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Stainless Steel 1.4877

EN 1.4877

EN 1.4877 (X6NiCrNbCe32-27) is a niobium- and cerium-stabilised 32Ni-27Cr austenitic heat-resistant alloy engineered for high-temperature strength and carburisation resistance up to about 1100 °C.

High cost $$$$

Reference datasheet — 1.4877 is not in the instant-quote catalog. Upload your part and an engineer will quote it in this grade or suggest the closest stocked equivalent.

Values for the SA condition

1.4877 tempers and conditions

1.4877 is supplied in 5 conditions, soft to hard. SA is the default FabDigit quotes; the values on this page are for it.

Compare all 5 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Forged bar/ring, solution annealed
For furnace rolls, hangers, grate bars and machined fittings needing large section sizes.25058035165 HB1.7 % IACS
Hot finished seamless tube, solution annealed and pickled
Choose for superheater, reheater and furnace tubing in the usual hot-finished sizes to EN 10216-2 / EN 10095.25559040170 HB1.7 % IACS
SADefault
Solution annealed
Standard delivery condition for tube, plate and bar: maximum ductility, homogeneous austenite with Nb carbides in solution/finely dispersed.26060040170 HB1.7 % IACS
Cold drawn then solution annealed
Use where tight dimensional tolerance and smooth bore are needed with fully annealed properties.27061038175 HB1.7 % IACS
Cold worked
Only for room-temperature strength or spring-like stiffness in small sections; not for creep service, since cold work is lost above ~600 °C.5508002024 HRC1.7 % IACS

Supply forms, finishes and certifications

Ways 1.4877 is supplied — form, process route, surface or paperwork — without a datasheet of their own. The property values above apply.

OptionWhat it isType
PLATE-SA
Hot rolled plate/sheet, solution annealed and descaledSupply form

What is 1.4877?

EN 1.4877 (X6NiCrNbCe32-27) is a niobium- and cerium-stabilised 32Ni-27Cr austenitic heat-resistant alloy engineered for high-temperature strength and carburisation resistance up to about 1100 °C. It is supplied as solution-annealed plate, bar, forgings, hot-finished and cold-drawn product with 260 MPa yield, 600 MPa tensile, 40% elongation and about 170 HB (86 HRB), and is chosen where 800H-class alloys run short on carburisation life. The high nickel content makes it costly and difficult to machine (score 25); Alloy 800H / 1.4876 is the cheaper option for milder furnace service. 1.4877 has a density of 7.9 g/cm³ (0.285 lb/in³), heavier than 68% of stainless steel grades. It melts at 1,340°C (2,444 °F). 1.4877 has a yield strength of 260 MPa (37.7 ksi) and a tensile strength of 600 MPa (87 ksi) — weaker than 84% of stainless steel grades. Elongation at break is 40% and the elastic modulus is 195 GPa (28.3 Msi).

What is 1.4877 used for?

  • furnace muffles
  • ethylene cracking components
  • high-temperature fasteners

Advantages

  • High service temperature — 1,100°C (2,012 °F), better than 96% of stainless steel grades

Limitations

  • Poor heat conductor — 11.5 W/m·K (6.64 BTU/hr·ft·°F), worse than 97% of stainless steel grades
  • High embodied carbon — 7.5 kg CO₂/kg, worse than 97% of stainless steel grades
  • Low electrical conductivity — 1.7 % IACS, worse than 93% of stainless steel grades
  • Difficult to machine — 25/100, worse than 88% of stainless steel grades
  • Low strength — 260 MPa (37.7 ksi), worse than 84% of stainless steel grades

1.4877 properties

Typical room-temperature values for 1.4877-SA; bars are the position among stainless steel grades.

Physical3

1.4877 has a density of 7.9 g/cm³ (0.285 lb/in³), heavier than 68% of stainless steel grades. It melts at 1,340°C (2,444 °F).

Density7.9 g/cm³0.29 lb/in³
Melting Point (Solidus)1,340°C2,444 °F
Liquidus Temperature1,390°C2,534 °F

Mechanical15

1.4877 has a yield strength of 260 MPa (37.7 ksi) and a tensile strength of 600 MPa (87 ksi) — weaker than 84% of stainless steel grades. Elongation at break is 40% and the elastic modulus is 195 GPa (28.3 Msi).

