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Quick Answer

Haynes 230 alloy (UNS N06230) is a nickel-chromium-tungsten-molybdenum solid-solution strengthened superalloy with oxidation resistance up to 1149°C (2100°F), creep rupture strength approximately 35% higher than Hastelloy X at 871°C, and industry-leading nitriding resistance. Governed by AMS 5891, ASTM B572, ASME SB-572. European designation: DIN 2.4733 / Ni62Cr22W14Mo2. Used in gas turbines, industrial furnaces, aerospace, and chemical processing.

Technical Deep Dive · Nickel Superalloy Guide

What Is Haynes 230 Alloy?
Composition, Properties & Applications Explained

The complete engineer's guide to UNS N06230 — from tungsten's role in its microstructure to why it outperforms Hastelloy X in creep rupture strength above 871°C. Written by Jiangsu Liangyi's production engineering team with 25+ years of Haynes 230 forging experience.

By Jiangsu Liangyi Engineering Team Published: June 22, 2026 ~2,100 words · 12 min read
1149°C Max continuous service temperature in oxidizing atmosphere
81% Tensile strength retained at 649°C vs. 73% for Hastelloy X
+35% Creep rupture strength advantage over Hastelloy X at 871°C
50+ Countries where Jiangsu Liangyi Haynes 230 parts are in service

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Version 1.0 — Published June 22, 2026  ·  Next review: September 2026  ·  Expert-verified by Jiangsu Liangyi Engineering Team  ·  Standards checked against AMS 5891 Rev. C and ASTM B572-22
Definition

What Exactly Is Haynes 230 Alloy?

Haynes 230 (UNS N06230, W.Nr. 2.4733, DIN Ni62Cr22W14Mo2) is a nickel–chromium–tungsten–molybdenum superalloy whose strength is derived entirely from solid-solution hardening — not precipitation of secondary phases. That single distinction gives it a fabricability and long-term microstructural stability profile that precipitation-hardened competitors like Inconel 718 cannot match above 700°C.

Developed by Haynes International, Inc., it has become the global benchmark for industrial applications demanding simultaneous oxidation resistance, nitriding resistance, creep strength, and thermal stability at temperatures up to 1149°C (2100°F). It performs where most other alloys begin to fail structurally.

UNS Designation
N06230

Primary international identifier. Used in ASTM B572 (rod/bar), ASME SB-572, and AMS 5891. Sits in the N0xxxx nickel alloy series alongside Inconel 600 (N06600) and Hastelloy X (N06002). European equivalent is DIN 2.4733 (Ni62Cr22W14Mo2).

Strengthening Mechanism
Solid-Solution Only

Chromium, tungsten, and molybdenum atoms substitute into the nickel FCC lattice, creating lattice distortion that impedes dislocation movement. No aging treatment is needed or possible — the alloy is supplied and used in the solution-annealed (ATA) condition.


Chemical Composition

Haynes 230 Chemical Composition (UNS N06230)

The table below lists the full compositional range per AMS 5891 / ASTM B572. Nickel is the balance element, typically 57–62%. All values are in weight percent.

Data table 1 — Haynes 230 (UNS N06230) technical data
Element Symbol Weight % Range Primary Function
NickelNiBalance (~47–65%)Austenitic FCC matrix; base for all properties
ChromiumCr20.00 – 24.00%Cr₂O₃ oxide scale; oxidation & nitriding resistance
TungstenW13.00 – 15.00%Primary solid-solution strengthener; creep resistance
MolybdenumMo1.00 – 3.00%Synergistic strengthening with W & Cr
IronFe3.00% maxResidual; controlled maximum
CobaltCo5.00% maxResidual; low Co content vs. cobalt-base alloys
CarbonC0.05 – 0.15%Controlled carbide strengthening; improves creep
AluminumAl0.20 – 0.50%Deoxidant; minor oxide scale stability contribution
LanthanumLa0.005 – 0.05%Reactive element; dramatically improves oxide scale adhesion in cyclic oxidation
ManganeseMn0.30 – 1.00%Deoxidant; minor sulfide-former
SiliconSi0.25 – 0.75%Deoxidant; minor oxidation resistance contribution
TitaniumTi0.10% maxControlled impurity; minimal γ′ precipitation
BoronB0.015% maxGrain boundary strengthener in trace quantities
PhosphorusP0.030% maxControlled impurity; embrittler if excessive
SulfurS0.015% maxControlled impurity; lowers oxidation resistance if excessive

Source: AMS 5891 Rev. C, ASTM B572. All values in weight percent.

