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Stainless Steel 1.4958 CR-A

Finish state

EN 1.4958 · UNS N08810 · also Incoloy 800H

CR-A = cold rolled sheet/strip, annealed

Thin gauge sheet and strip for furnace muffles, radiant tubes and formed components requiring a smooth surface.

High cost $$$$

Values for the CR-A condition

Other 1.4958 tempers and conditions

1.4958 is listed in 6 conditions; see the grade overview at 1.4958.

Compare all 6 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Forged and solution annealed
Heavy forged sections for headers, flanges and pigtail fittings in reformer service; grain size controlled for creep design.21551040145 HB1.7 % IACS
SADefault
Solution annealed
Standard supply condition for plate, tube and pipe used in creep-range service; gives the coarse grain required for 800H creep properties.22052045140 HB—
Cold drawn then solution annealed bar/tube
Precision seamless tube and bright bar restored to full 800H creep condition after cold drawing.22552045140 HB1.7 % IACS
Hot rolled plate, solution annealed and pickled
Heavy plate for furnace retorts, headers and pressure parts; slightly higher strength than thin annealed product.24054042150 HB1.7 % IACS
CR-AThis page
Cold rolled sheet/strip, annealed
Thin gauge sheet and strip for furnace muffles, radiant tubes and formed components requiring a smooth surface.25055045145 HB1.7 % IACS
Cold drawn
Choose for close-tolerance bar and small-bore tubing where higher room-temperature strength and better surface finish are wanted; not for long-term creep service without re-anneal.4006203011 HRC1.7 % IACS

What is 1.4958 CR-A?

1.4958 CR-A is 1.4958 supplied in the CR-A condition — thin gauge sheet and strip for furnace muffles, radiant tubes and formed components requiring a smooth surface. 1.4958 CR-A has a yield strength of 250 MPa (36.3 ksi) and a tensile strength of 550 MPa (79.8 ksi) — weaker than 91% of stainless steel grades. Elongation at break is 45% and the elastic modulus is 196 GPa (28.4 Msi). 1.4958 CR-A has a density of 7.94 g/cm³ (0.287 lb/in³), heavier than 78% of stainless steel grades. It melts at 1,357°C (2,475 °F). SA is the default condition FabDigit quotes; CR-A is available on request or by drawing note.

Advantages

  • High service temperature — 1,100°C (2,012 °F), better than 96% of stainless steel grades
  • Forms and bends easily — 75/100, better than 87% of stainless steel grades
  • Readily welded — 80/100, better than 80% of stainless steel grades
  • Ductile — tolerates forming and impact — 45%, better than 76% 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 — 6.8 kg CO₂/kg, worse than 95% of stainless steel grades
  • Low electrical conductivity — 1.7 % IACS, worse than 93% of stainless steel grades
  • Low strength — 250 MPa (36.3 ksi), worse than 91% of stainless steel grades

1.4958 CR-A properties

Typical room-temperature values for 1.4958 CR-A; 22 are specific to this condition. Other listed values are 1.4958 reference data and may not represent this condition. Bars are the position among stainless steel grades.

Physical3

1.4958 CR-A has a density of 7.94 g/cm³ (0.287 lb/in³), heavier than 78% of stainless steel grades. It melts at 1,357°C (2,475 °F).

Density7.94 g/cm³0.29 lb/in³
Melting Point (Solidus)1,357°C2,475 °F
Liquidus Temperature1,385°C2,525 °F

Mechanical15

1.4958 CR-A has a yield strength of 250 MPa (36.3 ksi) and a tensile strength of 550 MPa (79.8 ksi) — weaker than 91% of stainless steel grades. Elongation at break is 45% and the elastic modulus is 196 GPa (28.4 Msi).

Elastic (Young's) Modulus196 GPa28.4 Msi
Shear Modulus77 GPa11.2 Msi
Bulk Modulus200 GPa29 Msi
Poisson's Ratio0.34
Tensile Strength (Ultimate)550 MPa79.8 ksi
Yield Strength (0.2% offset)250 MPa36.3 ksi
Elongation at Break45%
Reduction in Area55%
Compressive Strength250 MPa36.3 ksi
Shear Strength395 MPa57.3 ksi
Fatigue Strength (Endurance Limit)250 MPa36.3 ksi
Charpy V-Notch Impact (RT)160 J118 ft·lbf
Hardness, Brinell145 HB
Hardness, Rockwell B80 HRB
Hardness, Vickers152 HV

Thermal5

1.4958 CR-A 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 14.4 µm/m·K (8 µin/in·°F).

Thermal Conductivity11.5 W/m·K6.6 BTU/hr·ft·°F
Specific Heat Capacity460 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)14.4 µm/m·K8 µin/in·°F
Max Service Temperature (continuous)1,100°C2,012 °F
Min Service Temperature-196°C-321 °F

Electrical3

1.4958 CR-A conducts electricity at 1.7 % IACS, worse than 93% of stainless steel grades.

Electrical Conductivity1.7 % IACS
Electrical Resistivity9.9×10⁻⁷ Ω·m39 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is very good (70/100), better than 68% of stainless steel grades.

Galvanic Potential (seawater, vs SCE)-0.15 V
Corrosion ResistanceVery good70/100
Chemical Resistance SummaryExcellent resistance to high-temperature oxidation, carburisation and nitriding; immune in practice to chloride SCC; good in steam, hot water, nitric and organic acids. Poor in sulphur-bearing reducing gases above ~600 °C and in hot halide/strong reducing acid service.

