AMS6478B Steel, Bars and Forgings, 3.1Cr - 11.5Ni - 13.5Co - 1.2Mo (0.21 - 0.25C), Vacuum Melted, Annealed, Heat Treatable to 290 ksi (1999 MPa) Tensile Strength

Canceled

09/30/2005

Scope
Content

This specification covers a premium aircraft-quality alloy steel in the form of bars, forgings, and forging stock.

These products have been used typically for parts requiring a combination of high strength, high toughness, and weldability, but usage is not limited to such applications. Product after proper heat treatment should attain a minimum tensile strength of 290 ksi (1999 MPa) and yield strength of 245 ksi (1689 MPa).

Meta TagsDetails
DOI
https://doi.org/10.4271/AMS6478B
Pages
9
Citation
SAE International Material Specification, Steel, Bars and Forgings, 3.1Cr - 11.5Ni - 13.5Co - 1.2Mo (0.21 - 0.25C), Vacuum Melted, Annealed, Heat Treatable to 290 ksi (1999 MPa) Tensile Strength, SAE Standard AMS6478B, Cancelled September 2005, https://doi.org/10.4271/AMS6478B.
Additional Details
Publisher
Published
Sep 30, 2005
Product Code
AMS6478B
Content Type
Material Specification
Status
Canceled
Language
English

Revisions