Chromium 33 vs. Nickel 200

Chromium 33 belongs to the otherwise unclassified metals classification, while nickel 200 belongs to the nickel alloys. They have a modest 32% of their average alloy composition in common, which, by itself, doesn't mean much. There are 21 material properties with values for both materials. Properties with values for just one material (11, in this case) are not shown.

For each property being compared, the top bar is chromium 33 and the bottom bar is nickel 200.

Chromium Alloy 33 (R20033)Nickel Alloy 200 (2.4066, N02200, NA11)

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa		200
Elastic (Young's, Tensile) Modulus, GPa		180

Elongation at Break, %		45
Elongation at Break, %		23 to 44

Poisson's Ratio		0.27
Poisson's Ratio		0.31

Shear Modulus, GPa		81
Shear Modulus, GPa		70

Tensile Strength: Ultimate (UTS), MPa		850
Tensile Strength: Ultimate (UTS), MPa		420 to 540

Tensile Strength: Yield (Proof), MPa		430
Tensile Strength: Yield (Proof), MPa		120 to 370

Thermal Properties

Latent Heat of Fusion, J/g		320
Latent Heat of Fusion, J/g		290

Specific Heat Capacity, J/kg-K		480
Specific Heat Capacity, J/kg-K		450

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

Otherwise Unclassified Properties

Base Metal Price, % relative		36
Base Metal Price, % relative		65

Density, g/cm³		7.9
Density, g/cm³		8.9

Embodied Carbon, kg CO₂/kg material		6.0
Embodied Carbon, kg CO₂/kg material		11

Embodied Energy, MJ/kg		84
Embodied Energy, MJ/kg		150

Embodied Water, L/kg		250
Embodied Water, L/kg		230

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m³		320
Resilience: Ultimate (Unit Rupture Work), MJ/m³		110 to 150

Resilience: Unit (Modulus of Resilience), kJ/m³		450
Resilience: Unit (Modulus of Resilience), kJ/m³		42 to 370

Stiffness to Weight: Axial, points		14
Stiffness to Weight: Axial, points		11

Stiffness to Weight: Bending, points		25
Stiffness to Weight: Bending, points		21

Strength to Weight: Axial, points		30
Strength to Weight: Axial, points		13 to 17

Strength to Weight: Bending, points		25
Strength to Weight: Bending, points		14 to 17

Thermal Shock Resistance, points		21
Thermal Shock Resistance, points		13 to 16

Alloy Composition

Carbon (C), %		0 to 0.015
Carbon (C), %		0 to 0.15

Chromium (Cr), %		31 to 35
Chromium (Cr), %		0

Copper (Cu), %		0.3 to 1.2
Copper (Cu), %		0 to 0.25

Iron (Fe), %		25.7 to 37.9
Iron (Fe), %		0 to 0.4

Manganese (Mn), %		0 to 2.0
Manganese (Mn), %		0 to 0.35

Molybdenum (Mo), %		0.5 to 2.0
Molybdenum (Mo), %		0

Nickel (Ni), %		30 to 33
Nickel (Ni), %		99 to 100

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

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

Silicon (Si), %		0 to 0.5
Silicon (Si), %		0 to 0.35

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