A nickel-iron-chromium alloy precipitation hardened by titanium and aluminum and solid-solution strengthened by an addition of molybdenum. It was developed as a high-strength sheet alloy for use at temperatures to 1020°F (550°C). The high iron content provides good workability and also relatively high tensile ductility, especially after welding. Used for components of gas turbines.

UNS: N09901
W.Nr.: 2.4662

Technical Bulletin (PDF, 80KB)

Available Product Forms: Sheet, plate, round bar, flat bar, forging stock and wire

Technical Papers
n/a

<<Back to Previous Page