Steel, Corrosion-Resistant, Bars, Wire, and Forgings 17Cr - 0.52Mo (0.95 - 1.20C) Powder Metallurgy Product, Hot Isostatically Pressed
- Aerospace Material Specification
- AMS5899B
- Revised
Scope
Rationale
Recommended Content
Aerospace Material Specification | Steel, Corrosion Resistant, Bars, Wire, and Forgings 17Cr - 0.52Mo (0.95 - 1.20C) Powder Metallurgy Product, Hot Isostatically Pressed |
Aerospace Material Specification | Steel Bars and Forgings 1.8Ni - 0.25Mo (0.38 - 0.43C) (4640) Heat Treated, 125 ksi (862 MPa) Tensile Strength |
Aerospace Material Specification | Steel Bars and Forgings 3.5Cr - 7.5Ni - 16.3Co - 1.75Mo - 0.2W - (0.09 - 0.13C) Double Vacuum Melted, Normalized, Annealed |
Topic
Data Sets - Support Documents
Title | Description | Download |
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Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE 1 | COMPOSITION | |
TABLE 2A | MAXIMUM DECARBURIZATION, INCH/POUND UNITS | |
TABLE 2B | MAXIMUM DECARBURIZATION, 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.