X5CrNiCuNb16-4 (17-4PH)

17-4PH β€” most widely used PH stainless. Rm up to 1310 MPa in H900. Combines stainless corrosion resistance with high-strength alloy steel mechanical properties.

Stainless Steels Precipitation-Hardening Stainless Steel ENX5CrNiCuNb16-4 DIN1.4542 AISI/SAE630 / 17-4PH ASTMA564 Type 630 / A693 / A705 +11
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Description

X5CrNiCuNb16-4 (EN 1.4542 / UNS S17400 / AISI 630) is a martensitic precipitation-hardening stainless steel. Its unique strengthening mechanism β€” precipitation of copper-rich intermetallic particles during aging β€” allows properties to be tailored across a wide range by selecting the aging temperature. Solution-annealed (Condition A) material is relatively soft (HRC ~28-32) and readily machined; after aging at 482 C (H900) it reaches Rm >1310 MPa with HRC 40-44, approaching high-strength alloy steels. Corrosion resistance is comparable to AISI 304 in most environments. Per Sandmeyer Steel / ASTM A564 data.

Key Properties β€” Condition A β€” Solution Annealed
Rm (Tensile Strength)
930 – 1,100
MPa
Re / Rp0.2 (Yield)
580 – 860
MPa
Aβ‚… (Elongation)
β‰₯ 16.0
%
Hardness
β€” – 321
HB
E (Young's Modulus)
193
GPa
Density
7.80
g/cmΒ³
Main Designations (15)
Standard BodyDesignationCountry / RegionNote
EN X5CrNiCuNb16-4 European Union
DIN 1.4542 Germany
AISI/SAE 630 / 17-4PH USA
ASTM A564 Type 630 / A693 / A705 USA
AMS AMS 5604 (bar/billet) / AMS 5622 (plate/sheet) USA (Aerospace)
UNS S17400 USA (UNS)
BS EN 1.4542 UK
JIS SUS630 Japan
GOST 09H17N7YU2 (09Kh17N7YU2) Russia / CIS
UNI X5CrNiCuNb16-4 Italy
NF Z7CNU17-04 France
ISO X5CrNiCuNb16-4 (ISO 15510) International
GB 0Cr17Ni4Cu4Nb China
JUS C.4542 Yugoslavia / Serbia PH martensitic stainless steel; JUS C.B2.090
API API 6A 17-4PH International
Standards (15)
#Standard BodyDesignationCountry / RegionNote
1 EN X5CrNiCuNb16-4 European Union β€”
2 DIN 1.4542 Germany β€”
3 AISI/SAE 630 / 17-4PH USA β€”
4 ASTM A564 Type 630 / A693 / A705 USA β€”
5 AMS AMS 5604 (bar/billet) / AMS 5622 (plate/sheet) USA (Aerospace) β€”
6 UNS S17400 USA (UNS) β€”
7 BS EN 1.4542 UK β€”
8 JIS SUS630 Japan β€”
9 GOST 09H17N7YU2 (09Kh17N7YU2) Russia / CIS β€”
10 UNI X5CrNiCuNb16-4 Italy β€”
11 NF Z7CNU17-04 France β€”
12 ISO X5CrNiCuNb16-4 (ISO 15510) International β€”
13 GB 0Cr17Ni4Cu4Nb China β€”
14 JUS C.4542 Yugoslavia / Serbia PH martensitic stainless steel; JUS C.B2.090
15 API API 6A 17-4PH International β€”
All values in wt.%
C
Carbon
≀ 0.0700
Mn
Manganese
≀ 1.0000
Si
Silicon
≀ 1.0000
Cr
Chromium
15.0000 – 17.5000
Ni
Nickel
3.0000 – 5.0000
Cu
Copper
3.0000 – 5.0000
Nb
Niobium (+ Ta)
0.1500 – 0.4500
P
Phosphorus
≀ 0.0400
ElementSymbolMin %Max %Typical %
Carbon C β€” 0.0700 0.0400
Manganese Mn β€” 1.0000 0.6000
Silicon Si β€” 1.0000 0.5000
Chromium Cr 15.0000 17.5000 16.5000
Nickel Ni 3.0000 5.0000 4.0000
Copper Cu 3.0000 5.0000 4.0000
Niobium (+ Ta) Nb 0.1500 0.4500 0.2800
Phosphorus P β€” 0.0400 β€”
Mechanical Properties
ConditionCode Rm min
MPa
Rm max
MPa
Re min
MPa
Re max
MPa
Aβ‚… min
%
Z
%
KV
J
HB minHB max HRC minHRC max E
GPa
Condition A β€” Solution Annealed +A 930 1,100 580 860 16.0 β€” β€” β€” 321 28.0 34.0 193.0
H900 β€” Aged 482 C / 1h H900 1,170 1,380 1,070 1,240 8.0 β€” β€” β€” β€” 40.0 44.0 197.0
H925 β€” Aged 496 C / 4h H925 1,170 1,310 1,000 1,170 8.0 β€” β€” β€” β€” 38.0 42.0 197.0
H1025 β€” Aged 552 C / 4h H1025 1,070 1,170 1,000 1,070 12.0 β€” 60.0 β€” β€” 35.0 38.0 197.0
H1075 β€” Aged 579 C / 4h H1075 1,000 1,100 862 1,000 13.0 β€” β€” β€” β€” 32.0 36.0 197.0
H1150 β€” Aged 621 C / 4h H1150 862 1,000 793 930 14.0 β€” β€” β€” β€” 28.0 32.0 197.0
Physical Properties
Density
7.800
g/cmΒ³
Melting Point
1404–1440
Β°C
Young's Modulus
197.0
GPa
Poisson's Ratio
0.272
β€”
Thermal Conductivity
16.3
W/mΒ·K
Thermal Expansion
10.80
Γ—10⁻⁢ /K
Specific Heat
460
J/kgΒ·K
Electrical Resistivity
0.7700
¡Ω·m
Magnetic
Yes
 
