
Al
Min. 0.70 · Max. 1.50
Mechanical Properties
DEFENCE METAL
Tensile Strength (MPa)
1170
Proof Stress (MPa)
–
Elongation A50 mm
–
Hardness Brinell
– Max HB
Density
7.80 g/cm3
Melting Point
1400-1450 °C
Modulus of Elasticity
204 GPa
Electrical Resistivity
– nΩ.m
Thermal Conductivity
16.4 W/m-K
Thermal Expansion
11.0 µm/m°C
Standards and Equivalents · 17-7Ph
DEFENCE METAL
Trade name
17-7Ph
UNS
S17700
W.Nr (DIN/EN)
1.4568
AMS
5528 · 5529 · 5568 · 5644 · 5678 · 5824
ASTM
A564 · A579 · A693 · A705
Available forms
Round bar · Flat bar · Plate · Sheet · Tube · Forgings All forms are supplied to order.
Sheet and strip (cold rolled, Condition C; 0.038-2.54 mm)
AMS 5529 · ASTM A693 / ASME SA-693 Type 631
Plate
AMS 5528 · ASTM A693 / ASME SA-693 Type 631
Round bar, flat bar, shapes
AMS 5644 · ASTM A564 / ASME SA-564 Type 631
Forging
AMS 5644 · ASTM A705 / ASME SA-705 Type 631
Wire (cold drawn)
AMS 5678 · ASTM A313 Type 631 (spring wire)
Tube (welded)
AMS 5568. A seamless tube specification specific to S17700 could not be confirmed with four sources; it is ordered against a proprietary specification.
Welding consumables
AMS 5824 (welding wire, 17Cr-7.1Ni-1.0Al, UNS S17780 — NOT S17700)
AMS 5824 belongs to a different UNS (S17780); it is a welding wire specification. ASTM A579 was withdrawn in 2024 and in any case does not use the designation ‘631’; it is not included in this map. CH900 is possible only on cold rolled sheet/strip and cold drawn wire.
17-7 PH (UNS S17700 / AISI 631 / 1.4568) is a semi-austenitic precipitation-hardening stainless steel. Its reason for existing, in one sentence: as delivered (Condition A) it is austenitic, soft and formable like Type 301; once the part is formed it is heat-treated to transform it to martensite and then aged to spring or structural strength. That is exactly what a fully martensitic grade such as 17-4 PH cannot do.
Standards by Product Form · 17-7 PH (S17700 / AISI 631)
DEFENCE METAL
Sheet · Plate · Strip
ASTM A693 (Type 631) · AMS 5528 (general purpose, all conditions) · AMS 5529 (cold rolled, Condition C / CH900)
Bar · Forgings
AMS 5644
Welded tube
AMS 5568
Wire · spring wire
ASTM A313 (Type 631) · AMS 5678
Welding wire (filler)
AMS 5824 — note that the filler has its own UNS number, S17780, not S17700
Welding electrode (covered)
— (no verifiable AWS covered-electrode class was found; the only confirmed route is GTAW/GMAW with AMS 5824 bare wire)
Seamless pipe · fittings
—
ASTM A564 for bar
— (coverage of S17700 by ASTM A564 could not be independently confirmed; specify AMS 5644 for bar)
Composition (ASTM A693): C ≤0.09% · Mn ≤1.00% · Si ≤1.00% · P ≤0.040% · S ≤0.030% · Cr 16.00–18.00% · Ni 6.50–7.75% · Al 0.75–1.50%. AISI Type 631, UNS S17700, EN 1.4568 and the trade name “17-7 PH” all denote the same grade; some catalogues list them as if they were different products.
