Hastelloy X is a nickel-chromium-molybdenum-cobalt superalloy designed for high-temperature applications requiring excellent corrosion and oxidation resistance up to 2200°F (1204°C); the solution-treated condition provides optimal ductility and toughness for sheet and plate forms used in aerospace engines, heat exchangers, and thermal processing equipment, with typical yield strengths in the 40-50 ksi range and elongations exceeding 30%.
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10 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)) | Curve (16 pts) | ksi | 21°C · L | ||
Elongation at Break(εf) | 29.00 – 35.00 | - | 5 entriesClick to expand | ||
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)) | — | ksi | 9 entriesClick to expand | ||
Ultimate Tensile Strength(σUTS) | 95.00 – 106 | ksi | 7 entriesClick to expand | ||
Yield Strength (0.2% offset)(σy) | 40.00 – 47.00 | ksi | 7 entriesClick to expand | ||
Young's Modulus(E) | 29,800 | ksi | 22°C · Sheet/Plate | ||
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 (5 pts) | µin/in·°F | — | ||
Specific Heat vs Temperature(Cp(T)) | Curve (8 pts) | BTU/(lb·°F) | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (6 pts) | BTU/(hr·ft·°F) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 0.2970 | lb/in³ | 22°C |