Supreme Steels

Inconel 600 Alloy (UNS N06600)

Inconel 600 (AMS 5540, ASTM B564)

Inconel 600 is a high-strength nickel-chromium alloy made for extreme conditions. It resists heat, corrosion, and pressure with ease. This alloy stays strong and stable from very low to very high temperatures. It works well up to 2000°F (1093°C). Inconel 600 fights oxidation, carburization, and chloride stress cracking. Because of this, it is trusted in chemical plants, aerospace parts, nuclear systems, and heat-treating tools.
This alloy offers great strength and long service life. The high nickel gives strong resistance to reducing chemicals. The chromium adds protection from oxidation and scaling. Together, they make the alloy tough and durable. Inconel 600 lasts longer and needs less maintenance than regular stainless steel. It is the best choice for furnaces, heat exchangers, and gas turbines. When the job demands strength and safety, Inconel 600 delivers every time.

Key properties

Performance Profile:

Common Applications:

Inconel 600 serves many industries. It keeps parts strong in heat and corrosion. Below is a detailed, end-to-end list of common applications. Each item shows typical parts, why Inconel 600 fits, and practical benefits.

1. Chemical Processing Equipment

2. Aerospace Components

3. Power Generation Systems

4. Heat-Treating Furnaces & Fixtures

5. Nuclear Industry

6. Marine and Offshore Equipment

6. Oil & Gas Processing

8. Food Processing & Pulp & Paper

9. Electronics & Instrumentation

10. Automotive & Exhaust Systems (High-Performance)

11. Furnace Components & Retorts

12. Industrial Valves, Fasteners & Hardware

13. Heat Exchangers & Condensers

14. Manufacturing Tools in Aggressive Environments

15. Custom & Specialty Applications

Specifications:

Chemical Composition (WT %):

Element Symbol Weight Percentage (WT %) Function / Significance
Nickel Ni 72.0 min Provides exceptional resistance to corrosion, particularly in reducing environments. It ensures stability across high and low temperatures and enhances ductility and toughness.
Chromium Cr 14.0 – 17.0 Strengthens oxidation resistance in high-temperature atmospheres and adds resistance to sulfur compounds and other oxidizing agents.
Iron Fe 6.0 – 10.0 Improves structural rigidity and thermal stability, contributing to the alloy’s mechanical balance and cost efficiency.
Carbon C 0.15 max Maintains strength and hardness while keeping the alloy resistant to grain boundary corrosion. Low carbon ensures weldability.
Manganese Mn 1.0 max Enhances hot-working characteristics and improves toughness under mechanical stress.
Sulfur S 0.015 max Controlled to a very low level to prevent hot cracking and maintain high purity and corrosion resistance.
Silicon Si 0.50 max Aids in oxidation resistance and improves high-temperature stability by forming a protective oxide layer.
Copper Cu 0.50 max Adds additional corrosion resistance, particularly in marine and acidic environments.
Aluminum Al 0.50 max Strengthens the protective oxide film and improves the material’s surface stability at elevated temperatures.
Titanium Ti 0.50 max Refines grain structure and enhances the alloy’s creep resistance and thermal stability.

Physical Properties:

Property Typical value (range where applicable) Units Notes / Test Condition
Alloy designationInconel 600 (UNS N06600)Nickel-chromium alloy
Density8.47g/cm³≈ 8470 kg/m³
Phase structureSingle-phase FCC (austenitic)Stable austenitic structure at RT
Melting / solidus-liquidus1370 – 1425°CMelting range (approx.)
Modulus of elasticity (Young’s modulus)≈ 205GPaRoom temperature
Poisson’s ratio≈ 0.29Typical for nickel alloys
Thermal conductivity11 – 14W·m⁻¹·K⁻¹Room temperature; decreases at high T
Specific heat capacity (Cp)≈ 435J·kg⁻¹·K⁻¹At ~20–100 °C (0.435 kJ·kg⁻¹·K⁻¹)
Coefficient of thermal expansion (CTE)≈ 13.3 ×10⁻⁶/°C20–100 °C typical; increases with T
Electrical resistivity≈ 100µΩ·cm (≈1.0×10⁻⁶ Ω·m)At 20 °C; alloy and cold-work alter value
Magnetic behaviorEssentially non-magneticMay show slight ferromagnetism if cold-worked
Hardness (annealed)HRB ~70 – 100Rockwell BVaries with product form and cold work
0.2% Proof (yield) strength (annealed)≈ 205MPaTypical room-temp value; depends on temper
Ultimate tensile strength (annealed)≈ 515 – 620MPaRoom temperature, annealed condition
Elongation (annealed)30 – 50%Percent elongation in 50 mm gauge typical
Reduction of area (typ.)35 – 60%Depends on product and test
Recommended continuous service temperatureUp to ≈ 700°CShorter exposures possible at higher T
Maximum intermittent service≈ 1000°CApplication-dependent; oxidation and strength limits
Thermal shock resistanceGoodQualitativeHigh strength retention; depends on section size
Weldability & fabricationExcellentQualitativeReadily welded; standard filler metals used
Corrosion resistance (qualitative)Excellent to very goodQualitativeStrong resistance to oxidizing and many reducing environments; contact supplier for specific media
Workability (forming)Good (annealed)QualitativeCold-work hardens the alloy; anneal to restore ductility
Typical surface scale / oxidation behaviorForms protective oxide layer (Cr-rich)QualitativeGood high-temp oxidation resistance