What the Condition Letters Mean
STRENGTH BY AGEING CONDITION
DEFENCE METAL
Condition
Hardness
Yield MPa
Tensile MPa
Elongation
Condition A (sheet/strip/plate)
≤ HRB 92
≤ 379
≤ 1034
≥ 20%
Condition C (cold rolled)
≥ HRC 41
≥ 1207
≥ 1379
≥ 1%
TH 1050
≥ HRC 38
≥ 1034
≥ 1241
≥ 6% (≥ 5% in thin gauges)
RH 950
≥ HRC 44
≥ 1310
≥ 1448
4-6% (depending on thickness and form — see contradictions)
CH 900
≥ HRC 46
≥ 1586
≥ 1655
—
TH 1050
≥ HRC 38
≥ 965
≥ 1172
≥ 6%
RH 950
≥ HRC 41
≥ 1034
≥ 1276
≥ 6%
DEFENCE METAL
Condition A
Condition
Condition A
Tensile MPa
827-896
Yield MPa
276-310
Elongation
35%
Hardness
HRB 85
Source type
Producer typical value (range) — NOT a specification value
DEFENCE METAL
TH 1050
Condition
TH 1050
Tensile MPa
1345-1379
Yield MPa
1207-1276
Elongation
8-9%
Hardness
HRC 42-43
Source type
Producer typical value (range) — NOT a specification value
DEFENCE METAL
RH 950
Condition
RH 950
Tensile MPa
1550-1620
Yield MPa
1379-1517
Elongation
6-7%
Hardness
HRC 47-48
Source type
Producer typical value (range) — NOT a specification value
DEFENCE METAL
CH 900
Condition
CH 900
Tensile MPa
1827-2034
Yield MPa
1793-1896
Elongation
2%
Hardness
HRC 49-52
Source type
Producer typical value (range) — NOT a specification value
The two tables below MUST NOT BE MIXED. Table 1 gives SPECIFICATION MINIMUMS (ASTM A693 Type 631 and AMS 5528/5529 for sheet/strip/plate; ASTM A564 Type 631 and AMS 5644 for bar/forging). Table 2 gives PRODUCER TYPICAL VALUES, which are not specification values; they are shown as ranges because they differ between producers. Elongation minimums vary with thickness. Specification minimums and producer typical values are given in separate tables and must not be mixed. The minimums for sheet/strip/plate and for bar/forging are DIFFERENT: the same condition name (e.g. TH1050) means different numbers in the two forms. Elongation minimums depend on thickness; the CH900 elongation minimum is left blank because it could not be confirmed with four sources. The bar/forging rows do not meet the four-source threshold and are marked as such.
HEAT TREATMENT — SCHEMATIC
1 · SOLUTION TREATMENT
1066 ± 14 °C (1950 ± 25 °F) — sheet, strip, plate section dependent; bar/rod/wire bulletins give 30 minutes minimum
2 · COOL
air cool to room temperature
3 · AGEING
see the table below
DEFENCE METAL
Condition A (solution treated — as-delivered)
Step
Condition A (solution treated — as-delivered)
section dependent; bar/rod/wire bulletins give 30 minutes minimum
Cooling
air cool to room temperature
Result
The structure stays AUSTENITIC: ≤ 1034 MPa tensile, ≤ HRB 92, ≥ 20% elongation. Forming is done in this state.
Note
Bar/rod/wire bulletins give the annealing temperature as 1038 ± 14 °C (1900 ± 25 °F) — see contradictions.
DEFENCE METAL
TH 1050
Step
TH 1050
Summary
Condition A → 760 °C austenite conditioning → cool below 16 °C (Condition T) → 566 °C aging
Product forms
Sheet, strip, plate, bar, forging, tube
Mechanism
At 760 °C more carbon precipitates as chromium carbide; the martensite finish (Mf) temperature rises to about 16 °C (60 °F), so the material transforms to martensite on cooling without any cryogenic step.
Step 1 · Austenite conditioning
760 ± 14 °C (1400 ± 25 °F) · 90 minutes · cool to 16 °C (60 °F) or below within 1 hour, hold 30 minutes · Condition T
Step 2 · Precipitation aging
566 ± 5.5 °C (1050 ± 10 °F) · 90 minutes · air cool to room temperature · Condition TH 1050
DEFENCE METAL
RH 950
Step
RH 950
Summary
Condition A → 954 °C austenite conditioning (Condition A 1750) → −73 °C cryogenic (Condition R 100) → 510 °C aging
Product forms
Sheet, strip, plate, bar, forging, tube
Mechanism
At 954 °C less carbon precipitates than at 760 °C; the martensite finish temperature stays far below room temperature, so cryogenic cooling is MANDATORY to complete the transformation.
