STEP 1
High-Temperature Strength
PWA 1480 retains excellent tensile strength of up to 1250 MPa at elevated temperatures, delivering reliable performance for jet engines and industrial turbines.

PWA 1480 is a first-generation high-performance single-crystal nickel-base superalloy, developed mainly for high-temperature aerospace components including gas turbine blades and vanes in aircraft engines.
PWA 1480 is a high performance single-crystal superalloy engineered to deliver outstanding mechanical properties at elevated temperatures. Widely deployed for jet engine turbine blades, it exhibits excellent resistance to thermal fatigue and creep at temperatures above 980°C.
The alloy features a carefully balanced composition of nickel, chromium, cobalt and tantalum, which imparts corrosion resistance, mechanical strength and stability under extreme operating conditions. Its single-crystal microstructure removes grain boundaries, thereby enhancing mechanical performance and fatigue life at high temperatures.
| Element | PWA 1480 |
|---|---|
| Chromium (Cr) | 10% |
| Cobalt (Co) | 5% |
| Molybdenum (Mo) | 2% |
| Tungsten (W) | 4% |
| Aluminium (Al) | 5% |
| Tantalum (Ta) | 12% |
| Hafnium (Hf) | 1.5% |
| Nickel (Ni) | Bal. |