Chemical Composition (wt.%): Element Content Ni Balance Cr 14-17 Ti ≈2.5 Al ≈2.5 Fe ≤10

Mechanical Properties: Property Typical Value Tensile Strength ≈930 MPa Yield Strength ≈620 MPa Elongation ≥10%

Applications: Aerospace components Gas turbine parts High-temperature fasteners

Chemical Composition (wt.%): Element Content Ni Balance Cr 14-17 Ti ≈2.5 Al ≈2.5 Fe ≤10

Mechanical Properties: Property Typical Value Tensile Strength ≈930 MPa Yield Strength ≈620 MPa Elongation ≥10%

Applications: Aerospace components Gas turbine parts High-temperature fasteners

Alloy 702 / UNS N07702

Grade: Inconel 702 / UNS N07702/Alloy 702/Nickel Alloy 702

Sheet/Plate: 0.3mm-150mm

Strip/Foil: 0.02mm-16mm

Pipe: 6mm*0.5mm-1200mm*100mm

Bar: Ф6mm – Ф600mm

Wire: Ф0.01mm – Ф6mm

Others: Forged Rings, Flanges, Elbows, Tees, Reducers etc.

Standard: ASTM/ASME/AMS

INCONEL 702 is a precipitation-hardenable nickel-chromium alloy developed for high strength and oxidation resistance at elevated temperatures. It maintains good mechanical properties under thermal cycling and is suitable for demanding aerospace and industrial applications.

Chemical Composition (wt.%):