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.
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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) | 29,800 | ksi | 22°C · Sheet/Plate | ||
Compressive Tangent Modulus vs Stress(Etn(σ))3 entries | Curve (16 pts) | ksi | 21°C · L | ||
| ↳ | Curve (16 pts) | ksi | 371°C · L | ||
| ↳ | Curve (16 pts) | ksi | 482°C · L | ||
Poisson's Ratio(ν) | 0.3200 | - | 22°C | ||
Shear Modulus(G) | 11,300 | ksi | 22°C · Sheet/Plate | ||
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain))3 entries | Curve (10 pts) | ksi | 21°C · L | ||
| ↳ | Curve (10 pts) | ksi | 371°C · L | ||
| ↳ | Curve (10 pts) | ksi | 482°C · L | ||
Ultimate Tensile Strength(σUTS) | Curve (15 pts) | ksi | L | ||
Yield Strength (0.2% offset)(σy) | Curve (14 pts) | ksi | L | ||
Young's Modulus(E)2 entries | 29,800 | ksi | 22°C · Sheet/Plate | ||
| ↳ | Curve (7 pts) | ksi | — |
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) | µin/in·°F | — | ||
Specific Heat vs Temperature(Cp(T)) | Curve (17 pts) | BTU/(lb·°F) | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (17 pts) | BTU/(hr·ft·°F) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 0.2970 | lb/in³ | 22°C |