EN 2.4608UNS N06333Alloy 333Heat-resistant Ni-Cr

The Complete Guide to NiCr26MoW (2.4608)

NiCr26MoW (EN 2.4608 / UNS N06333) is a heat-resistant nickel-chromium alloy strengthened in solid solution with molybdenum, tungsten and cobalt. It resists oxidation in air to about 1200°C and carburisation in furnace atmospheres, making it a proven choice for forged furnace, turbine and thermal-processing parts.

By Jiangsu Liangyi engineering team Published Updated ~12 min read

Key facts at a glance

NiCr26MoW / 2.4608 — quick reference

Alloy typeHeat-resistant Ni-Cr, solid-solution
DesignationsEN 2.4608 · UNS N06333 · Alloy 333
Nominal chemistryNi ~45% · Cr ~25% · Mo/W/Co ~3% each
Density8.5 g/cm³
ConditionSolution annealed
Oxidation limit~1200°C in air
Load-bearing limit~1000°C
Key strengthsOxidation, carburisation & thermal-fatigue resistance
Product formsRings, discs, shafts, bars, flanges (30 kg–30 t)
CertificationISO 9001:2015 · EN 10204 3.1 MTC (3.2 on request)
~26%
Chromium
1200°C
Oxidation limit
8.5
Density g/cm³
30 t
Max forging weight

01 — Overview

What NiCr26MoW actually is

NiCr26MoW is a nickel-base heat-resistant alloy — not a wet-corrosion alloy. Its job is to hold together, resist scaling and keep useful strength in the hot, aggressive atmospheres inside furnaces and combustion equipment.

Underneath the designation sits a nickel-chromium-iron matrix strengthened with molybdenum, tungsten and cobalt in solid solution. That combination is deliberate: the high chromium builds a tough, self-healing oxide skin; the nickel-rich austenite stays stable and shrugs off carburising gases; and the refractory metals slow the creep that would otherwise let a part sag under its own weight at red heat.

Because the alloy is strengthened by dissolved elements rather than by hardening precipitates, it does not depend on a delicate ageing treatment to perform. It is delivered solution annealed and stays ductile, weldable and dimensionally forgiving across a very wide temperature band — exactly what a furnace fixture or a radiant tube needs when it is heated and cooled thousands of times.

Quick answer

NiCr26MoW (EN 2.4608, UNS N06333, Alloy 333) is a heat-resistant nickel-chromium alloy that resists oxidation to ~1200°C, resists carburisation in furnace gases, and holds useful load-bearing strength to ~1000°C. It is supplied solution annealed and forged into rings, discs, shafts and bars.

02 — Naming

Designations & cross-references

One alloy, several names — a common source of confusion at the purchasing stage. The same material turns up on drawings and datasheets under all of the following:

Equivalent designations for NiCr26MoW
SystemDesignationNote
EN — numeric2.4608Werkstoffnummer used across European drawings
EN — chemicalNiCr26MoWName encodes Ni-Cr with Mo and W additions
UNSN06333North-American unified number
Trade namesAlloy 333Common commercial designations

They are treated here as one material. Even so, a name on a drawing is not a specification — always pin the exact acceptance standard, condition and testing scope on the purchase order so the mill certificate and the design intent agree.

03 — Chemistry

Chemical composition

The chemistry is what makes the alloy behave the way it does. Nickel forms the stable austenitic base, chromium supplies oxidation resistance, and a balanced package of iron, cobalt, molybdenum, tungsten and silicon does the rest. Typical permitted ranges (weight %):

NiCr26MoW nominal composition · weight %
ElementMinMaxRelative content
Nickel — Ni44.047.0
Chromium — Cr24.026.0
Iron — Fe11.423.8
Molybdenum — Mo2.54.0
Tungsten — W2.54.0
Cobalt — Co2.54.0
Silicon — Si0.71.5
Manganese — Mn2.0
Carbon — C0.0300.080

Note the deliberately generous silicon and the modest, controlled carbon. Silicon reinforces the oxide scale; carbon is held low enough to keep the alloy tough and weldable, yet high enough to give a little carbide strengthening at temperature.

