Chromium 33 vs. EN 1.6958 Steel

Chromium 33 belongs to the otherwise unclassified metals classification, while EN 1.6958 steel belongs to the iron alloys. They have a modest 38% 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 (13, in this case) are not shown.

For each property being compared, the top bar is chromium 33 and the bottom bar is EN 1.6958 steel.

Chromium Alloy 33 (R20033)EN 1.6958 (26NiCrMo14-6) Nickel-Chromium Steel

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa		200
Elastic (Young's, Tensile) Modulus, GPa		190

Elongation at Break, %		45
Elongation at Break, %		16

Poisson's Ratio		0.27
Poisson's Ratio		0.29

Shear Modulus, GPa		81
Shear Modulus, GPa		73

Tensile Strength: Ultimate (UTS), MPa		850
Tensile Strength: Ultimate (UTS), MPa		1140

Tensile Strength: Yield (Proof), MPa		430
Tensile Strength: Yield (Proof), MPa		1070

Thermal Properties

Latent Heat of Fusion, J/g		320
Latent Heat of Fusion, J/g		250

Specific Heat Capacity, J/kg-K		480
Specific Heat Capacity, J/kg-K		470

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

Otherwise Unclassified Properties

Base Metal Price, % relative		36
Base Metal Price, % relative		5.0

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

Embodied Carbon, kg CO₂/kg material		6.0
Embodied Carbon, kg CO₂/kg material		2.0

Embodied Energy, MJ/kg		84
Embodied Energy, MJ/kg		27

Embodied Water, L/kg		250
Embodied Water, L/kg		60

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m³		320
Resilience: Ultimate (Unit Rupture Work), MJ/m³		180

Resilience: Unit (Modulus of Resilience), kJ/m³		450
Resilience: Unit (Modulus of Resilience), kJ/m³		3050

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

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

Strength to Weight: Axial, points		30
Strength to Weight: Axial, points		40

Strength to Weight: Bending, points		25
Strength to Weight: Bending, points		31

Thermal Shock Resistance, points		21
Thermal Shock Resistance, points		39

Alloy Composition

Aluminum (Al), %		0
Aluminum (Al), %		0.0050 to 0.050

Carbon (C), %		0 to 0.015
Carbon (C), %		0.25 to 0.3

Chromium (Cr), %		31 to 35
Chromium (Cr), %		1.2 to 1.7

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

Iron (Fe), %		25.7 to 37.9
Iron (Fe), %		92.6 to 94.5

Manganese (Mn), %		0 to 2.0
Manganese (Mn), %		0.2 to 0.5

Molybdenum (Mo), %		0.5 to 2.0
Molybdenum (Mo), %		0.35 to 0.55

Nickel (Ni), %		30 to 33
Nickel (Ni), %		3.3 to 3.8

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

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

Silicon (Si), %		0 to 0.5
Silicon (Si), %		0.15 to 0.3

Sulfur (S), %		0 to 0.010
Sulfur (S), %		0 to 0.015

Vanadium (V), %		0
Vanadium (V), %		0 to 0.12