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Inconel X-750

2.4669
Nickel AlloysSuperalloy
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Age-hardenable Ni-Cr-Fe superalloy for high-temperature spring and fastener applications. Strengthened by gamma-prime precipitation (Al+Ti). Oxidation and corrosion resistant to ~700°C service. Used for gas turbine springs, rocket engine thrust chambers, nuclear reactor components, and high-temp fasteners.

International equivalents

FlagStandardCountryGradeNumberMatch
🇺🇸ASTMUSAUNS N07750N07750REF
🇪🇺ENEuropeNiCr15Fe7TiAl2.4669100%
🇺🇸AMSUSAAMS 5542/5598/5667/5668—100%

Sources: ASTM B637, DIN 17742, AMS

Chemical composition comparison (wt%)

Side-by-side: Inconel X-750 (ASTM) (ASTM B637) vs NiCr15Fe7TiAl (EN)

ElementInconel X-750 (ASTM)NiCr15Fe7TiAl (EN)Overlap
C0–0.08%——
Si0–0.5%——
Mn0–1%——
S0–0.01%——
Cr14–17%——
Ni≥ 70%——
Cu0–0.5%——
Al0.4–1%——
Ti2.25–2.75%——
Nb0.7–1.2%——
Co0–1%——
Fe5–9%——

Mechanical properties

Precipitation hardened

PropertyValueUnit
Tensile Strength≥ 1100MPa
Yield Strength≥ 690MPa
Elongation≥ 20%
Hardness HRC30–38HRC
Elastic Modulus≥ 214GPa
Density≥ 8.28g/cm3

Heat treatment

ProcessTemperatureMediumHolding TimeNotes
solution_treating1150–1175 °Cair2-4 hoursEqualizing treatment for coarse grain (creep resistance)
stabilizing845–845 °Cair24 hoursStabilize carbides at grain boundaries
aging705–705 °Cair20 hoursPrecipitate gamma-prime. Air cool.

Compatibility verdict

Inconel X-750 and NiCr15Fe7TiAl: 100% composition match

Close equivalents but NOT identical.

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All data is for reference only. Equivalents indicate similarity, not identity. Always verify against the applicable specification for safety-critical applications. materialref.com accepts no liability for decisions based on this data.