Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 65ni 15.8cr 15.2mo 0.30al 0.05la, Consumable Electrode Melted, Solution Heat Treated
- Aerospace Material Specification
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate.
These products have been used typically for formed and drawn parts, such as turbine seals, burner liners, exhaust cone assemblies, and nozzle diaphragm vanes, requiring relatively high strength up to 1800 degrees F (982 degrees C) and oxidation resistance up to 2000 degrees F (1093 degrees C), but usage is not limited to such applications.
Data Sets - Support Documents
The committee of Corrosion and Heat Resistant Steels and Alloys and Specialty Steels and Alloys, AMS Committee F, will prepare, coordinate, and revise documents related to corrosion and heat resistant steels and alloys and specialty steels and alloys technology, such as stainless steels and nickel and base alloys, through the participation of metals suppliers, users, and interested government agencies. Committee activities shall provide a forum for the cooperative interchange of ideas and experience of the participants, resulting in the publication of specifications that embody sound, established aerospace industry practices and requirements to serve the suppliers and customers of aerospace materials.