SAE AMS6478B-2005
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 (UNS K92580)
- Standard No.
- SAE AMS6478B-2005
- Release Date
- 2005
- Published By
- SAE - SAE International
- Status
- 2005-09
- Latest
- SAE AMS6478B-2005
- Scope
- Form: This specification covers a premium aircraft-quality alloy steel in the form of bars@ forgings@ and forging stock. Application: 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 heat treatment should attain a minimum tensile strength of 290 ksi (1999 MPa) and yield strength of 245 ksi (1689 MPa).
SAE AMS6478B-2005 history
- 2005 SAE AMS6478B-2005 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 (UNS K92580)
- 2001 SAE AMS6478A-2001 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 UNS K92580
- 2000 SAE AMS6478-2000 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
- 1994 SAE AMS6478-1994 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 (UNS K92580)