Mechanical Properties

Property Symbol / Unit Typical Value (Room Temp) Range / Notes
Densityρ8.47 g/cm³ (0.306 lb/in³)From Special Metals Table 2 (typical).
Melting range1354 – 1413 °C (2470 – 2575 °F)Reported melting range (solidus–liquidus).
Young’s modulus (tension)E214 GPa (≈214 000 MPa) at 22 °CFalls with temperature (e.g., ~199 GPa at 300 °C).
Shear modulusG80.8 GPa (RT)Values decline with temperature.
Poisson’s ratioν0.324 (RT)Small variation with temperature.
Tensile strength (ultimate, UTS) — annealedUTS550 – 690 MPa (typical for annealed rod/bar)Higher for cold-worked or hard tempers (e.g., 725–1035 MPa as-drawn/cold).
Yield strength (0.2% offset) — annealedRp0.2 / YS170 – 345 MPa (typical, annealed forms)Many form/temper dependent ranges in the datasheet (rod, plate, tube).
Elongation (in 50 mm or specified gauge)A%55 – 35 % (annealed typical)Heavily cold-worked material shows much lower elongation.
Reduction of area (RA)RA%~60–70% (typical examples reported)Depends on form/temper and test specimen.
Hardness (Rockwell B) — annealedHRB65 – 85 HRB (annealed typical for rod/plate)Hardness increases with cold work; some tempers are given as HRB 90+ or HRC values for heavily worked conditions.
Hardness (Rockwell C) — hard tempersHRCUp to ~30–35 HRC (hard tempers)See datasheet for specific temper conversions.
Fatigue strength / enduranceGood fatigue resistance for high-temp service (data available)Fatigue (rotating-beam / LCF) data provided in Special Metals; values vary with temperature and condition.
Creep & rupture (elevated T)Useful creep resistance to ~600–1150 °C depending on conditionDetailed creep-rupture tables and curves in datasheet; not precipitation-hardening (strength via cold work).
Thermal conductivity (RT)k≈ 14.9 W/m·K (≈ at 20 °C)Falls slightly with temperature; table available.
Specific heatcp≈ 444 J/kg·K (≈ 0.106 Btu/lb·°F) at RTSee thermal properties table for temperature dependence.
Coefficient of linear thermal expansionα (mean)~10.4 µm/m·°C (20 → 100 °C)Increases with temperature; full expansion table in datasheet.
Electrical resistivity (RT)ρₑ≈ 1.03 µΩ·mGiven in datasheet (typical).
Magnetic behaviorParamagnetic / essentially non-magnetic at RTCurie temp ~ −124 °C; suitable for nuclear/reactor uses.
Work hardening / formabilityReadily cold-worked; can be strengthened by cold workFabrication guidance and typical temper tables available in datasheet.
Weldability & fabricationExcellentQualitativeReadily welded; standard filler metals used.
Corrosion resistance (qualitative)Excellent to very goodQualitativeStrong resistance to oxidizing and many reducing environments; contact supplier for specific media.
Workability (forming)Good (annealed)QualitativeCold-work hardens the alloy; anneal to restore ductility.
Typical surface scale / oxidation behaviorForms protective oxide layer (Cr-rich)QualitativeGood high-temp oxidation resistance.

