N06601 is a nickel–chromium–iron solid-solution alloy distinguished from Alloy 600 by a deliberate aluminium addition (1.0–1.7%), which gives it outstanding resistance to high-temperature oxidation and excellent resistance to other forms of high-temperature corrosion, including carburisation and nitriding. The aluminium promotes a tightly adherent oxide scale that resists spalling even under severe thermal cycling. This datasheet presents the material within the American (ASTM / SAE-AMS / UNS) standard system.
The alloy retains high mechanical strength and good ductility at elevated temperature and is widely used in thermal-processing, petrochemical, power-generation, and aerospace applications. Like Alloy 600, it is not strengthened by aging — properties derive from solid-solution hardening, with additional strength available only through cold work. It resists oxidation up to approximately 1250 °C and is suitable for continuous high-temperature service where ordinary stainless steels and Alloy 800H/HT are inadequate.
Note: the alloy is not recommended for strongly reducing, sulphur-bearing environments at red heat, owing to its high nickel content.
Values per published manufacturer data (Special Metals / Ulbrich / Elgiloy) for INCONEL alloy 601, annealed condition.
| Property | Value | Unit |
|---|---|---|
| Density | 8.11 | g/cm³ |
| Melting range (solidus–liquidus) | 1360–1411 | °C |
| Elastic modulus (20 °C) | 207 | GPa |
| Modulus of rigidity (20 °C) | 81.2 | GPa |
| Thermal conductivity (20 °C) | 11.2 | W/m·K |
| Coefficient of thermal expansion (20–100 °C) | 13.75 | µm/m·°C |
| Specific heat capacity (20 °C) | 448 | J/kg·K |
| Electrical resistivity (20 °C) | 1.18 | µΩ·m |
| Magnetic permeability | ~1.01 | Essentially non-magnetic |
| Maximum oxidation-resistant temperature | ~1250 | °C |
| Cryogenic service capability | Down to –196 | °C |
Specified per ASTM B166 / B168.
| Element | Symbol | Min % | Max % | Role in Alloy |
|---|---|---|---|---|
| Nickel | Ni | 58.0 | 63.0 | Austenitic FCC matrix; corrosion resistance; high-temperature strength |
| Chromium | Cr | 21.0 | 25.0 | Forms Cr₂O₃ passive film; oxidation and corrosion resistance |
| Iron | Fe | — | Balance | Matrix constituent |
| Aluminium | Al | 1.0 | 1.7 | Key addition; forms adherent oxide scale; superior oxidation resistance vs Alloy 600 |
| Carbon | C | — | 0.10 | Controlled |
| Manganese | Mn | — | 1.00 | Deoxidiser |
| Silicon | Si | — | 0.50 | Deoxidiser |
| Copper | Cu | — | 1.00 | Residual; controlled |
| Sulphur | S | — | 0.015 | Residual impurity; controlled |
Annealed condition, room temperature. Minimum specification values per ASTM B166 / supplier data.
| Property | Value | Source |
|---|---|---|
| Ultimate tensile strength (min) | 550 MPa (80 ksi) | ASTM B166 / supplier datasheet |
| 0.2% proof strength (yield, min) | 205 MPa (30 ksi) | Supplier datasheet |
| Elongation at break (min) | 40 % | Supplier datasheet |
| Hardness | 60–80 HRB (typical) | Supplier datasheet |
| Elastic modulus | 207 GPa | Special Metals / Elgiloy |
| Strengthening method | Cold work only (not age-hardenable) | Special Metals |
Note: Values above are typical/specification-minimum annealed properties and are not for design specification purposes. Confirm against the mill test certificate for each delivery.
| Environment | Performance | Notes |
|---|---|---|
| High-temperature oxidation (air) | Outstanding | Al-bearing scale resists spalling to ~1250 °C, even under thermal cycling |
| Cyclic oxidation | Outstanding | Superior to Alloy 600 due to aluminium addition |
| Carburisation | Excellent | High Ni + Cr resists carbon pickup |
| Nitriding atmospheres | Very Good | Improved nitriding resistance vs Alloy 600 |
| Aqueous corrosion | Good | Good resistance in many water environments |
| Chloride stress-corrosion cracking | Good | High Ni content provides useful resistance |
| Reducing, sulphur-bearing environments (red heat) | Poor | Not recommended; high Ni forms low-melting Ni-S eutectic |
| Carbon dioxide / combustion gases | Good | Suitable for many furnace atmospheres |
The alloy is a solid-solution material and is NOT precipitation-hardenable. Heat treatment is used for annealing, solution treatment, and stress relief only. Strength is increased by cold work.
