Inconel X-750 Equalized and aged

Verifiedmetal

Inconel X-750 is a precipitation-hardened nickel-iron-base superalloy strengthened by gamma-double-prime (γ″) phase, designed for high-temperature applications in gas turbines, jet engines, and aerospace components requiring sustained strength to approximately 1300°F (704°C). The equalized and aged condition provides optimized strength and creep resistance through controlled heat treatment, with tensile yield strength typically in the 140–160 ksi range and superior bearing and shear strength characteristics suitable for critical fasteners and structural components.

aerospacestructural

Compliance & Regulations

?ITAR?EAR?Conflict Free?RoHS?REACH?TSCA?Prop 65
Inconel X-750/Inconel X-750 Equalized and aged
Property OverviewNormalized to typical max values
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Form
Thickness
e/D Ratio
PropertyValueUnitConditionsSource
Ultimate Bearing Strength(Fbru)4 entries
247
ksi22°C · Bar/Forging · Equalized and aged · AMS 5667 · t=<4.000 in · e/D=1.5
240
ksi22°C · Bar/Forging · Equalized and aged · AMS 5667 · t=4.000-10.000 in · e/D=1.5
313
ksi22°C · Bar/Forging · Equalized and aged · AMS 5667 · t=<4.000 in · e/D=2
304
ksi22°C · Bar/Forging · Equalized and aged · AMS 5667 · t=4.000-10.000 in · e/D=2
Bearing Yield Strength(Fbry)4 entries
157
ksi22°C · Bar/Forging · Equalized and aged · AMS 5667 · t=<4.000 in · e/D=1.5
150
ksi22°C · Bar/Forging · Equalized and aged · AMS 5667 · t=4.000-10.000 in · e/D=1.5
189
ksi22°C · Bar/Forging · Equalized and aged · AMS 5667 · t=<4.000 in · e/D=2
180
ksi22°C · Bar/Forging · Equalized and aged · AMS 5667 · t=4.000-10.000 in · e/D=2
Compressive Modulus(Ec)
30,600
ksi22°C · Strip
Compressive Yield Strength(Fcy)2 entries
105
ksi22°C · Bar/Forging · Equalized and aged · AMS 5667 · L · t=<4.000 in
100
ksi22°C · Bar/Forging · Equalized and aged · AMS 5667 · L · t=4.000-10.000 in
Elongation at Break(εf)2 entries
20.00
-22°C · Bar/Forging · Equalized and aged · AMS 5667 · L · t=<4.000 in
15.00
-22°C · Bar/Forging · Equalized and aged · AMS 5667 · L · t=4.000-10.000 in
Poisson's Ratio(ν)
0.3000
-22°C
Reduction of Area(RA)2 entries
25.00
-22°C · Bar/Forging · Equalized and aged · AMS 5667 · L · t=<4.000 in
17.00
-22°C · Bar/Forging · Equalized and aged · AMS 5667 · L · t=4.000-10.000 in
Shear Modulus(G)
11,800
ksi22°C · Strip
Ultimate Shear Strength(Fsu)2 entries
102
ksi22°C · Bar/Forging · Equalized and aged · AMS 5667 · t=<4.000 in
99.00
ksi22°C · Bar/Forging · Equalized and aged · AMS 5667 · t=4.000-10.000 in
Ultimate Tensile Strength(σUTS)2 entries
165
ksi22°C · Bar/Forging · Equalized and aged · AMS 5667 · L · t=<4.000 in
160
ksi22°C · Bar/Forging · Equalized and aged · AMS 5667 · L · t=4.000-10.000 in
Yield Strength (0.2% offset)(σy)2 entries
105
ksi22°C · Bar/Forging · Equalized and aged · AMS 5667 · L · t=<4.000 in
100
ksi22°C · Bar/Forging · Equalized and aged · AMS 5667 · L · t=4.000-10.000 in
Young's Modulus(E)
30,600
ksi22°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
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
CTE vs Temperature(α(T))
Curve (14 pts)
µin/in·°F
Specific Heat vs Temperature(Cp(T))
Curve (11 pts)
BTU/(lb·°F)
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
Density(ρ)
0.2980
lb/in³22°C
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source

Regulatory Screening

Environmental

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Quality & Standards

Industry-Specific

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.