Step 1 · Austenite conditioning
954 ± 8 °C (1750 ± 15 °F) · 10 minutes · air cool to room temperature · Condition A 1750
Step 2 · Cryogenic transformation
−73 ± 5.5 °C (−100 ± 10 °F) · 8 hours · air warm to room temperature · Condition R 100
Step 3 · Precipitation aging
510 ± 5.5 °C (950 ± 10 °F) · 60 minutes · air cool to room temperature · Condition RH 950
DEFENCE METAL
CH 900
Step
CH 900
Summary
Condition C (mill cold rolled/drawn) → 482 °C aging
Product forms
Cold rolled sheet/strip and cold drawn wire only
Mechanism
The transformation is produced by cold work rather than by heat treatment, so a single low-temperature cycle is enough. Not applicable to plate, bar or forgings.
Step 1 · Starting state
— · — · — · Condition C: material transformed to martensite by cold work at the mill
Step 1 · Precipitation aging
482 ± 5.5 °C (900 ± 10 °F) · 60 minutes · air cool to room temperature · Condition CH 900
Schematic; the time axis is not to scale. No published TTT/CCT curve was used. Schematic; the time axis is not to scale. No published TTT/CCT curve was used. TH1050 and RH950 are SEPARATE PATHS; their steps are not interchangeable and must not be mixed. Condition A is AUSTENITIC; aging directly without austenite conditioning produces no hardening. In both paths the aging step ends with an air cool; there is no water or oil quench.
The condition designations are the most confusing feature of this grade. 17-7 PH cannot be aged directly: in Condition A the matrix is austenite and there is no martensite for the precipitates to form in. First comes an intermediate anneal called austenite conditioning, which precipitates chromium carbides at the grain boundaries, locally depleting the matrix of chromium and carbon and thereby raising the alloy’s martensite start and finish temperatures. Only then does the material transform to martensite and become ageable.
17-7 PH Conditions
DEFENCE METAL
Condition A
Solution annealed at about 1066 °C (1950 °F), air cooled. Austenitic, soft, formable, only weakly magnetic. The standard as-delivered condition
Condition C
Condition A material that has been cold rolled (sheet and strip). No thermal conditioning, no ageing
TH 1050 route
A → Condition T: conditioning anneal at 760 °C (1400 °F) for 90 min, then cooled to about 16 °C and held 30 min (no further cooling is needed because this temperature raises the martensite-finish point above room temperature) → age at 566 °C (1050 °F) for 90 min, air cool
RH 950 route
A → Condition A-1750: conditioning at 954 °C (1750 °F) for 10 min, air cool → Condition R-100: refrigerate to −73 °C (−100 °F) and hold 8 hours (this step is mandatory because the higher conditioning temperature leaves the martensite-finish point below room temperature) → age at 510 °C (950 °F) for 60 min, air cool
CH 900
Condition C (cold rolled) material aged at 482 °C (900 °F) for 60 min. There is no austenite-conditioning step — cold work substitutes for it
For material 0.25 mm and thinner the Condition A maximum yield is 448 MPa — a genuine thickness sub-clause, not an error
WARNING — two catalogue traps. (1) For this grade the “typical” mill values and the specification limits are different figures, and datasheets of different vintages diverge from each other as well. State which is which on anything customer-facing or contractual; the table above gives specification limits. (2) Copied tables have been observed with the RH 950, C and CH 900 rows shuffled. Quick check: hardness must always follow the order A < TH 1050 < RH 950 ≈ C < CH 900; if it does not, the table has been mis-transcribed.
Forming, Welding and Machining
Forming — the whole point of the grade
In Condition A, formability is comparable to Type 301: it deep-draws and bends with standard tooling. Because it work-hardens rapidly, intermediate anneals may be needed for complex or multi-stage drawing. Dimensional change on hardening must be designed in: the A → TH 1050 / RH 950 route gives a net expansion of about 0.004 in./in. (a transformation expansion of ~0.0045 in./in., partly offset by ~0.0005 in./in. of contraction during ageing); the C → CH 900 route gives a contraction of about 0.0005 in./in.