Jiangsu Liangyi manufactures Haynes 230 (UNS N06230) forged parts to this AMS 5891 composition, with full chemistry verification on every heat via EN 10204 3.1 mill test certificates.


Element Roles

What Each Key Alloying Element Does

Understanding why each element is present — and at what level — is essential for correctly specifying Haynes 230 and interpreting its performance data.

Cr
Chromium — 20 to 24% · Oxidation & Nitriding Shield
Chromium forms a continuous, slow-growing Cr₂O₃ scale on the alloy surface above ~900°C. This scale acts as a barrier against oxygen, nitrogen, and sulfur ingress. At 22% Cr, Haynes 230 sits at the sweet spot between sufficient scale-forming ability and a stable austenitic matrix without sigma-phase risk. This is the element primarily responsible for the alloy's industry-benchmark nitriding resistance.
W
Tungsten — 13 to 15% · Primary Strength Provider
Tungsten is the most important strength-giving element in Haynes 230. Its large atomic radius creates significant lattice strain when dissolved in the nickel matrix, making dislocation movement — and therefore creep deformation — much harder. At 13–15%, it delivers solid-solution strengthening at temperatures above 900°C that most Ni-Cr alloys without tungsten simply cannot achieve. This is the primary reason Haynes 230 outperforms Hastelloy X and Inconel 601 in creep rupture tests above 871°C.
La
Lanthanum — 0.005 to 0.05% · Oxide Scale Anchor
Lanthanum is added in trace amounts but delivers disproportionately large benefits. It segregates to the Cr₂O₃/metal interface and dramatically improves the mechanical adhesion of the oxide scale to the base metal during thermal cycling. Without La, the scale can spall off during rapid heating and cooling, re-exposing bare metal. With La, the scale remains intact through thousands of thermal cycles — a key reason Haynes 230 is specified for cyclic oxidation environments like turbine combustion liners.
Mo
Molybdenum — 1 to 3% · Synergistic Strengthener
Molybdenum works in concert with tungsten and chromium in the solid-solution matrix. Its effect on creep resistance is synergistic with W rather than independent — the Cr-W-Mo triad together produces better creep rupture life than any single element in isolation. Molybdenum content is kept moderate (compared to Hastelloy X at 9%) to avoid MoO₃ volatilization in oxidizing atmospheres above 700°C.
C
Carbon — 0.05 to 0.15% · Carbide Strengthener
Carbon forms M₆C and M₂₃C₆ carbides (primarily W- and Cr-rich) during solution annealing. These fine carbides provide additional grain boundary strengthening that contributes to creep resistance without requiring a separate precipitation step. Carbon content is controlled to a moderate range — high enough for strengthening, low enough to preserve weldability and avoid sensitization in most service environments.

Mechanical Properties

Haynes 230 Mechanical Properties

Room-Temperature Minimums — AMS 5891 / ASTM B572

Ultimate Tensile Strength
760 MPa
110 KSI minimum per AMS 5891 at room temperature
0.2% Yield Strength
310 MPa
45 KSI minimum. Rises modestly with cold work prior to solution annealing.
Elongation at Break
40% min
Exceptional ductility enables cold-forming of complex geometries
Hardness (Solution Treated)
HB 180–220
Typical for solution-annealed forgings. No age-hardening required.

