Inconel X-750 Annealed
VerifiedmetalInconel X-750 is a precipitation-hardenable nickel-chromium superalloy with aluminum and titanium additions, used primarily in aerospace gas turbine engines, fasteners, and high-temperature structural applications requiring strength retention to approximately 1300°F (700°C). The annealed condition provides a softened baseline microstructure suitable for machining and forming prior to age hardening, with moderate strength and good ductility as supplied per AMS 5542.
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Property OverviewNormalized to typical max values
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Thickness
e/D Ratio
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Ultimate Bearing Strength(Fbru)4 entries | 1.703 | GPa | 22°C · Sheet · Annealed and aged · AMS 5542 · t=0.010-0.187 in · e/D=1.5 | ||
| ↳ | 1.600 | GPa | 22°C · Plate · Annealed and aged · AMS 5542 · t=0.188-4.000 in · e/D=1.5 | ||
| ↳ | 2.158 | GPa | 22°C · Sheet · Annealed and aged · AMS 5542 · t=0.010-0.187 in · e/D=2 | ||
| ↳ | 2.027 | GPa | 22°C · Plate · Annealed and aged · AMS 5542 · t=0.188-4.000 in · e/D=2 | ||
Bearing Yield Strength(Fbry)4 entries | 1.082 | GPa | 22°C · Sheet · Annealed and aged · AMS 5542 · t=0.010-0.187 in · e/D=1.5 | ||
| ↳ | 1.034 | GPa | 22°C · Plate · Annealed and aged · AMS 5542 · t=0.188-4.000 in · e/D=1.5 | ||
| ↳ | 1.303 | GPa | 22°C · Sheet · Annealed and aged · AMS 5542 · t=0.010-0.187 in · e/D=2 | ||
| ↳ | 1.241 | GPa | 22°C · Plate · Annealed and aged · AMS 5542 · t=0.188-4.000 in · e/D=2 | ||
Compressive Modulus(Ec) | 211.0 | GPa | 22°C · Strip | ||
Compressive Yield Strength(Fcy)2 entries | 723.9 | MPa | 22°C · Sheet · Annealed and aged · AMS 5542 · LT · t=0.010-0.187 in | ||
| ↳ | 689.5 | MPa | 22°C · Plate · Annealed and aged · AMS 5542 · LT · t=0.188-4.000 in | ||
Elongation at Break(εf)3 entries | 15.00 | - | 22°C · Strip · Annealed and aged · AMS 5542 · LT · t=≥0.010 in | ||
| ↳ | 20.00 | - | 22°C · Sheet · Annealed and aged · AMS 5542 · LT · t=0.010-0.187 in | ||
| ↳ | 20.00 | - | 22°C · Plate · Annealed and aged · AMS 5542 · LT · t=0.188-4.000 in | ||
Poisson's Ratio(ν) | 0.3000 | - | 22°C | ||
Shear Modulus(G) | 81.36 | GPa | 22°C · Strip | ||
Ultimate Shear Strength(Fsu)2 entries | 737.7 | MPa | 22°C · Sheet · Annealed and aged · AMS 5542 · t=0.010-0.187 in | ||
| ↳ | 689.5 | MPa | 22°C · Plate · Annealed and aged · AMS 5542 · t=0.188-4.000 in | ||
Ultimate Tensile Strength(σUTS)4 entries | 1.069 | GPa | 22°C · Plate · Annealed and aged · AMS 5542 · LT · t=0.188-4.000 in | ||
| ↳ | 1.034 | GPa | 22°C · Strip · Annealed and aged · AMS 5542 · LT · t=≤0.009 in | ||
| ↳ | 1.069 | GPa | 22°C · Strip · Annealed and aged · AMS 5542 · LT · t=≥0.010 in | ||
| ↳ | 1.138 | GPa | 22°C · Sheet · Annealed and aged · AMS 5542 · LT · t=0.010-0.187 in | ||
Yield Strength (0.2% offset)(σy)2 entries | 723.9 | MPa | 22°C · Sheet · Annealed and aged · AMS 5542 · LT · t=0.010-0.187 in | ||
| ↳ | 689.5 | MPa | 22°C · Plate · Annealed and aged · AMS 5542 · LT · t=0.188-4.000 in | ||
Young's Modulus(E) | 211.0 | GPa | 22°C · Strip |
N entriesMultiple entries per property — large groups are collapsed; click a summary row to expand. Use filters above to narrow by form / heat treatment / basis.
Rows with are inherited from the base material
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| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
CTE vs Temperature(α(T)) | Curve (14 pts) | 1/K | — | ||
Specific Heat vs Temperature(Cp(T)) | Curve (11 pts) | J/(kg·K) | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 8.249 | kg/m³ | 22°C |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
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RoHS, REACH, and Prop 65 statuses are validated against official substance lists (ECHA SVHC Candidate List, OEHHA Prop 65, RoHS Annex II). Other regulations are estimated from composition and material classification. All screening is a starting point for due diligence — always verify with your supplier before making compliance decisions.