Solution Treatment Temperature: 1100–1200 °C, followed by rapid cooling (water quench or rapid air cool) Purpose: Maximum rupture/creep strength for high-temperature service above 540 °C.
Anneal Temperature: ~1090–1150 °C Purpose: Maximum tensile properties for service below 540 °C; recrystallises grain structure.
Hot working: 870–1230 °C; large deformations at 1040–1230 °C. Avoid working in the 650–870 °C range (low ductility).
Good weldability by conventional processes. As a solid-solution alloy, it is not subject to strain-age cracking. Owing to lower thermal conductivity and higher thermal expansion than carbon steel, use wider root gaps and larger included angles.
| Welding Process | Applicability | Filler / Consumable |
|---|---|---|
| GTAW / TIG | Excellent | ERNiCrFe-11 / matching 601 filler |
| GMAW / MIG | Good | ERNiCrFe-11 |
| SMAW / stick | Good | ENiCrFe-type electrode |
| SAW / submerged arc | Suitable | matching filler + flux |
Post-weld heat treatment is generally not required for general service.
Machining Guidelines
| Parameter | Recommendation |
|---|---|
| Machinability group | Group C (similar to austenitic stainless steel) |
| Preferred condition | Cold-drawn, or cold-drawn and stress-relieved |
| Tooling | Heavy-duty tools; work-hardens during machining |
| Coolant | Flood coolant recommended |
Forming Processes
| Process | Notes |
|---|---|
| Hot forming | 870–1230 °C; large deformations at 1040–1230 °C; avoid 650–870 °C |
| Cold forming | Readily formed by conventional methods; heavy-duty lubricants |
| Annealing between operations | Recommended for heavy cold reductions |
| Industry | Typical Components | Key Requirements |
|---|---|---|
| Thermal processing | Radiant tubes, muffles, retorts, furnace fixtures, mesh belts, baskets | Cyclic oxidation resistance to ~1250 °C |
| Aerospace | Combustion can-liners, jet engine igniters, gas turbine components | High-temperature strength + oxidation resistance |
| Chemical / petrochemical | Catalyst support grids (nitric acid), thermocouple protection tubes | Oxidation and carburisation resistance |
| Power generation | Steam superheater tube supports, high-temperature ducting | Strength and oxidation resistance at elevated temperature |
| Pollution control | Components for high-temperature gas handling | Cyclic oxidation resistance |
| Product Form | ASTM Standard | ASME Code | AMS Standard |
|---|---|---|---|
| Plate, sheet and strip | ASTM B168 · B906 | ASME SB-168 | AMS 5870 |
| Bar, rod and wire | ASTM B166 | ASME SB-166 | — |
| Seamless pipe and tube | ASTM B167 · B829 | ASME SB-167 | — |
| Welded pipe | ASTM B775 | — | — |
| Welded tube | ASTM B751 | — | — |
| Forgings | ASTM B564 | ASME SB-564 | — |
| Welding consumables | AWS A5.14 ERNiCrFe-11 | — | — |
| UNS | Ni % | Cr % | Fe % | Mo % | UTS (annealed) | Max Temp. | Best Used For |
|---|---|---|---|---|---|---|---|
| N06601 | 58–63 | 21–25 | balance | — | ≥550 MPa | ~1250 °C | Cyclic high-temp oxidation; radiant tubes |
| N06600 | ≥72 | 14–17 | 6–10 | — | ~655 MPa | ~1095 °C | General high-temp; carburisation/nitriding |
| N06625 | ≥58 | 20–23 | ≤5 | 8–10 | ~830 MPa | ~980 °C | Universal corrosion resistance; seawater |
| N06690 | ≥58 | 27–31 | 7–11 | — | ~690 MPa | ~1000 °C | Nuclear SCC resistance; high-Cr oxidation |
| N07718 | 50–55 | 17–21 | balance | 2.8–3.3 | ~1380 MPa (aged) | ~650 °C | High-strength weldable structures |




