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Stainless Steel 1.4922 +N (Normalized)

Heat-treated state

EN 1.4922

Intermediate mill condition for forgings/tubes; because of the high hardenability it is essentially air-hardened and must be tempered before service.

Premium cost $$$

Values for the +N condition

Other 1.4922 tempers and conditions

1.4922 is listed in 6 conditions; see the grade overview at 1.4922.

Compare all 6 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Softest supply state for heavy machining, deep drilling or cold straightening before final hardening.4307202017 HRC—
+QT700Default
Quenched and tempered ~730–780 °C, Rm 690–840 MPa
Default delivery condition for boiler tubes, pipe, forgings and rotors operating with creep loading up to ~565 °C.5607601822 HRC—
Quenched and tempered ~700–720 °C, Rm 800–950 MPa
Higher-strength condition for high-temperature bolting, flanges and valve stems where Rp0.2 ≥600 MPa is required.7008701527 HRC—
Quenched and tempered ~650–690 °C, Rm 900–1050 MPa
Maximum practical strength for turbine blades and short-time-loaded parts; toughness and long-term creep stability are reduced.8009701331 HRC—
+NThis page
Normalized
Intermediate mill condition for forgings/tubes; because of the high hardenability it is essentially air-hardened and must be tempered before service.9501,300843 HRC2.7 % IACS
Hardened (austenitize 1020–1070 °C, oil/air quench), untempered
As-quenched state only — brittle and highly stressed; temper immediately, never use as delivered condition.1,1001,450646 HRC2.7 % IACS

What is 1.4922 +N?

1.4922 +N is 1.4922 heat treated to +N — intermediate mill condition for forgings/tubes; because of the high hardenability it is essentially air-hardened and must be tempered before service. 1.4922 +N has a yield strength of 950 MPa (138 ksi) and a tensile strength of 1,300 MPa (189 ksi) — stronger than 98% of stainless steel grades. Elongation at break is 8% and the elastic modulus is 216 GPa (31.3 Msi). 1.4922 +N has a density of 7.7 g/cm³ (0.278 lb/in³), lighter than 83% of stainless steel grades. It melts at 1,425°C (2,597 °F). +QT700 is the default condition FabDigit quotes; +N is available on request or by drawing note.

Advantages

  • High strength — 950 MPa (138 ksi), better than 98% of stainless steel grades
  • Low embodied carbon — 3.5 kg CO₂/kg, better than 88% of stainless steel grades
  • Conducts heat well — 23.5 W/m·K (13.6 BTU/hr·ft·°F), better than 79% of stainless steel grades
  • High electrical conductivity — 2.7 % IACS, better than 78% of stainless steel grades

Limitations

  • Limited ductility — 8%, worse than 99% of stainless steel grades
  • Low fracture toughness — 32 MPa·√m (29.1 ksi·√in), worse than 99% of stainless steel grades
  • Limited formability — 5/100, worse than 99% of stainless steel grades
  • Difficult to machine — 20/100, worse than 98% of stainless steel grades
  • Difficult to weld — 15/100, worse than 98% of stainless steel grades

1.4922 +N properties

Typical room-temperature values for 1.4922 +N; 22 are specific to this condition. Other listed values are 1.4922 reference data and may not represent this condition. Bars are the position among stainless steel grades.

Physical3

1.4922 +N has a density of 7.7 g/cm³ (0.278 lb/in³), lighter than 83% of stainless steel grades. It melts at 1,425°C (2,597 °F).

Density7.7 g/cm³0.28 lb/in³
Melting Point (Solidus)1,425°C2,597 °F
Liquidus Temperature1,500°C2,732 °F

Mechanical16

1.4922 +N has a yield strength of 950 MPa (138 ksi) and a tensile strength of 1,300 MPa (189 ksi) — stronger than 98% of stainless steel grades. Elongation at break is 8% and the elastic modulus is 216 GPa (31.3 Msi).

Elastic (Young's) Modulus216 GPa31.3 Msi
Shear Modulus84 GPa12.2 Msi
Bulk Modulus165 GPa23.9 Msi
Poisson's Ratio0.29
Tensile Strength (Ultimate)1,300 MPa189 ksi
Yield Strength (0.2% offset)950 MPa138 ksi
Elongation at Break8%
Reduction in Area28%
Compressive Strength980 MPa142 ksi
Shear Strength780 MPa113 ksi
Fatigue Strength (Endurance Limit)550 MPa79.8 ksi
Fracture Toughness (K_IC)32 MPa·√m29.1 ksi·√in
Charpy V-Notch Impact (RT)12 J8.9 ft·lbf
Hardness, Brinell400 HB
Hardness, Rockwell C43 HRC
Hardness, Vickers420 HV

Thermal6

1.4922 +N is rated for continuous service to 400°C (752 °F). It conducts heat at 23.5 W/m·K (13.6 BTU/hr·ft·°F), better than 79% of stainless steel grades. Thermal expansion is 10.8 µm/m·K (6 µin/in·°F).

Thermal Conductivity23.5 W/m·K13.6 BTU/hr·ft·°F
Specific Heat Capacity460 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)10.8 µm/m·K6 µin/in·°F
Latent Heat of Fusion260 J/g112 BTU/lb
Max Service Temperature (continuous)400°C752 °F
Min Service Temperature-20°C-4 °F

Electrical3

1.4922 +N conducts electricity at 2.7 % IACS, better than 78% of stainless steel grades.

