Chromium 33 vs. N10624 Nickel

Chromium 33 belongs to the otherwise unclassified metals classification, while N10624 nickel belongs to the nickel alloys. They have 48% of their average alloy composition in common. There are 21 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.

For each property being compared, the top bar is chromium 33 and the bottom bar is N10624 nickel.

Chromium Alloy 33 (R20033)UNS N10624 Nickel-Molybdenum Alloy

Metric UnitsUS Customary Units

Mechanical Properties

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

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

Poisson's Ratio		0.27
Poisson's Ratio		0.3

Shear Modulus, GPa		81
Shear Modulus, GPa		84

Tensile Strength: Ultimate (UTS), MPa		850
Tensile Strength: Ultimate (UTS), MPa		810

Tensile Strength: Yield (Proof), MPa		430
Tensile Strength: Yield (Proof), MPa		360

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		410

Thermal Expansion, µm/m-K		14
Thermal Expansion, µm/m-K		11

Otherwise Unclassified Properties

Base Metal Price, % relative		36
Base Metal Price, % relative		70

Density, g/cm³		7.9
Density, g/cm³		9.0

Embodied Carbon, kg CO₂/kg material		6.0
Embodied Carbon, kg CO₂/kg material		13

Embodied Energy, MJ/kg		84
Embodied Energy, MJ/kg		170

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		300

Resilience: Unit (Modulus of Resilience), kJ/m³		450
Resilience: Unit (Modulus of Resilience), kJ/m³		300

Stiffness to Weight: Axial, points		14
Stiffness to Weight: Axial, points		13

Stiffness to Weight: Bending, points		25
Stiffness to Weight: Bending, points		22

Strength to Weight: Axial, points		30
Strength to Weight: Axial, points		25

Strength to Weight: Bending, points		25
Strength to Weight: Bending, points		22

Thermal Shock Resistance, points		21
Thermal Shock Resistance, points		24

Alloy Composition

Aluminum (Al), %		0
Aluminum (Al), %		0 to 0.5

Carbon (C), %		0 to 0.015
Carbon (C), %		0 to 0.010

Chromium (Cr), %		31 to 35
Chromium (Cr), %		6.0 to 10

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

Copper (Cu), %		0.3 to 1.2
Copper (Cu), %		0 to 0.5

Iron (Fe), %		25.7 to 37.9
Iron (Fe), %		5.0 to 8.0

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

Molybdenum (Mo), %		0.5 to 2.0
Molybdenum (Mo), %		21 to 25

Nickel (Ni), %		30 to 33
Nickel (Ni), %		53.9 to 68

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

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

Silicon (Si), %		0 to 0.5
Silicon (Si), %		0 to 0.1

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