Alloy 263 NIMONIC® 263 is a precipitation-hardenable nickel-cobalt-chromium-molybdenum-based alloy, originally developed by Rolls-Royce to offer excellent machinability and high ductility in welds, as a replacement for alloy 80A.
Designed for gas turbine sheet metal components, it is now available in all standard forms, including bars, sheets and tubes. It maintains high mechanical properties and creep resistance up to approximately 800°C, making it ideal for aerospace and industrial applications.
Reference standards:
AMS 5872 (sheet, plate and strip)
BS HR 10, HR 206, HR 404
DIN 17750, 17751, 17752, 17753, 17754
AECMA PrEn 2199–2203, 2418
UNS N07263 / W. Nr. 2.4650
| Element | Value (%) |
|---|---|
| Nickel (Ni) | Balance |
| Cobalt (Co) | 19.0 – 21.0 |
| Chromium (Cr) | 19.0 – 21.0 |
| Molybdenum (Mo) | 5.6 – 6.1 |
| Titanium (Ti) | 1.9 – 2.4 |
| Aluminium (Al) | up to 0.6 |
| Iron (Fe) | up to 0.7 |
| Manganese (Mn) | up to 0.6 |
| Silicon (Si) | up to 0.4 |
| Carbon (C) | 0.04 – 0.08 |
| Sulphur, Phosphorus, Boron, Bismuth, Lead | Traces |
| Temperature (°C) | 0.2% Yield Strength (MPa) | Rm (MPa) | Elongation (%) |
|---|---|---|---|
| 20 | 585 | 1004 | 45 |
| 400 | 490 | 849 | 46 |
| 800 | 460 | 772 | 27 |
| 1000 | 145 | 232 | 15 |
| Temperature (°C) | 0.2% Yield Strength (MPa) | Rm (MPa) | Elongation (%) |
|---|---|---|---|
| 20 | 580 | 973 | 39 |
| 400 | 470 | 816 | 43 |
| 800 | 440 | 757 | 23 |
| 1000 | 135 | 201 | 20 |
Density: 8.36 g/cm³
Melting range: 1300 – 1355°C
Specific heat: 461 J/kg·K
Thermal conductivity (20°C): 11.72 W/m·K
Electrical resistivity (20°C): 115 µΩ·cm
Young’s modulus: 224 GPa (at 20°C)
Thermal expansion (20-1000°C): 10.3–18.9 ×10⁻⁶ /°C
Solution treatment: 1150°C for 2h (bars) or 3–10 min (sheet), with rapid cooling (WQ or FBQ)
Aging: 800°C for 8h with air cooling
Interstage: 1050–1100°C for 15 min to eliminate work hardening
NIMONIC® Alloy 263 is available in:
Thanks to its excellent creep resistance, thermal fatigue resistance and weldability, NIMONIC® 263 is used in:
Aerospace and Defence: Combustion chambers, turbine blades, structural rings.
Power Generation: Components for gas turbines and engines.
Chemical and Pharmaceutical Industry: Components subject to cyclic heat and corrosion.
Motorsport: Exhausts and manifolds in high-temperature environments.
Nuclear: High-integrity components exposed to heat and radiation.
Oil & Gas: Structural parts resistant to oxidation and fatigue.