STEEL Chromium Molybdenum
- Aerospace Material Specification
|Technical Paper||Optimizing Forgings for Automotive Transmission Hubs by Warm Forming Vanadium-Microalloyed Steels|
|Aerospace Material Specification||Wire, Steel 0.18 - 0.23C (SAE 1020) Annealed|
|Aerospace Material Specification||Carbon Steel, Sheet, Strip, and Plate (SAE 1020 and 1025)|
Data Sets - Support Documents
|Unnamed Dataset 1|
The committee of Carbon and Low Alloy Steels, AMS Committee E, shall prepare, coordinate, and revise documents related to carbon and low alloy steels technology, such as steel cleanliness and steel quality assurance sampling, 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.