teel, Corrosion and Heat Resistant, Wire, 18Cr - 10.5Ni - 0.40Ti (SAE 30321), Solution Heat Treated
- Aerospace Material Specification
|Aerospace Material Specification||Steel, Corrosion and Heat Resistant, Wire 18Cr - 10.5Ni - 0.40Ti (321) Solution Heat Treated|
|Aerospace Material Specification||Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 46Fe – 20.5Cr – 32Ni – 1.1Ti Annealed|
|Aerospace Material Specification||Alloy Bars and Forgings, Corrosion and Heat Resistant, 38fe 13.2cr 38ni 5.5mo 0.85cb 2.5ti 1.6al 0.009b, Consumable Electrode Melted, Solution and Precipitation Heat Treated|
Data Sets - Support Documents
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.