Elastic (Young's) Modulus195 GPa28.3 Msi
Shear Modulus75 GPa10.9 Msi
Bulk Modulus160 GPa23.2 Msi
Poisson's Ratio0.29
Tensile Strength (Ultimate)600 MPa87 ksi
Yield Strength (0.2% offset)260 MPa37.7 ksi
Elongation at Break40%
Reduction in Area55%
Compressive Strength265 MPa38.4 ksi
Shear Strength400 MPa58 ksi
Fatigue Strength (Endurance Limit)250 MPa36.3 ksi
Charpy V-Notch Impact (RT)130 J95.9 ft·lbf
Hardness, Brinell170 HB
Hardness, Rockwell B86 HRB
Hardness, Vickers180 HV

Thermal6

1.4877 is rated for continuous service to 1,100°C (2,012 °F). It conducts heat at 11.5 W/m·K (6.64 BTU/hr·ft·°F), worse than 97% of stainless steel grades. Thermal expansion is 15 µm/m·K (8.33 µin/in·°F).

Thermal Conductivity11.5 W/m·K6.6 BTU/hr·ft·°F
Specific Heat Capacity470 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)15 µm/m·K8.3 µin/in·°F
Latent Heat of Fusion285 J/g123 BTU/lb
Max Service Temperature (continuous)1,100°C2,012 °F
Min Service Temperature-196°C-321 °F

Electrical3

1.4877 conducts electricity at 1.7 % IACS, worse than 93% of stainless steel grades.

Electrical Conductivity1.7 % IACS
Electrical Resistivity1×10⁻⁶ Ω·m39.4 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is very good (72/100), better than 73% of stainless steel grades.

Galvanic Potential (seawater, vs SCE)-0.1 V
Corrosion ResistanceVery good72/100
Chemical Resistance SummaryOutstanding resistance to high-temperature oxidation, carburization, nitriding and sulphur-bearing flue gases up to ~1100 °C; good in hot dilute acids and caustics, but chloride pitting/crevice resistance is only moderate because the alloy contains no molybdenum.

Sustainability4

Producing a kilogram of 1.4877 takes about 110 MJ of energy and emits 7.5 kg of CO₂ — more than 99% of stainless steel grades. Typical recycled content is 45%.

Embodied Energy (primary production)110 MJ/kg47,292 BTU/lb
Embodied Carbon (primary production)7.5 kg CO₂/kg
Embodied Water150 L/kg18 gal/lb
Typical Recycled Content45%

Manufacturability7

1.4877's machinability is poor (25/100, worse than 88% of stainless steel grades); weldability good (68/100); formability good (62/100).

MachinabilityPoor25/100
Machinability Rating (AISI 1212 = 100 %)28%
WeldabilityGood68/100
Formability (cold)Good62/100
Brazeability / SolderabilityGood55/100
PolishabilityVery good70/100
Anodizing Responsen/a — not an anodizable alloy; use pickling and passivation or electropolishing instead

Common Calculations5

Specific Strength (UTS / density)calculated76 kN·m/kg
Specific Stiffness (E / density)calculated24.7 MN·m/kg
Modulus of Resiliencecalculated173 kJ/m³
Thermal Diffusivitycalculated3.1 mm²/s
Thermal Shock Resistance Indexcalculated2

Values are nominal handbook figures for design screening. Certified mill or lot data ships with every FabDigit order on request.

Strength versus weight in the stainless steel family

Yield strength against density for every stainless steel grade FabDigit runs. 1.4877 is highlighted; hover a dot for its name, or open the interactive family chart.

3005007001,0001,5002,0007.27.47.67.888.2Density (g/cm³)Yield strength (MPa) — log scale1.4877

Working with 1.4877

Is 1.4877 easy to machine?

Machine like Alloy 800H/803: rigid setups, sharp positive-rake carbide, low speed (20–40 m/min) with heavy constant feed and copious coolant to avoid work-hardened glaze.

Can 1.4877 be welded?

Weldable by GTAW/SMAW/GMAW with Ni-base or matching high-Ni filler (e.g. ERNiCr-3 / Alloy 82 type); keep heat input low, no preheat, interpass below ~150 °C, avoid excessive dilution to limit hot cracking.

Can 1.4877 be formed, bent or molded?

Hot work at 1150–950 °C then solution anneal; cold forming is possible but the alloy work-hardens rapidly so allow extra power, generous radii and intermediate annealing at 1050–1120 °C.

