Chromium 33 vs. N06975 Nickel

Chromium 33 belongs to the otherwise unclassified metals classification, while N06975 nickel belongs to the nickel alloys. They have 76% of their average alloy composition in common. There are 21 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.

For each property being compared, the top bar is chromium 33 and the bottom bar is N06975 nickel.

Chromium Alloy 33 (R20033)UNS N06975 Nickel Alloy

Metric UnitsUS Customary Units

Mechanical Properties

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

Elongation at Break, %		45
Elongation at Break, %		45

Poisson's Ratio		0.27
Poisson's Ratio		0.28

Shear Modulus, GPa		81
Shear Modulus, GPa		80

Tensile Strength: Ultimate (UTS), MPa		850
Tensile Strength: Ultimate (UTS), MPa		660

Tensile Strength: Yield (Proof), MPa		430
Tensile Strength: Yield (Proof), MPa		250

Thermal Properties

Latent Heat of Fusion, J/g		320
Latent Heat of Fusion, J/g		320

Specific Heat Capacity, J/kg-K		480
Specific Heat Capacity, J/kg-K		460

Thermal Expansion, µm/m-K		14
Thermal Expansion, µm/m-K		13

Otherwise Unclassified Properties

Base Metal Price, % relative		36
Base Metal Price, % relative		50

Density, g/cm³		7.9
Density, g/cm³		8.3

Embodied Carbon, kg CO₂/kg material		6.0
Embodied Carbon, kg CO₂/kg material		8.9

Embodied Energy, MJ/kg		84
Embodied Energy, MJ/kg		120

Embodied Water, L/kg		250
Embodied Water, L/kg		270

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m³		320
Resilience: Ultimate (Unit Rupture Work), MJ/m³		240

Resilience: Unit (Modulus of Resilience), kJ/m³		450
Resilience: Unit (Modulus of Resilience), kJ/m³		150

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

Stiffness to Weight: Bending, points		25
Stiffness to Weight: Bending, points		24

Strength to Weight: Axial, points		30
Strength to Weight: Axial, points		22

Strength to Weight: Bending, points		25
Strength to Weight: Bending, points		20

Thermal Shock Resistance, points		21
Thermal Shock Resistance, points		18

Alloy Composition

Carbon (C), %		0 to 0.015
Carbon (C), %		0 to 0.030

Chromium (Cr), %		31 to 35
Chromium (Cr), %		23 to 26

Copper (Cu), %		0.3 to 1.2
Copper (Cu), %		0.7 to 1.2

Iron (Fe), %		25.7 to 37.9
Iron (Fe), %		10.2 to 23.6

Manganese (Mn), %		0 to 2.0
Manganese (Mn), %		0 to 1.0

Molybdenum (Mo), %		0.5 to 2.0
Molybdenum (Mo), %		5.0 to 7.0

Nickel (Ni), %		30 to 33
Nickel (Ni), %		47 to 52

Nitrogen (N), %		0.35 to 0.6
Nitrogen (N), %		0

Phosphorus (P), %		0 to 0.020
Phosphorus (P), %		0 to 0.030

Silicon (Si), %		0 to 0.5
Silicon (Si), %		0 to 1.0

Sulfur (S), %		0 to 0.010
Sulfur (S), %		0 to 0.030

Titanium (Ti), %		0
Titanium (Ti), %		0.7 to 1.5