Welding
GTAW/GMAW and resistance welding are usable, and parts are normally welded in Condition A. Weldability is poorer than that of 17-4 PH: the 0.75–1.5% aluminium oxidises readily in the weld pool, degrading penetration and producing oxide or slag, so inert-gas shielding is essential. The matching filler is AMS 5824 (UNS S17780). The full austenite-conditioning and ageing sequence must be re-applied after welding — otherwise the HAZ and weld metal remain unhardened. No verified preheat or interpass temperature was found for this grade.
Machining
Machinability is about 75% of B1112. Chips are long and gummy, so chip breakers, slow speeds and steady feeds are needed. Bulk machining is normally done in Condition A (the softest state); where critical dimensions must hold in the hardened state, finish machining is left until after heat treatment — standard practice for precipitation-hardening grades.
Applications and Limits
17-7 PH · Properties and Comparison
DEFENCE METAL
Service temperature
About 427 °C (800 °F) for structural and sheet applications. Lower for spring wire: roughly 315–343 °C
Corrosion
Good in fresh water and mild industrial atmospheres; not recommended for salt water or reducing environments. A quantitative comparison with 301/304 or 17-4 PH could not be verified
Magnetic response
Condition A is only weakly magnetic (relative permeability ~1.4–3.6); after conditioning and ageing it becomes strongly magnetic (TH 1050 ~120–208, RH 950 ~119–135, CH 900 ≤125). This gives a practical magnet test to separate hardened from unhardened parts — though Condition A is not strictly non-magnetic
Typical applications
Flat springs, Belleville washers, diaphragms, bellows, eyelets, aerospace sheet parts
Martensitic rather than semi-austenitic: it hardens in a single ageing step from the as-received condition, with no austenite conditioning and no sub-zero treatment, and has better weldability. In exchange, it cannot be deep-drawn the way Condition A 17-7 PH can
Frequently Asked Questions
Should I order TH 1050 or RH 950?
Both start from the same Condition A stock and diverge at the austenite-conditioning temperature (760 °C versus 954 °C), giving different strength/toughness trade-offs. By the specification limits, RH 950 gives higher guaranteed strength (tensile ≥1448 MPa, yield ≥1310 MPa, ≥44 HRC), while TH 1050 stops at ≥1241 MPa tensile and ≥1034 MPa yield (≥38 HRC); minimum elongation is 6% for both. Where maximum strength and hardness matter (springs, fasteners), order RH 950. TH 1050’s lower conditioning temperature and simpler cooling regime — there is no −73 °C sub-zero step — reduce distortion risk and heat-treatment logistics, so where toughness and dimensional consistency matter more than the last 15% of strength, TH 1050 is the easier choice.
Why must I order Condition A if the part will be formed?
Because Condition A is the only condition in this grade that is still austenitic and ductile — it deep-draws, bends and forms comparably to Type 301. Every other condition (C, CH 900, TH 1050, RH 950) has either been cold worked or transformed to martensite and aged, and is correspondingly hard, limited in ductility and unsuitable for significant forming. That is precisely why this semi-austenitic grade is chosen over a fully martensitic PH steel: form the part cold while it is still austenitic, then heat-treat it to final spring or structural strength. So whenever forming is downstream, the mill condition ordered must be Condition A.
How much dimensional change should I plan for during heat treatment?
Per the mill’s own data, the A → TH 1050 / RH 950 route produces a net expansion of about 0.004 in./in.: the transformation to martensite gives about 0.0045 in./in. of expansion, partly offset by roughly 0.0005 in./in. of contraction from precipitation during ageing. The C → CH 900 route produces a small contraction of about 0.0005 in./in. Build these figures into tolerances and fixture allowances before heat treatment: parts that must hold tight dimensions afterwards are either formed deliberately over- or undersize to compensate, or finish-machined after the heat-treat cycle rather than before it.