Nickel 200 vs. Chromium 33

Nickel 200 belongs to the nickel alloys classification, while chromium 33 belongs to the otherwise unclassified metals. 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 nickel 200 and the bottom bar is chromium 33.

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

Metric UnitsUS Customary Units

Mechanical Properties

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

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

Poisson's Ratio		0.31
Poisson's Ratio		0.27

Shear Modulus, GPa		70
Shear Modulus, GPa		81

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

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

Thermal Properties

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

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

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

Otherwise Unclassified Properties

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

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

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

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

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

Common Calculations

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

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

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

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

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

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

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

Alloy Composition

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

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

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

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

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

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

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

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

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

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

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