STEP 1
High-Temperature Strength
Nimonic 80A sustains outstanding mechanical strength at temperatures up to 815 °C, delivering long-term durability for rigorous applications such as jet engines and gas turbines.

Nimonic 80A is a precipitation-hardened nickel-chromium alloy featuring exceptional mechanical properties and superior thermal fatigue resistance. Engineered for rigorous high-temperature service conditions, this alloy maintains stable structural strength and excellent oxidation resistance in extreme operating environments, with minimal performance degradation under prolonged high-heat exposure.
Nimonic 80A, designated as UNS N07080, is a premium nickel-chromium alloy compliant with multiple authoritative industrial standards, including ASTM B637, DIN/EN 2.4952 (NiCr20TiAl), BS HR 1, GB/T 14992 (GH4033), and AMS 5828.
Nimonic 80A is a precipitation-hardened nickel-chromium alloy featuring exceptional mechanical properties and superior thermal fatigue resistance. Engineered for rigorous high-temperature service conditions, this alloy maintains stable structural strength and excellent oxidation resistance in extreme operating environments, with minimal performance degradation under prolonged high-heat exposure.
Widely applied in the aerospace and energy industries, Nimonic 80A is a preferred material for manufacturing turbine blades, high-temperature valves, exhaust system components, and nuclear reactor parts. It delivers outstanding durability and consistent operational stability under cyclic thermal stress, guaranteeing high reliability for critical and high-precision industrial applications with an extended service lifespan.
The chemical composition of Nimonic 80A delivers an optimal balance of strength, oxidation resistance and thermal stability. Nickel endows the alloy with excellent toughness, while chromium improves its corrosion resistance. Titanium and aluminum enable precipitation hardening, which further boosts mechanical strength.
| Element | Composition (%) |
|---|---|
| Nickel (Ni) | 70.0 min |
| Chromium (Cr) | 18.0 – 21.0 |
| Titanium (Ti) | 1.8 – 2.7 |
| Iron (Fe) | 3.0 max |
| Aluminum (Al) | 1.0 – 1.8 |
| Others | Trace elements |
| Property | Values |
|---|---|
| Density | 8.31 g/cm³ |
| Melting Point | 1380°C |
| Thermal Conductivity | 12.1 W/(m·K) |
| Modulus of Elasticity | 208 GPa |
Nimonic 80A adopts a face-centered cubic (FCC) crystal structure, a common characteristic of nickel-based alloys that endows the material with high strength and superior thermal fatigue resistance. Aluminum and titanium form intermetallic precipitates, further optimizing its mechanical performance.
The alloy retains stable microstructure even after long-term high-temperature exposure, effectively inhibiting grain growth and phase transformation. Such structural stability enables it to sustain mechanical strength and creep resistance under extreme service conditions.
Aerospace & Aviation
Power Generation
Oil & Gas
General Energy
Marine
Mining
Automotive
Chemical Processing
Food & Pharmaceutical Processing
Military & Defense
Nuclear Industry