Elevated-Temperature Tensile Properties (ASTM E21)

Data table 2 — Haynes 230 (UNS N06230) technical data
Temperature UTS (MPa) 0.2% YS (MPa) Elongation (%) Reduction of Area (%)
21°C (70°F) — Room8003554758
538°C (1000°F)7202754657
649°C (1200°F)6552554860
760°C (1400°F)6002355263
871°C (1600°F)5102155567
982°C (1800°F)2751806873
1093°C (2000°F)105757882

Typical average values on solution-annealed forged bar, tested per ASTM E21. Contact Jiangsu Liangyi for heat-specific certified test data.

Engineering Insight

The 8-percentage-point gap at 649°C doesn't sound dramatic, but in 50,000+ operating hours of gas turbine service, it translates to reduced wall thickness requirements and longer component replacement intervals — both measurable economic benefits that justify the material cost premium for hot-section forgings.

Creep Rupture Strength — Stress to Cause Rupture in 1,000 Hours

Data table 3 — Haynes 230 (UNS N06230) technical data
Temperature 100-hr Rupture Stress 1,000-hr Rupture Stress vs. Hastelloy X at Same Temp.
871°C (1600°F)165 MPa (24 KSI)110 MPa (16 KSI)~35% higher rupture strength
982°C (1800°F)72 MPa (10.4 KSI)45 MPa (6.5 KSI)~28% higher rupture strength
1093°C (2000°F)28 MPa (4 KSI)16 MPa (2.3 KSI)~22% higher rupture strength

The Cr-W-Mo solid-solution triad is the mechanism behind these margins. Tungsten's large atomic radius creates maximum lattice distortion — and maximum creep resistance — in the 871–1093°C service window.


Physical & Thermal Data

Haynes 230 Physical and Thermal Properties

These values directly control component design decisions — from wall thickness in pressure vessel engineering to differential expansion stresses in bolted turbine flanges.

Data table 4 — Haynes 230 (UNS N06230) technical data
Property At 21°C (70°F) At 538°C (1000°F) At 871°C (1600°F)
Density8.97 g/cm³8.80 g/cm³ (est.)8.65 g/cm³ (est.)
Melting Range1301–1371°C (2375–2500°F)
Specific Heat397 J/kg·K481 J/kg·K536 J/kg·K
Thermal Conductivity8.9 W/m·K14.8 W/m·K19.7 W/m·K
Mean Thermal Expansion Coeff. (from 21°C)13.9 µm/m·°C15.6 µm/m·°C
Young's Modulus211 GPa182 GPa138 GPa
Magnetic Permeability1.0003 — essentially non-magnetic across full service range
Design Note — Thermal Expansion

Haynes 230's mean thermal expansion coefficient of 13.9 µm/m·°C (21–538°C) is lower than Hastelloy X at 14.8 µm/m·°C and considerably lower than austenitic stainless steels (17–18 µm/m·°C). In a thermally cycled bolted flange assembly operating between ambient and 900°C, this lower coefficient means reduced differential expansion stresses and better long-term joint integrity — a quantifiable lifetime benefit.


Alloy Comparison

Haynes 230 vs. Competing High-Temperature Alloys

The table below compares Haynes 230 against five alloys most commonly evaluated alongside it. Application parameters always govern the correct selection — this table identifies where each alloy genuinely wins and loses.

Data table 5 — Haynes 230 (UNS N06230) technical data
Alloy Max Temp. Haynes 230 Advantage Competitor Advantage
Hastelloy X (N06002)~1080°C +35% creep rupture at 871°C; better nitriding; lower thermal expansion Higher Mo (9%) for aqueous corrosion; wider filler availability
Inconel 601 (N06601)~1100°C Superior nitriding resistance; higher creep strength >900°C; no σ-phase risk Higher Al for sulfidizing; lower material cost
Inconel 625 (N06625)~980°C Much higher strength >900°C; better nitriding resistance Superior aqueous/chloride corrosion; better for marine service
Inconel 718 (N07718)~700°C Can operate to 1149°C vs. 718's 700°C limit; no γ″ dissolution risk Much higher room-temp yield (1035 MPa); ideal for cold high-stress fasteners
310S Stainless (S31008)~1040°C Far superior creep strength, nitriding and oxidation resistance above 900°C Significantly lower material cost; easier to machine and weld

Contact Jiangsu Liangyi for a free application-specific alloy selection recommendation based on your operating temperature, atmosphere, and stress profile.


