Rene 41 Stainless Steels to SAE AMS 5712J (2006)

Rene 41 - Specification & Application

  • SAE AMS 5712J (2006) - Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution Heat Treated Precipitation Hardenable

Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution Heat Treated Precipitation Hardenable

Chemical composition(wt.%) of Rene 41 grade: to SAE AMS 5712J (2006)

Elements Min.(≥) Max.(≤) Similar Remarks
C - 0.09
Si - 0.25
Mn - 0.25
Cr - 19.00
Ni - remaining
Mo - 10.00
Co - 11.00
W - -
Al - 1.50
Cu - -
Ti - 3.10
Fe - 1.80
B - 0.005

Rene 41 - Detail

Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution Heat Treated Precipitation Hardenable

Mechanical properties of grade Rene 41 SAE AMS 5712J (2006)

Proof strength
Rp0.2 (MPa)
Tensile strength
Rm (MPa)
Impact energy
KV (J)
Elongation at fracture
A (%)
Reduction in cross section on fracture
Z (%)
As-Heat-Treated Condition Brinell hardness (HBW)
243 (≥) 298 (≥) 33 23 41 Solution and Aging, Annealing, Ausaging, Q+T,etc 213

Physical properties of grade Rene 41 SAE AMS 5712J (2006)

Property Density
kg/dm3
Temperature T
°C/F
Specific heat
J / kgK
Thermal conductivity
W/mK
Electric resistance
µΩ·cm
Modulus of elasticity
kN/mm2
Expansion rate
864 (≥) 557 (≥) 32 23 24 Solution and Aging, Annealing, Ausaging, Q+T,etc 213
Temp.
°C/°F
Creep strain limit
(10000h)
(Rp1,0) N/mm2
Creep rupture strength
(10000h)
(Rp1,0) N/mm2
863 736 489

Equivalent Products

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