04 — Data

Mechanical & physical properties

Room-temperature figures for the solution-annealed condition are given below as an engineering reference. The values that matter most for this alloy, though, are the ones it retains once it is hot — see the next section.

NiCr26MoW indicative properties · solution annealed, room temperature
PropertyValueUnit
Density8.5g/cm³
Ultimate tensile strength~620MPa
0.2% proof (yield) strength~270MPa
Elongation at break~34%
Young's modulus~210GPa
Melting range1410–1460°C
Thermal conductivity~11W/m·K
Mean thermal expansion~13µm/m·K

Two numbers deserve a second look. The low thermal conductivity (roughly a fifth of carbon steel's) means heat travels slowly through the alloy — good for a barrier, but something to plan for when machining, where the heat stays at the cutting edge. And the modest room-temperature strength is by design: this is not a high-strength structural steel, it is an alloy chosen for stability at temperatures where ordinary steels have already lost most of theirs.

05 — Metallurgy

What each element does

The performance of NiCr26MoW is best understood element by element — each addition is pulling its weight:

  • Nickel (~45%) — forms the face-centred-cubic austenite that stays stable from cryogenic to red heat, resists carburising and nitriding atmospheres, and provides the toughness backbone.
  • Chromium (~25%) — grows the adherent Cr₂O₃ oxide film that is the alloy's first line of defence against scaling and hot corrosion; the high level pushes usable oxidation resistance toward 1200°C.
  • Silicon (up to 1.5%) — feeds a silica-rich sub-layer beneath the chromia scale, sharply improving resistance to carburisation and to cyclic oxidation.
  • Molybdenum + Tungsten (2.5–4% each) — heavy, slow-diffusing atoms that lock the lattice and deliver the solid-solution strengthening and creep resistance that keep parts from sagging under load at temperature.
  • Cobalt (2.5–4%) — raises high-temperature strength and structural stability, and helps the alloy hold up under thermal fatigue.
  • Iron (balance) — dilutes cost and tunes thermal expansion without giving up the essential nickel character.

Why it resists thermal shock

A stable austenitic matrix plus a tough, self-repairing oxide scale means the surface does not spall away each time the part heats and cools. That is what lets NiCr26MoW survive the repeated thermal cycling that destroys lesser materials in batch furnaces.

06 — The core strength

High-temperature performance

This is the section that justifies the alloy. NiCr26MoW is specified precisely because of how it behaves in three regimes of heat — and its practical ceiling depends on which of those regimes you are in.

NiCr26MoW high-temperature service bands A temperature scale showing NiCr26MoW carburisation onset context near 870 degrees C, load-bearing limit near 1000 degrees C, and oxidation limit near 1200 degrees C. 870°C 1000°C 1200°C ambient service band oxidation limit
Figure 1. Indicative service bands for NiCr26MoW (EN 2.4608 / UNS N06333). Real limits depend on atmosphere, applied stress and thermal cycling.

Oxidation

Protective Cr₂O₃/SiO₂ scale resists scaling in air to roughly 1200°C.

Load-bearing

Useful creep strength for stressed parts to about 1000°C.

Carburisation

Nickel-rich matrix strongly resists carbon pick-up in furnace gases.

Oxidation resistance

In air and combustion atmospheres the chromium-silicon oxide scale reforms as fast as it is worn away, holding metal loss low even during repeated heating and cooling. That cyclic oxidation resistance — not just steady-state performance — is a defining strength of the alloy.

Carburisation & nitriding resistance

Endothermic and carburising furnace gases attack many stainless steels by dumping carbon into the metal, embrittling it. The high nickel content of NiCr26MoW makes carbon far less soluble and far slower to diffuse, so parts stay tough far longer in carbon-rich duty.

Creep & rupture strength

Molybdenum, tungsten and cobalt in solution resist the slow, permanent deformation that occurs under sustained load at temperature. For stressed components — support grids, fans, rolls, turbine hardware — this creep resistance is what determines service life.

Need this alloy as a finished part? See stock forms, sizes and certification for our custom NiCr26MoW forgings →

07 — Comparison

How NiCr26MoW compares to other heat-resistant grades

Engineers usually reach NiCr26MoW after weighing it against cheaper stainless and other nickel grades. The table below positions it qualitatively against common alternatives; always confirm against design data for a specific duty.

