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Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 62Ni - 21.5Cr - 9.0Mo - 3.65Nb
- Aerospace Material Specification
- AMS7001
- Issued
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This specification covers a corrosion and heat-resistant nickel alloy in the form of pre-alloyed powder.
Rationale
This Aerospace Material Specification is intended to provide the technical requirements such as alloy composition, particle size distribution for both feedstock and as-built part materials via the laser powder bed additive manufacturing process. No such specification currently exists.
Recommended Content
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Table 1 | Composition | |
| Table 2 | Oxygen limits based on powder classification | |
| Table 3 | Particle size distribution based on powder classification | |
| Table 4 | Testing requirements |
Issuing Committee
AMS AM Additive Manufacturing Metals
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.Reference
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