Heat treatment:

Process / Step Purpose Temperature (°C) Soak / Hold Time (guideline) Cooling Method Microstructure / Effect Typical Applications / When to use Key Notes & Precautions
Solution anneal (full anneal) Restore ductility, dissolve carbides, homogenize alloy after fabrication or heavy cold work 1,020 – 1,120°C 15–60 min depending on section thickness (longer for heavy sections) Rapid cooling (air or water quench) to avoid precipitation Produces a homogenized, single-phase solid-solution microstructure; reduces prior cold-work hardening After heavy cold working, before final machining or service where maximum corrosion resistance is required Avoid slow cooling through 600–900°C range to minimize carbide precipitation and sensitization
Stress relieving (general) Reduce residual stresses from forming, welding or machining without major microstructure change 600 – 760°C 1–4 hours (depends on mass and residual stress level) Air cool / furnace cool Relieves residual stress; minimal change to solid-solution structure After forming, bending, moderate machining; when distortion or cracking risk from residual stress is a concern Keep temperature below solution anneal; excessive temp/time can cause grain growth or sensitization in certain conditions
Post-weld heat treatment (PWHT) / weld stress relief Relieve weld-induced stresses and reduce risk of stress-corrosion cracking in some assemblies 650 – 750°C (typical weld-relief range) 1–3 hours depending on weld size and thickness Controlled air or furnace cooling Reduces residual stresses near welds; can reduce susceptibility to certain cracking modes For large weldments where distortion or stress-corrosion is a concern. PWHT is not always required for Inconel 600 — evaluate per code/spec. Avoid temperatures and hold times that promote carbide precipitation; if design code prohibits PWHT, follow code. Monitor for oxidation/scaling if exposed in-air at these temps.
Recrystallization / anneal after heavy cold work Re-crystallize and restore ductility after heavy cold deformation ~1,000 – 1,080°C (within solution anneal range) Long enough to fully recrystallize (dependent on thickness) Rapid cooling recommended New equiaxed grains, relief of strain hardening After heavy cold working where recrystallization is required for forming or service Use the higher end of range for thicker sections; verify grain size requirements
Stabilization (not typical for Inconel 600) For some alloys stabilization (e.g., Ti or Nb additions) ties up C — Inconel 600 is not normally stabilized N/A N/A N/A N/A Not commonly used — choose stabilized grades if required for specific environments If carbide precipitation and sensitization are a critical risk, consider different alloy or specification
Aging / precipitation hardening Produce hardening via precipitation — Inconel 600 is a solid-solution alloy and is not effectively age-hardened N/A (not applicable) N/A N/A N/A Not applicable — choose precipitation-hardening alloys (e.g., Inconel 718) if required Do not expect aging to increase strength in Inconel 600
Surface bright anneal / decarburizing control Reduce surface oxides or produce bright finish after cleaning 850 – 1,050°C in controlled atmosphere Short hold sufficient to affect surface Controlled atmosphere cooling Reduces surface oxidation/scaling; improves surface finish When surface appearance or cleanliness is required (e.g., fittings, visible parts) Use controlled atmosphere (vacuum or inert gas) to avoid heavy oxidation/scaling
Hydrogen or vacuum anneal (special cases) Remove gases, prevent oxidation, produce very clean surface Process dependent — often similar or slightly higher than solution anneal but in vacuum Hold as required by vacuum furnace practice Slow or controlled furnace cooling in vacuum/inert Clean surface, minimal scale, controlled microstructure For components needing low surface contamination or for subsequent brazing/clean-room service Requires appropriate furnace equipment; follow supplier/AMS/ASTM guidance
Final stress check & inspection Verify residual stress reduction & dimensional stability N/A (inspection step) N/A N/A N/A After heat treatment and cooling, before final machining or assembly Perform NDT, dimensional checks, hardness tests, or metallography as required

Frequently Asked Questions (FAQs):

What is Inconel 600 and what makes it unique?
Inconel 600 is a nickel-chromium alloy. It resists heat, oxidation, and corrosion. High nickel content protects against chloride stress cracking. Chromium adds strength and oxidation resistance. It performs well where stainless steels fail.
Industries use Inconel 600 in chemical plants, furnaces, and power systems. It is ideal for heat exchangers, aerospace parts, and reactor vessels. The alloy performs safely in high-pressure and high-temperature environments.
Inconel 600 stays strong at high heat. It resists scaling and deformation. It keeps stability up to 1150°C (2100°F). This makes it ideal for heat treatment and thermal cycle operations.
Inconel 600 lasts longer than stainless steel in harsh settings. It resists oxidation, carburization, and chloride corrosion. It keeps strength at higher temperatures. It reduces maintenance and extends equipment life.
Yes. Inconel 600 comes in bars, sheets, plates, pipes, and tubes. It is also available in fittings. Supreme Special Steels supplies custom sizes that meet global standards and industry needs.