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Inconel 718

2.4668
Nickel AlloysSuperalloy
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THE most widely used aerospace superalloy. Precipitation-hardened Ni-Cr-Fe alloy strengthened by gamma-prime and gamma-double-prime phases (Nb). Unique slow aging kinetics allow welding without cracking. UTS >1275 MPa aged. Used for gas turbine discs, jet engine components, rocket motors, cryogenic tanks, and oil/gas downhole tools. Service to 700°C.

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International equivalents

FlagStandardCountryGradeNumberMatch
🇺🇸ASTMUSAUNS N07718N07718REF
🇪🇺ENEuropeNiCr19Fe19Nb5Mo32.4668100%
🇺🇸AMSUSAAMS 5662/5663/5664100%
🇫🇷AFNORFranceNC19FeNb95%

Sources: ASTM B637, DIN 17752, AMS, AFNOR

Mechanical properties — Pro

Precipitation hardened

PropertyValueUnit
Tensile Strength
Yield Strength
Elongation
Hardness HB
Elastic Modulus
Density

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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.