Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 64Ni - 5.0Cr - 24.5Mo - 5.5Fe Solution Heat Treated
- Aerospace Material Specification
- AMS5755G
- Reaffirmed
Scope
Rationale
Recommended Content
Aerospace Material Specification | Nickel-Iron Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 42.5Ni - 12.5Cr - 5.8Mo - 2.9Ti - 0.015B - 35Fe Consumable Electrode or Vacuum Induction Melted Solution, Stabilization, and Precipitation Heat Treated |
Aerospace Material Specification | Nickel-Copper Alloy, Corrosion Resistant, Bars and Forgings 66.5Ni - 2.9Al - 30Cu Annealed |
Aerospace Material Specification | Nickel-Copper Alloy, Corrosion-Resistant, Bars and Forgings 67Ni - 30Cu |
Topic
Data Sets - Support Documents
Title | Description | Download |
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Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE 1 | COMPOSITION | |
TABLE 2 | MINIMUM ELEVATED TEMPERATURE TENSILE PROPERTIES |
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.