N10665 Nickel vs. 60Cr-40Ni Alloy

N10665 nickel belongs to the nickel alloys classification, while 60Cr-40Ni alloy belongs to the otherwise unclassified metals. They have a modest 39% of their average alloy composition in common, which, by itself, doesn't mean much. There are 19 material properties with values for both materials. Properties with values for just one material (12, in this case) are not shown.

For each property being compared, the top bar is N10665 nickel and the bottom bar is 60Cr-40Ni alloy.

UNS N10665 (2.4617, NiMo28) Nickel-Molybdenum Alloy 60Cr-40Ni (R20600) Casting Alloy

Metric UnitsUS Customary Units

Mechanical Properties

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

Poisson's Ratio		0.31
Poisson's Ratio		0.25

Shear Modulus, GPa		84
Shear Modulus, GPa		87

Tensile Strength: Ultimate (UTS), MPa		860
Tensile Strength: Ultimate (UTS), MPa		870

Tensile Strength: Yield (Proof), MPa		400
Tensile Strength: Yield (Proof), MPa		660

Thermal Properties

Latent Heat of Fusion, J/g		310
Latent Heat of Fusion, J/g		370

Specific Heat Capacity, J/kg-K		390
Specific Heat Capacity, J/kg-K		490

Thermal Expansion, µm/m-K		10
Thermal Expansion, µm/m-K		16

Otherwise Unclassified Properties

Base Metal Price, % relative		75
Base Metal Price, % relative		49

Density, g/cm³		9.3
Density, g/cm³		7.8

Embodied Carbon, kg CO₂/kg material		15
Embodied Carbon, kg CO₂/kg material		7.4

Embodied Energy, MJ/kg		200
Embodied Energy, MJ/kg		110

Embodied Water, L/kg		270
Embodied Water, L/kg		380

Common Calculations

Resilience: Unit (Modulus of Resilience), kJ/m³		360
Resilience: Unit (Modulus of Resilience), kJ/m³		1000

Stiffness to Weight: Axial, points		13
Stiffness to Weight: Axial, points		16

Stiffness to Weight: Bending, points		22
Stiffness to Weight: Bending, points		26

Strength to Weight: Axial, points		26
Strength to Weight: Axial, points		31

Strength to Weight: Bending, points		22
Strength to Weight: Bending, points		26

Thermal Shock Resistance, points		27
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), %		0 to 1.0
Chromium (Cr), %		58 to 62

Cobalt (Co), %		0 to 1.0
Cobalt (Co), %		0

Iron (Fe), %		0 to 2.0
Iron (Fe), %		0 to 1.0

Manganese (Mn), %		0 to 1.0
Manganese (Mn), %		0 to 0.3

Molybdenum (Mo), %		26 to 30
Molybdenum (Mo), %		0

Nickel (Ni), %		64.8 to 74
Nickel (Ni), %		34.5 to 42

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

Phosphorus (P), %		0 to 0.040
Phosphorus (P), %		0 to 0.020

Silicon (Si), %		0 to 0.1
Silicon (Si), %		0 to 1.0

Sulfur (S), %		0 to 0.030
Sulfur (S), %		0 to 0.020

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