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Precipitation Hardenable Steel Alloy, Corrosion and Heat-Resistant Powder for Additive Manufacturing 16.0Cr - 4.0Ni - 4.0Cu - 0.30Nb

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7012
  • Current
Published 2019-11-14 by SAE International in United States

This specification covers a corrosion and heat-resistant steel alloy in the form of pre-alloyed powder.

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Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 47.5Ni - 22Cr - 1.5Co - 9.0Mo - 0.60W - 18.5Fe

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7008
  • Current
Published 2019-03-26 by SAE International in United States
This specification covers a corrosion and heat-resistant nickel alloy in the form of pre-alloyed powder.
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Titanium Alloy, High Temperature Applications, Powder for Additive Manufacturing, Ti - 6.0Al - 2.0Sn - 4.0Zr - 2.0Mo

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7014
  • Current
Published 2019-03-11 by SAE International in United States
This specification covers a heat-resistant titanium alloy in the form of pre-alloyed powder.
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Titanium Alloy Preforms from Plasma Arc Directed Energy Deposition Additive Manufacturing on Substrate Ti-6Al-4V Stress Relieved

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7004
  • Current
Published 2019-01-31 by SAE International in United States
This specification covers preforms fabricated up through 5.5 inches (140 mm) inclusive in deposition width thickness (see 8.2.5) using a Plasma Arc Directed Energy Deposition (PA-DED) additive manufacturing process on a Ti-6Al-4V substrate that are subjected to post-deposition stress relief heat treatment. This is a wire fed additive manufacturing process. If required by the CEO, preforms may require subsequent machining to meet requirements for their intended final part application.
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Wire Fed Plasma Arc Directed Energy Deposition Additive Manufacturing Process

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7005
  • Current
Published 2019-01-31 by SAE International in United States
This specification establishes process controls for the repeatable production of preforms by Wire Fed Plasma Arc Directed Energy Deposition (PA-DED). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications.
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Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 60Ni - 22Cr - 2.0Mo - 14W - 0.35Al - 0.03La

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7013
  • Current
Published 2019-01-03 by SAE International in United States
The intended upper bound of this specification is that the particle size distribution (PSD) of powders supplied shall be <60 mesh (250 µm) and that no powder (0.0 wt.%) greater than 40 mesh (425 µm) is allowed.
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Laser Powder Bed Fusion Process

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7003
  • Current
Published 2018-06-08 by SAE International in United States
This specification establishes process controls for the repeatable production of aerospace parts by Laser Powder Bed Fusion (L-PBF). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications.
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Process Requirements for Production of Metal Powder Feedstock for Use in Additive Manufacturing of Aerospace Parts

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7002
  • Current
Published 2018-06-08 by SAE International in United States
This specification is to prescribe process requirements for production of metal powder feedstock for use in additive manufacturing of aerospace parts.
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Laser-Powder Bed Fusion (L-PBF) Produced Parts, Nickel Alloy, Corrosion and Heat-Resistant, 62Ni - 21.5Cr - 9.0Mo - 3.65Nb Stress Relieved, Hot Isostatic Pressed and Solution Annealed

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7000
  • Current
Published 2018-06-08 by SAE International in United States
This specification covers a corrosion and heat-resistant nickel alloy in the form of parts produced by laser-powder bed fusion (L-PBF) that are subjected to post-deposition stress relief (SR), hot isostatic press (HIP) and solution anneal operations. Parts may require subsequent machining or surface finishing to meet specific application requirements.
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Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 62Ni - 21.5Cr - 9.0Mo - 3.65Nb

AMS AM Additive Manufacturing Metals
  • Aerospace Material Specification
  • AMS7001
  • Current
Published 2018-06-08 by SAE International in United States
This specification covers a corrosion and heat-resistant nickel alloy in the form of pre-alloyed powder.
This content contains downloadable datasets
Annotation ability available