Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 41.5Ni - 16Cr - 37Fe - 2.9Cb (Nb) - 1.8Ti Consumable Electrode Remelted or Vacuum Induction Melted 1750 °F (954 °C) Solution Heat Treated
- Aerospace Material Specification
- AMS5702D
- Reaffirmed
Scope
Rationale
Recommended Content
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | COMPOSITION | |
| TABLE 2A | MINIMUM TENSILE PROPERTIES, INCH/POUND UNITS | |
| TABLE 2B | MINIMUM TENSILE PROPERTIES, SI UNITS |
Issuing Committee
AMS F Corrosion and Heat Resistant Alloys Committee
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.