Electrical Conductivity2.7 % IACS
Electrical Resistivity6.4×10⁻⁷ Ω·m25.2 µΩ·in
Magnetic Responseferromagnetic

Chemical & Environmental3

Corrosion resistance is fair (36/100), worse than 96% of stainless steel grades.

Galvanic Potential (seawater, vs SCE)-0.3 V
Corrosion ResistanceFair36/100
Chemical Resistance SummaryResists steam, dry combustion gases and mild atmospheric attack up to ~600 °C; will rust in wet/condensate service, and is not resistant to chlorides, seawater or reducing acids. Best corrosion behaviour in the tempered-and-polished condition.

Sustainability4

Producing a kilogram of 1.4922 +N takes about 50 MJ of energy and emits 3.5 kg of CO₂ — less than 80% of stainless steel grades. Typical recycled content is 45%.

Embodied Energy (primary production)50 MJ/kg21,496 BTU/lb
Embodied Carbon (primary production)3.5 kg CO₂/kg
Embodied Water180 L/kg21.6 gal/lb
Typical Recycled Content45%

Manufacturability6

1.4922 +N's machinability is poor (20/100, worse than 98% of stainless steel grades); weldability poor (15/100); formability not recommended (5/100).

MachinabilityPoor20/100
Machinability Rating (AISI 1212 = 100 %)20%
WeldabilityPoor15/100
Formability (cold)Not recommended5/100
Brazeability / SolderabilityPoor30/100
PolishabilityGood60/100

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with 1.4922 +N

Is 1.4922 easy to machine?

Machine in the annealed or +QT700 state with rigid setups, sharp carbide tooling, low-to-moderate speed and generous coolant; work-hardening and gummy chips above ~28 HRC.

Can 1.4922 be welded?

Weldable with matched 12Cr-Mo-V filler (or Ni-base for dissimilar joints) but requires 300–400 °C preheat/interpass, no cooling below Ms before PWHT, and 730–760 °C tempering to restore toughness.

Can 1.4922 be formed, bent or molded?

Hot form at 1100–850 °C followed by slow cool/anneal; cold forming is limited to gentle bends in the annealed condition.

What surface finishes work on 1.4922?

Takes a good ground/polished finish; passivation or light chrome/nitride treatment improves wet-service rust resistance, and shot peening is common on blade roots.

1.4922 chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
C0.17 – 0.230.2
Si0.1 – 0.50.3
Mn0.3 – 0.80.55
P≤ 0.03—
S≤ 0.02—
Cr10 – 12.511.3
Mo0.8 – 1.21
Nicontrols delta ferrite / toughness0.3 – 0.80.55
V0.25 – 0.350.3
Febalance—

1.4922 +N — frequently asked

What is 1.4922 +N used for?

1.4922 +N is typically used for steam turbine rotors and blades, high-temperature bolts, boiler components and power plant valves. In short: best-machining 12Cr creep steel; proven turbine rotor grade; service to 565 °C.

What is the yield strength of 1.4922 +N?

1.4922 +N has a typical yield strength of 950 MPa (138 ksi) and a tensile strength of 1,300 MPa (189 ksi) — stronger than 98% of stainless steel grades. Strength varies by condition: see the 6 listed tempers.

Is 1.4922 +N easy to machine?

Not especially — machinability is rated poor (20/100, worse than 98% of stainless steel grades). Machine in the annealed or +QT700 state with rigid setups, sharp carbide tooling, low-to-moderate speed and generous coolant; work-hardening and gummy chips above ~28 HRC.

Can 1.4922 +N be welded?

Not readily — weldability is rated poor (15/100). Weldable with matched 12Cr-Mo-V filler (or Ni-base for dissimilar joints) but requires 300–400 °C preheat/interpass, no cooling below Ms before PWHT, and 730–760 °C tempering to restore toughness.

What surface finishes work on 1.4922 +N?

Takes a good ground/polished finish; passivation or light chrome/nitride treatment improves wet-service rust resistance, and shot peening is common on blade roots.

Can 1.4922 +N be formed, bent or molded?

Hot form at 1100–850 °C followed by slow cool/anneal; cold forming is limited to gentle bends in the annealed condition.

What is the maximum service temperature of 1.4922 +N?

1.4922 +N is rated for continuous use to about 400°C (752 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

Sources

  1. DIN 17175 — Seamless tubes of heat-resistant steels (X20CrMoV12-1) — DIN (1979)
  2. EN 10302 — Creep resisting steels, nickel and cobalt alloys — CEN (2008)
  3. EN 10222-2 — Steel forgings for pressure purposes: ferritic and martensitic steels with specified elevated temperature properties — CEN (2021)
  4. GB/T 1221 — Heat-resisting steel bars (1Cr11MoV) — SAC (2007)
  5. ASM Handbook Vol. 1 — Properties and Selection: Irons, Steels and High-Performance Alloys — ASM International (1990)
  6. ASM Handbook Vol. 13B — Corrosion: Materials — ASM International (2005)
  7. X20CrMoV11-1 (1.4922) heat-resisting steel data sheet — European special steel producer (2020)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.