Key Applications

Where Haynes 230 Is Used — Industry by Industry

Three properties together define Haynes 230's application space: oxidation resistance to 1149°C, industry-best nitriding resistance, and solid-solution creep strength that requires no aging treatment. Any application where all three matter simultaneously is a Haynes 230 application. Jiangsu Liangyi supplies custom Haynes 230 open die forgings and seamless rolled rings across all four industries covered below.

Industrial Gas Turbines
Power generation / mechanical drive
  • Combustion cans and transition ducts
  • Hot-section heat shields and shrouds
  • Seal rings and labyrinth rings
  • Turbine discs and guide rings
  • Thermocouple protection sheaths
Industrial Furnaces
Heat treatment / nitriding / carburizing
  • Nitriding furnace retorts and baskets
  • Radiant tubes and burner shrouds
  • Heat-treating trays and grates
  • Recuperator internals
  • Thermocouple protection tubes
Chemical Processing
Reforming / petrochemical / separations
  • Catalyst grid supports
  • Heat exchanger tube sheets
  • Reformer tube headers and flanges
  • Pressure vessel nozzles
  • Bellows and expansion joints
Aerospace
Military and commercial engines
  • Gas turbine combustor components
  • Afterburner flame holders
  • Exhaust system structural rings
  • High-temperature fasteners (>800°C)
  • Transition duct forgings

Welding & Machining

Fabrication Guidelines for Haynes 230 Forgings

One of Haynes 230's most significant but under-documented advantages is its fabricability. Because strengthening is achieved through solid-solution hardening rather than precipitation of γ′ or γ″ phases, the alloy does not require complex multi-stage aging heat treatments after fabrication — reducing downstream processing cost and risk.

Welding — Processes and Parameters

Data table 6 — Haynes 230 (UNS N06230) technical data
Process Filler Metal Key Parameters Best For
GTAW / TIG (preferred) Haynes 230-W (ERNiCrWMo-1) 100% Ar, ≥15 L/min; interpass <93°C; no preheat to 25mm All section thicknesses; highest weld integrity
GMAW / MIG Haynes 230-W wire 75% Ar / 25% He; pulsed arc; interpass <93°C Higher deposition on thicker sections
SAW (Submerged Arc) Haynes 230-W Low-fluoride flux; low heat input; interpass <93°C Heavy tube sheets and large flanges
EBW / LBW None (autogenous) Vacuum environment; minimal HAZ Precision aerospace components
Post-Weld Heat Treatment Note

No mandatory PWHT is required for most industrial applications. For components in continuous service above 870°C, a post-weld solution anneal at 1177°C for 15–30 minutes followed by rapid quench is strongly recommended to restore full HAZ microstructure — especially for nitriding furnace internals and turbine hot-section components.

Machining — Recommended Cutting Parameters

Haynes 230 work-hardens rapidly and has low thermal conductivity — both factors that concentrate heat at the cutting edge. The parameters below, refined over 25+ years of production experience at Jiangsu Liangyi, consistently achieve Ra ≤ 1.6 µm:

Data table 7 — Haynes 230 (UNS N06230) technical data
Operation Tooling Cutting Speed Feed Rate Coolant
Rough Turning PVD TiAlN carbide (P20–P30) 30–45 m/min 0.15–0.25 mm/rev Flood, continuous
Finish Turning PVD TiAlN carbide 45–60 m/min 0.08–0.12 mm/rev Flood, continuous
Milling Solid carbide, positive rake 20–35 m/min 0.06–0.12 mm/tooth Flood or high-pressure
Drilling Solid carbide, 135° point, through-coolant 8–15 m/min 0.04–0.08 mm/rev Through-tool coolant mandatory

Need Custom Haynes 230 Forgings?

