HAYNES HR-120 is a nickel-based superalloy with cobalt and chromium additions designed for high-temperature structural applications in aerospace engines and gas turbines. The annealed condition provides optimal ductility and machinability while maintaining excellent creep resistance and oxidation protection up to approximately 1200°C.
Compliance & Regulations
1 interactive curve for this material
Stress-strain, S-N fatigue and environmental knockdown curves are free with an account.
Create free account| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Young's Modulus vs Temperature(E(T)) | Curve (19 pts) | Pa | — |
3 interactive curves for this material
Stress-strain, S-N fatigue and environmental knockdown curves are free with an account.
Create free account| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
CTE vs Temperature(α(T)) | Curve (17 pts) | 1/K | — | ||
Specific Heat vs Temperature(Cp(T)) | Curve (23 pts) | J/(kg·K) | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (24 pts) | W/(m·K) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 8.968 | kg/m³ | 22°C |