Heat Treatment
Solution Annealing (Condition A)
Temperature:1038Β°C – 1038Β°C
Medium:Air or oil quench to <32 C
Duration:30 min at temp
Cooling:Rapid quench β€” below 32 C
Hardness After:HRC 28-32
Supplied in this condition. NEVER use in Condition A without aging β€” low toughness, SCC risk.
Aging H900 (max strength)
Temperature:482Β°C – 482Β°C
Medium:Air oven
Duration:1 h
Cooling:Air cool
Hardness After:HRC 40-44 / Rm >1170 MPa
Maximum strength. Higher SCC risk in chloride environments. Standard for aerospace structural parts.
Aging H925 (balance)
Temperature:496Β°C – 496Β°C
Medium:Air oven
Duration:4 h
Cooling:Air cool
Hardness After:HRC 38-42
Good strength-toughness balance. Aerospace and defence fasteners.
Aging H1025 (best balance)
Temperature:552Β°C – 552Β°C
Medium:Air oven
Duration:4 h
Cooling:Air cool
Hardness After:HRC 35-38
Best overall balance of strength, toughness and SCC resistance. Recommended for most structural applications.
Aging H1150 (max toughness)
Temperature:621Β°C – 621Β°C
Medium:Air oven
Duration:4 h
Cooling:Air cool
Hardness After:HRC 28-32
Maximum ductility and SCC resistance. Lower strength β€” for marine and offshore.
Machinability
Machinability Rating
relative to AISI B1112 = 100%
40.0%
Difficult
Turning Speed (HSS)
20
m/min
Turning Speed (Carbide)
95
m/min
Feed Rate (Turning)
0.120
mm/rev
Drilling Speed (HSS)
10
m/min
Milling Speed (Carbide)
98
m/min
CoolantFlood coolant or cutting oil β€” mandatory
Chip FormationShort-medium chips; work-hardening in Condition A
Tool MaterialMachine in Cond.A: TiAlN carbide positive rake; after aging: CBN or grinding preferred
Surface FinishRa 0.4-1.6 um (Cond.A); ground finish (hardened)
Machine in Condition A for efficiency. Post-machining age hardens the finished part. Machinability in Cond.A similar to 304 SS β€” use same approach. Rating ~40% vs B1112.
Applications
Aerospace
Structural fittings, bulkheads, pump housings, valve bodies and fasteners (H900/H925 conditions).
Oil & Gas
Christmas tree valves, wellhead connectors, gate valve stems and subsea fasteners (H1025/H1150 per NACE).
Food & Beverage
Food processing machinery parts requiring high strength and moderate corrosion resistance.
Medical
Surgical instruments, bone screws and orthopaedic device components.
Technical Notes
βœ…
Condition Selection
H900: max strength, use for aerospace non-corrosive environments. H1025: standard engineering β€” best balance. H1150: marine/sour service β€” max SCC resistance. NEVER use Condition A in service.
⚠️
SCC in H900
In warm chloride environments (>50 C, >1000 ppm Cl-), H900 condition is susceptible to SCC. Always specify H1025 or H1150 for marine, offshore or saline service.
πŸ”₯
Weldability
Good. Weld in Cond.A. Use filler ER630 (17-4PH). No pre-heat required. Post-weld age-harden to desired condition.