1.4877 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
Ccarbon level set for creep strength0.04 – 0.080.06
Si≤ 0.30.2
Mn≤ 10.6
P≤ 0.03—
S≤ 0.02—
Croxidation/carburization resistance26 – 2827
Niaustenite stability, carburization resistance31 – 3332
Nbstabilizer, precipitation strengthening0.6 – 10.8
Ceimproves scale adherence and creep life0.05 – 0.10.07
Al≤ 0.03—
Ti≤ 0.05—
Febalance, approx. 36–40 %balance—

What surface finishes work on 1.4877?

Pickle and passivate or grind/blast to remove high-temperature scale before service; can be electropolished, but it is not anodizable and rarely plated.

Surface treatments FabDigit runs on stainless steel parts — pick them in the quote configurator or call them out on the drawing. Each links to its datasheet in the surface-finish library (thickness, specs, call-out, material verdicts).

Equivalent designations

Standards and trade names that resolve to Stainless Steel 1.4877 in FabDigit's catalog. Equivalence is nominal — check the exact specification when certification matters.

EN / DIN / Werkstoff-Nr.
X6NiCrNbCe32-27

How much does 1.4877 cost?

1.4877 is a high-cost stainless steel ($$$$), pricier than about 78% of the materials FabDigit quotes. Part price depends far more on geometry, tolerance and quantity than on the raw stock — upload a CAD file for a live quote.

1.4877 — frequently asked

What is 1.4877 used for?

1.4877 is typically used for furnace muffles, ethylene cracking components and high-temperature fasteners. In short: top carburisation resistance; nb/Ce-stabilised for creep strength; above 800H in service life.

What is the yield strength of 1.4877?

1.4877 has a typical yield strength of 260 MPa (37.7 ksi) and a tensile strength of 600 MPa (87 ksi) — weaker than 84% of stainless steel grades. Strength varies by condition: see the 5 listed tempers.

Is 1.4877 easy to machine?

Not especially — machinability is rated poor (25/100, worse than 88% of stainless steel grades). Machine like Alloy 800H/803: rigid setups, sharp positive-rake carbide, low speed (20–40 m/min) with heavy constant feed and copious coolant to avoid work-hardened glaze.

Can 1.4877 be welded?

Yes — weldability is rated good (68/100). Weldable by GTAW/SMAW/GMAW with Ni-base or matching high-Ni filler (e.g. ERNiCr-3 / Alloy 82 type); keep heat input low, no preheat, interpass below ~150 °C, avoid excessive dilution to limit hot cracking.

What surface finishes work on 1.4877?

Pickle and passivate or grind/blast to remove high-temperature scale before service; can be electropolished, but it is not anodizable and rarely plated.

Can 1.4877 be formed, bent or molded?

Hot work at 1150–950 °C then solution anneal; cold forming is possible but the alloy work-hardens rapidly so allow extra power, generous radii and intermediate annealing at 1050–1120 °C.

What is the maximum service temperature of 1.4877?

1.4877 is rated for continuous use to about 1,100°C (2,012 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between 1.4877-SA and 1.4877-CW?

SA is the default condition — standard delivery condition for tube, plate and bar: maximum ductility, homogeneous austenite with Nb carbides in solution/finely dispersed. CW: only for room-temperature strength or spring-like stiffness in small sections; not for creep service, since cold work is lost above ~600 °C. Yield strength is 260 MPa in SA versus 550 MPa in CW.

How much does 1.4877 cost?

1.4877 is a high-cost stainless steel ($$$$), pricier than about 78% of the materials FabDigit quotes. Part price depends far more on geometry, tolerance and quantity than on the raw stock — upload a CAD file for a live quote.

Sources

  1. EN 10095 — Heat resisting steels and nickel alloys — CEN (2018)
  2. EN 10216-2 — Seamless steel tubes for pressure purposes, elevated temperature grades — CEN (2020)
  3. Nicrofer 3228 NbCe / Alloy 803 alloy data — VDM Metals (2018)
  4. ASM Handbook Vol. 1 — Properties and Selection: Irons, Steels, and High-Performance Alloys — ASM International (1990)
  5. ASM Handbook Vol. 13B — Corrosion: Materials — ASM International (2005)

Property data is compiled from published supplier and standards handbooks and normalised for comparison; hardness values on non-Brinell scales are converted approximately for charting only. Manufacturability limits are FabDigit quote-engine defaults and may be relaxed by engineering review. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.