Qualitative positioning vs common heat-resistant materials
GradeCharacterRelative to NiCr26MoW
310S stainless (1.4845)25Cr-20Ni austeniticCheaper; lower creep strength and weaker carburisation resistance
Alloy 800H/HT (N08810/11)Fe-Ni-Cr, ~32NiGood creep; NiCr26MoW adds Mo/W/Co for thermal-fatigue duty
Alloy 601 (N06601)Ni-Cr-AlExcellent oxidation via Al; NiCr26MoW favours carburising service
NiCr26MoW (2.4608)Ni-Cr + Mo/W/Co/SiBalanced oxidation, carburisation and thermal-cycling resistance

The short version: NiCr26MoW earns its place where a single part must simultaneously resist scaling, carbon attack and creep through many heat-and-cool cycles — a combination that trips up the cheaper single-purpose grades.

08 — Manufacturing

Forging the alloy

NiCr26MoW is hot-worked, not cold-formed — the same solid-solution elements that make it strong at temperature also make it stiff to deform. A disciplined forging window matters:

  • Heating — soak thoroughly and uniformly to about 1150–1200°C before working; a cold core will crack under the press.
  • Finishing temperature — stop working before the piece drops below roughly 950°C to avoid tearing and to control final grain size.
  • Reduction & grain refinement — sufficient deformation and controlled cooling refine the structure, which lifts both toughness and creep life.
  • Press capacity — the alloy's hot strength calls for substantial forging force; open-die presses in the multi-thousand-tonne class handle the large rings and shafts.

Because it is forged rather than cast, the finished part carries a wrought, grain-flowed structure that is denser and more reliable under thermal cycling than an equivalent casting — one of the main reasons buyers choose forgings for critical hot-section hardware.

09 — Processing

Heat treatment

The delivery condition is solution annealed. The purpose is to dissolve carbides and homogenise the structure so the alloy reaches service ductile, stress-free and ready to build its protective scale.

  • Solution anneal — heat to a high annealing temperature (typically the ~1150–1200°C band), hold to take carbides into solution, then cool rapidly enough to keep them there.
  • Cooling — water or accelerated air quench maximises ductility and retained toughness; slow cooling risks grain-boundary carbide films.
  • After machining — heavy machining can be preceded by an anneal to relieve stress and stabilise dimensions on close-tolerance parts.

Practical note

Because the alloy is solid-solution strengthened, it does not require an ageing / precipitation step. That makes its heat treatment simpler and more robust than that of the precipitation-hardened superalloys it sometimes competes with.

10 — Fabrication

Machining & welding

Machining

Like most nickel alloys, NiCr26MoW work-hardens quickly and conducts heat poorly, so the cutting zone runs hot. A few habits keep it under control:

  • Rigidity first — heavy, chatter-free set-ups and sharp tooling; let the tool cut, never rub.
  • Moderate speed, positive rake — favour a consistent feed and generous depth of cut to stay below the work-hardened skin.
  • Flood coolant — pull heat away from the edge; the alloy will not do it for you.

Welding

The alloy is readily welded by common gas-shielded arc processes using a matching or compatible nickel-chromium filler. Keep heat input controlled, hold interpass temperature down, and clean between passes. Solution annealing after welding restores full oxidation performance on demanding assemblies.

11 — Where it is used

Industrial applications

Wherever a component has to keep working while it glows, NiCr26MoW is a candidate. Typical duty:

Heat-treatment industry

Baskets, trays, grids, fixtures, muffles, retorts and radiant tubes that ride through furnace after furnace.

Petrochemical & refining

Furnace internals and supports exposed to hot, carbon-rich process gas.

Gas & steam turbines

Combustor and transition hardware, rings and structural parts in the hot section.

Industrial furnaces

Rolls, fans, hangers and burner components in continuous thermal plant.

Power & energy

High-temperature structural forgings where oxidation and creep both matter.

Thermal & chemical processing

Components for high-temperature reaction and calcining equipment.

In each of these the failure mode being designed out is the same story: scaling, carbon attack, or slow creep. NiCr26MoW addresses all three at once, which is why it survives as a specified grade where cheaper stainless steels are consumed.

