Alloy, Corrosion and Heat Resistant, Welded Tubing 32Fe - 21Cr - 20Ni - 20Co - 3Mo - 2.5W - 1.0Cb (Nb) - 0.15N Solution Heat Treated
- Aerospace Material Specification
- AMS5585G
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Steel, Corrosion Resistant, Sheet, Strip, and Plate 18Cr - 8.5Ni (302) Solution Heat Treated, High Ductility |
| Aerospace Material Specification | Steel, Corrosion and Heat Resistant, Tubing, Seamless 12.5Cr (410) Annealed |
| Aerospace Material Specification | Steel, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 12.5Cr (410) Annealed |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | COMPOSITION | |
| TABLE 2 | TENSILE PROPERTIES | |
| TABLE 3A | MINIMUM PERMANENT EXPANDED OD, INCH/POUND UNITS | |
| TABLE 3B | MINIMUM PERMANENT EXPANDED OD, 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.