Hastelloy X is a nickel-cobalt-chromium-molybdenum superalloy designed for high-temperature applications requiring excellent creep resistance and oxidation resistance up to 2200°F. Primary applications include jet engine components, gas turbine blades, and aerospace exhaust systems where sustained elevated-temperature strength and resistance to thermal fatigue are critical.
Compliance & Regulations
9 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 | |
|---|---|---|---|---|---|
Compressive Modulus(Ec) | 205.5 | GPa | 22°C · Sheet/Plate | ||
Compressive Tangent Modulus vs Stress(Etn(σ))3 entries | Curve (16 pts) | Pa | 21°C · L | ||
| ↳ | Curve (16 pts) | Pa | 371°C · L | ||
| ↳ | Curve (16 pts) | Pa | 482°C · L | ||
Poisson's Ratio(ν) | 0.3200 | - | 22°C | ||
Shear Modulus(G) | 77.91 | GPa | 22°C · Sheet/Plate | ||
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain))3 entries | Curve (10 pts) | Pa | 21°C · L | ||
| ↳ | Curve (10 pts) | Pa | 371°C · L | ||
| ↳ | Curve (10 pts) | Pa | 482°C · L | ||
Ultimate Tensile Strength(σUTS) | Curve (15 pts) | Pa | L | ||
Yield Strength (0.2% offset)(σy) | Curve (14 pts) | Pa | L | ||
Young's Modulus(E)2 entries | 205.5 | GPa | 22°C · Sheet/Plate | ||
| ↳ | Curve (7 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 (17 pts) | J/(kg·K) | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (17 pts) | W/(m·K) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 8.221 | kg/m³ | 22°C |