Jiangsu Liangyi manufactures custom Haynes 230 (UNS N06230) open die forgings and seamless rolled rings from 30 kg to 30,000 kg. ISO 9001:2015 certified. EN 10204 3.1/3.2. Ships to 50+ countries with a 24-hour quote response.


FAQ

Frequently Asked Questions About Haynes 230 Alloy

What is the maximum service temperature of Haynes 230?

Haynes 230 is rated for continuous service up to 1149°C (2100°F) in oxidizing atmospheres, where its Cr₂O₃ protective scale remains stable and adherent. For short-duration excursions, it can withstand temperatures up to approximately 1200°C before oxidation rate becomes structurally significant. This makes it the highest continuous-service-temperature alloy available in the weldable, solid-solution-strengthened nickel alloy category that can also be forged in heavy sections.

What is the difference between Haynes 230 and Hastelloy X?

Both are nickel-chromium solid-solution alloys for high-temperature service, but they differ in strengthening approach and performance ceiling. Haynes 230 uses tungsten (13–15%) as its primary solid-solution strengthener, delivering approximately 35% higher creep rupture strength at 871°C and superior nitriding resistance. Hastelloy X uses higher molybdenum (9%) and has slightly better aqueous corrosion resistance at lower temperatures. For most gas turbine hot-section forgings operating above 850°C, Haynes 230 is the superior choice.

Does Haynes 230 require heat treatment after welding?

For most industrial applications, post-weld heat treatment is not mandatory. The alloy's solid-solution-strengthened microstructure is relatively tolerant of the weld heat-affected zone. However, for components operating continuously above 870°C — particularly nitriding furnace internals, turbine combustion components, and anything subject to cyclic thermal loading — a post-weld solution anneal at 1177°C for 15–30 minutes followed by rapid quench is strongly recommended to homogenize the HAZ and restore full high-temperature mechanical properties.

What standards govern Haynes 230 forgings?

The primary standards are AMS 5891 (aerospace and industrial), ASTM B572 (rod and bar for general industrial use), and ASME SB-572 (ASME Boiler and Pressure Vessel Code equivalent). European market projects reference EN 10302 and DIN 2.4733. Oil and gas projects may additionally reference NACE MR0175 / ISO 15156 for sour service. Jiangsu Liangyi produces Haynes 230 forgings compliant with all of these standards — specify the applicable standard when submitting your RFQ.

Why does Haynes 230 have better nitriding resistance than other nickel alloys?

Nitriding resistance is primarily determined by the nature and continuity of the protective oxide scale. Haynes 230's 22% chromium content produces a dense, continuous Cr₂O₃ scale that is also an effective nitrogen barrier. The addition of lanthanum (0.005–0.05%) greatly improves scale adhesion during thermal cycling, preventing spallation events that would expose bare metal to nitriding attack. Low aluminum and titanium content — both nitride-formers — further reduces susceptibility. Together, these factors make it the industry standard for nitriding furnace retorts and baskets operating in ammonia-based atmospheres at 900–1050°C.

Is Haynes 230 magnetic?

No. Haynes 230 has a magnetic permeability of approximately 1.0003 — essentially non-magnetic. Its austenitic FCC crystal structure, stabilized by high nickel and chromium content, remains non-magnetic across its entire service range from cryogenic to 1149°C. Unlike some austenitic stainless steels, Haynes 230 does not transform to martensite under severe cold working. This makes it suitable for scientific instruments, MRI-adjacent equipment, and electronic industry furnace components requiring magnetic neutrality.

What is the recommended filler metal for welding Haynes 230?

Haynes 230-W (AWS A5.14 classification ERNiCrWMo-1) is the preferred filler metal. It is compositionally matched to the base alloy, ensuring equivalent high-temperature strength, oxidation resistance, and nitriding resistance in the weld deposit. If Haynes 230-W is unavailable, Inconel Filler Metal 625 (ERNiCrMo-3) is acceptable for applications below 900°C, but the weld zone will have lower creep strength above that temperature due to the absence of tungsten.