Sustainability4

Producing a kilogram of 1.4958 CR-A takes about 90 MJ of energy and emits 6.8 kg of CO₂ — more than 94% of stainless steel grades. Typical recycled content is 40%.

Embodied Energy (primary production)90 MJ/kg38,693 BTU/lb
Embodied Carbon (primary production)6.8 kg CO₂/kg
Embodied Water250 L/kg30 gal/lb
Typical Recycled Content40%

Manufacturability7

1.4958 CR-A's machinability is poor (30/100, worse than 70% of stainless steel grades); weldability very good (80/100); formability very good (75/100).

MachinabilityPoor30/100
Machinability Rating (AISI 1212 = 100 %)25%
WeldabilityVery good80/100
Formability (cold)Very good75/100
Brazeability / SolderabilityGood60/100
PolishabilityVery good70/100
Anodizing Responsen/a — not an anodizable alloy; use pickling/passivation or bright annealing

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

Working with 1.4958 CR-A

Is 1.4958 easy to machine?

Machine like a tough austenitic: rigid setup, positive-rake carbide, low speed / heavy positive feed, flood coolant and no dwelling — the alloy work-hardens rapidly and is gummy.

Can 1.4958 be welded?

Readily welded by GTAW/GMAW/SMAW with Ni-Cr-Nb fillers (ERNiCr-3 / ENiCrFe-2); no preheat needed, keep interpass low and heat input moderate, post-weld heat treatment normally unnecessary.

Can 1.4958 be formed, bent or molded?

Good cold formability but ~1.5× the forming loads of 304 and high springback; hot work at 950–1200 °C and re-solution anneal at 1100–1180 °C to restore the coarse grain required for 800H creep properties.

What surface finishes work on 1.4958?

Pickle in HNO₃–HF or bright anneal to remove the tenacious Cr/Al/Ti oxide before service; can be ground and polished to a bright finish, not anodizable, plating rarely used.

1.4958 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
Ccontrolled carbon distinguishes 800H from 800 (EN 1.4958 permits 0.03–0.08)0.05 – 0.10.07
Si≤ 10.4
Mn≤ 1.50.8
P≤ 0.03—
S≤ 0.02—
Cr19 – 2321
Ni30 – 3532
Al0.15 – 0.60.4
Ti0.15 – 0.60.4
Cu≤ 0.75—
Febalance, 39.5 % min per ASTM B409/B408≥ 39.5 (balance)—

1.4958 CR-A — frequently asked

What is 1.4958 CR-A used for?

1.4958 CR-A is typically used for reformer tubes, cracking furnace components, heat exchanger tubing and power generation piping. In short: creep-rated Alloy 800; coarse-grain 800H condition; pressure service to 1100 °C.

What is the yield strength of 1.4958 CR-A?

1.4958 CR-A has a typical yield strength of 250 MPa (36.3 ksi) and a tensile strength of 550 MPa (79.8 ksi) — weaker than 91% of stainless steel grades. Strength varies by condition: see the 6 listed tempers.

Is 1.4958 CR-A easy to machine?

Not especially — machinability is rated poor (30/100, worse than 70% of stainless steel grades). Machine like a tough austenitic: rigid setup, positive-rake carbide, low speed / heavy positive feed, flood coolant and no dwelling — the alloy work-hardens rapidly and is gummy.

Can 1.4958 CR-A be welded?

Yes — weldability is rated very good (80/100). Readily welded by GTAW/GMAW/SMAW with Ni-Cr-Nb fillers (ERNiCr-3 / ENiCrFe-2); no preheat needed, keep interpass low and heat input moderate, post-weld heat treatment normally unnecessary.

What surface finishes work on 1.4958 CR-A?

Pickle in HNO₃–HF or bright anneal to remove the tenacious Cr/Al/Ti oxide before service; can be ground and polished to a bright finish, not anodizable, plating rarely used.

Can 1.4958 CR-A be formed, bent or molded?

Good cold formability but ~1.5× the forming loads of 304 and high springback; hot work at 950–1200 °C and re-solution anneal at 1100–1180 °C to restore the coarse grain required for 800H creep properties.

What is the maximum service temperature of 1.4958 CR-A?

1.4958 CR-A 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 1.4958-SA and 1.4958-CD?

SA is the default condition — standard supply condition for plate, tube and pipe used in creep-range service; gives the coarse grain required for 800H creep properties. CD: choose for close-tolerance bar and small-bore tubing where higher room-temperature strength and better surface finish are wanted; not for long-term creep service without re-anneal. Yield strength is 220 MPa in SA versus 400 MPa in CD.

Sources

  1. ASTM B409 / B408 / B564 — Ni-Fe-Cr alloy plate, bar and forgings (UNS N08810) — ASTM International (2021)
  2. EN 10095 — Heat resisting steels and nickel alloys (X5NiCrAlTi31-20, 1.4958) — CEN (1999)
  3. INCOLOY alloy 800H & 800HT product datasheet — Special Metals Corporation (2004)
  4. ASM Handbook Vol. 1 — Heat-Resistant Alloys — ASM International (1990)
  5. ASME BPVC Section II Part D — allowable stresses for N08810 — ASME (2023)

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.