Precipitation Hardenable Steel Alloy, Corrosion and Heat-Resistant Powder for Additive Manufacturing 16.0Cr - 4.0Ni - 4.0Cu - 0.30Nb
- Aerospace Material Specification
Published November 14, 2019 by SAE International in United States
This specification covers a corrosion and heat-resistant steel alloy in the form of pre-alloyed powder.
This purpose of this initial release is to produce a powder specification to cover alloy 630 powder for additive manufacturing applications.
|Aerospace Material Specification||Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 47.5Ni - 22Cr - 1.5Co - 9.0Mo - 0.60W - 18.5Fe|
|Aerospace Material Specification||Chemical Check Analysis Limits Titanium and Titanium Alloys|
|Aerospace Material Specification||Titanium Alloy Sheet 6Al - 4V Driver Sheet|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|Table 2||Oxygen Limits Based on Powder Classification|
|Table 3||Particle size distribution based on powder classification|
|Table 4||Testing Requirements|
Welcome to the SAE AMS AM, Additive Manufacturing public forum area.Scope: AMS AM is a technical committee in SAE’s Aerospace Materials Systems Group with the responsibility to develop and maintain aerospace material and process specifications and other SAE technical reports for additive manufacturing, including precursor material, additive processes, system requirements and post-build materials, pre-processing and post-processing, non-destructive testing and quality assurance.
* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.