Nickel, Corrosion and Heat-Resistant, Bars, Forgings, and Extrusions Thoria Dispersion Strengthened 2.2ThO2 Stress-Relieved
- Aerospace Material Specification
- AMS5890E
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Rings, Flash Welded Titanium and Titanium Alloys |
| Aerospace Material Specification | Steel, Welding Wire 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) Vacuum Melted, Environment Controlled Packaging |
| Aerospace Material Specification | Structural Examination of Titanium Alloys Etch-Anodize Inspection Procedure |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | COMPOSITION | |
| TABLE 2 | MINIMUM ROOM TEMPERATURE TENSILE PROPERTIES | |
| TABLE 3A | MINIMUM ELEVATED TEMPERATURE TENSILE PROPERTIES, INCH/POUND UNITS | |
| TABLE 3B | MINIMUM ELEVATED TEMPERATURE TENSILE PROPERTIES, SI UNITS | |
| TABLE 4 | STRESS RUPTURE 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.