12 — Product

Available product forms

As a forging house, we supply NiCr26MoW in the shapes that feed hot-section fabrication and machining:

Typical NiCr26MoW forged forms & capability
FormTypical useRange
Seamless rolled ringsTurbine & furnace rings, spacers, seal ringslarge diameters
Discs & blanksRotating and structural hot partsmachined / as-forged
Shafts & barsRolls, spindles, machined componentsround / stepped
Flanges & bodiesHigh-temperature connections and housingsto drawing
Custom open-die forgingsOne-off shaped parts~30 kg – 30 t

Every piece is traceable from melt to finished part and supplied with EN 10204 3.1 (or 3.2 on request) mill test certificates. Full details of stock forms and sizes are on the NiCr26MoW (2.4608) forging parts page.

13 — Buying

Specifying & sourcing forgings

A clean order prevents almost every downstream dispute. When you request a quotation for NiCr26MoW forgings, state:

  • Form & dimensions — ring / disc / bar / shaped part, with rough or finish-machined stock allowance.
  • Specification & condition — the acceptance standard and the delivery condition (solution annealed).
  • Testing & certification — chemistry, mechanicals, NDT and the certificate level (3.1 or 3.2), plus any third-party witness.
  • Traceability — heat-number marking and documentation requirements.
JL

About this guide

Written by the engineering team at Jiangsu Liangyi Co., Limited, an ISO 9001:2015 certified Chinese manufacturer of nickel-alloy and heat-resistant open-die forgings and seamless rolled rings since 1997, supplying customers in 50+ countries. Figures are drawn from our production experience and published EN/UNS material data.

14 — FAQ & references

Frequently asked questions

Is NiCr26MoW (2.4608) the same as Alloy 333?
Yes — EN 2.4608 / NiCr26MoW shares the same nominal chemistry and heat-resistant character as UNS N06333, commonly sold as Alloy 333. Confirm the exact acceptance standard on your order so the certificate matches your design.
What is the maximum service temperature of NiCr26MoW?
Useful load-bearing strength extends to roughly 1000°C, while oxidation resistance in air reaches about 1200°C. The real limit depends on the atmosphere, applied stress and how often the part is thermally cycled.
What are the main alloying elements?
About 45% nickel and 25% chromium form the base, with roughly 3% each of molybdenum, tungsten and cobalt for solid-solution strengthening, up to 1.5% silicon for oxidation resistance, iron as balance and low carbon of 0.03–0.08%.
Why choose a forging over a casting in this alloy?
A forging has a wrought, grain-flowed structure that is denser and more consistent than a casting, which improves toughness and resistance to thermal-fatigue cracking — decisive advantages for cyclic hot-section duty.
Is NiCr26MoW weldable?
Yes. It is readily welded by gas-shielded arc processes with a matching or compatible nickel-chromium filler, using controlled heat input and interpass temperature. A post-weld solution anneal restores full properties on demanding assemblies.
Can you supply to a customer specification?
Yes. Parts are produced to international standards and to customer-specific material and inspection requirements, with EN 10204 mill test certificates and third-party inspection available on request.

References & standards

  • EN 10302 — Creep resisting steels, nickel and cobalt alloys (designation reference for 2.4608).
  • UNS N06333 — Unified Numbering System designation for the alloy.
  • EN 10204 — Types of inspection documents (3.1 / 3.2 mill test certificates).
  • Published nickel-alloy engineering property data for NiCr26MoW / N06333.

Property values in this guide are indicative and provided for general engineering guidance only. For design use, confirm against the governing material specification and your own qualification data.

Trademarks. Third-party alloy and grade names referenced for comparison or identification (for example Alloy 333, Alloy 800H, Alloy 601) remain the property of their respective owners. Their use here is descriptive only and does not imply any affiliation with, sponsorship by, or endorsement from those owners.

Certification. Jiangsu Liangyi Co., Limited operates under an ISO 9001:2015 quality management system. Mill test certificates issued to EN 10204 (type 3.1, or type 3.2 with independent inspection arranged on request) are material inspection documents supplied with an order; they are not separate third-party company certifications.

NiCr26MoW · EN 2.4608 · UNS N06333

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