EN 1.4466 Stainless Steel vs. 60Cr-40Ni Alloy

EN 1.4466 stainless steel belongs to the iron alloys classification, while 60Cr-40Ni alloy belongs to the otherwise unclassified metals. They have 48% of their average alloy composition in common. There are 19 material properties with values for both materials. Properties with values for just one material (15, in this case) are not shown.

For each property being compared, the top bar is EN 1.4466 stainless steel and the bottom bar is 60Cr-40Ni alloy.

EN 1.4466 (X1CrNiMoN25-22-2) Stainless Steel 60Cr-40Ni (R20600) Casting Alloy

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa		200
Elastic (Young's, Tensile) Modulus, GPa		220

Poisson's Ratio		0.28
Poisson's Ratio		0.25

Shear Modulus, GPa		80
Shear Modulus, GPa		87

Tensile Strength: Ultimate (UTS), MPa		640
Tensile Strength: Ultimate (UTS), MPa		870

Tensile Strength: Yield (Proof), MPa		280
Tensile Strength: Yield (Proof), MPa		660

Thermal Properties

Latent Heat of Fusion, J/g		300
Latent Heat of Fusion, J/g		370

Specific Heat Capacity, J/kg-K		470
Specific Heat Capacity, J/kg-K		490

Thermal Expansion, µm/m-K		16
Thermal Expansion, µm/m-K		16

Otherwise Unclassified Properties

Base Metal Price, % relative		28
Base Metal Price, % relative		49

Density, g/cm³		7.9
Density, g/cm³		7.8

Embodied Carbon, kg CO₂/kg material		5.0
Embodied Carbon, kg CO₂/kg material		7.4

Embodied Energy, MJ/kg		70
Embodied Energy, MJ/kg		110

Embodied Water, L/kg		200
Embodied Water, L/kg		380

Common Calculations

Resilience: Unit (Modulus of Resilience), kJ/m³		200
Resilience: Unit (Modulus of Resilience), kJ/m³		1000

Stiffness to Weight: Axial, points		14
Stiffness to Weight: Axial, points		16

Stiffness to Weight: Bending, points		25
Stiffness to Weight: Bending, points		26

Strength to Weight: Axial, points		22
Strength to Weight: Axial, points		31

Strength to Weight: Bending, points		21
Strength to Weight: Bending, points		26

Thermal Shock Resistance, points		14
Thermal Shock Resistance, points		18

Alloy Composition

Aluminum (Al), %		0
Aluminum (Al), %		0 to 0.25

Carbon (C), %		0 to 0.020
Carbon (C), %		0 to 0.1

Chromium (Cr), %		24 to 26
Chromium (Cr), %		58 to 62

Iron (Fe), %		45.6 to 52.9
Iron (Fe), %		0 to 1.0

Manganese (Mn), %		0 to 2.0
Manganese (Mn), %		0 to 0.3

Molybdenum (Mo), %		2.0 to 2.5
Molybdenum (Mo), %		0

Nickel (Ni), %		21 to 23
Nickel (Ni), %		34.5 to 42

Nitrogen (N), %		0.1 to 0.16
Nitrogen (N), %		0 to 0.3

Phosphorus (P), %		0 to 0.025
Phosphorus (P), %		0 to 0.020

Silicon (Si), %		0 to 0.7
Silicon (Si), %		0 to 1.0

Sulfur (S), %		0 to 0.010
Sulfur (S), %		0 to 0.020

Titanium (Ti), %		0
Titanium (Ti), %		0 to 0.5