50Cr-50Ni Alloy vs. C95400 Bronze

50Cr-50Ni alloy belongs to the otherwise unclassified metals classification, while C95400 bronze belongs to the copper alloys. There are 21 material properties with values for both materials. Properties with values for just one material (8, in this case) are not shown.

For each property being compared, the top bar is 50Cr-50Ni alloy and the bottom bar is C95400 bronze.

50Cr-50Ni (R20500) Casting Alloy UNS C95400 Aluminum Bronze

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa		210
Elastic (Young's, Tensile) Modulus, GPa		110

Elongation at Break, %		5.7
Elongation at Break, %		8.1 to 16

Poisson's Ratio		0.26
Poisson's Ratio		0.34

Shear Modulus, GPa		84
Shear Modulus, GPa		43

Tensile Strength: Ultimate (UTS), MPa		620
Tensile Strength: Ultimate (UTS), MPa		600 to 710

Tensile Strength: Yield (Proof), MPa		390
Tensile Strength: Yield (Proof), MPa		240 to 360

Thermal Properties

Latent Heat of Fusion, J/g		350
Latent Heat of Fusion, J/g		230

Specific Heat Capacity, J/kg-K		490
Specific Heat Capacity, J/kg-K		440

Thermal Expansion, µm/m-K		15
Thermal Expansion, µm/m-K		18

Otherwise Unclassified Properties

Base Metal Price, % relative		50
Base Metal Price, % relative		27

Density, g/cm³		8.0
Density, g/cm³		8.2

Embodied Carbon, kg CO₂/kg material		7.9
Embodied Carbon, kg CO₂/kg material		3.2

Embodied Energy, MJ/kg		110
Embodied Energy, MJ/kg		53

Embodied Water, L/kg		350
Embodied Water, L/kg		390

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m³		31
Resilience: Ultimate (Unit Rupture Work), MJ/m³		48 to 75

Resilience: Unit (Modulus of Resilience), kJ/m³		350
Resilience: Unit (Modulus of Resilience), kJ/m³		250 to 560

Stiffness to Weight: Axial, points		15
Stiffness to Weight: Axial, points		7.7

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

Strength to Weight: Axial, points		21
Strength to Weight: Axial, points		20 to 24

Strength to Weight: Bending, points		20
Strength to Weight: Bending, points		19 to 22

Thermal Shock Resistance, points		14
Thermal Shock Resistance, points		21 to 25

Alloy Composition

Aluminum (Al), %		0 to 0.25
Aluminum (Al), %		10 to 11.5

Carbon (C), %		0 to 0.1
Carbon (C), %		0

Chromium (Cr), %		48 to 52
Chromium (Cr), %		0

Copper (Cu), %		0
Copper (Cu), %		83 to 87

Iron (Fe), %		0 to 1.0
Iron (Fe), %		3.0 to 5.0

Manganese (Mn), %		0 to 0.3
Manganese (Mn), %		0 to 0.5

Nickel (Ni), %		44.5 to 52
Nickel (Ni), %		0 to 1.5

Nitrogen (N), %		0 to 0.3
Nitrogen (N), %		0

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

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

Sulfur (S), %		0 to 0.020
Sulfur (S), %		0

Titanium (Ti), %		0 to 0.5
Titanium (Ti), %		0

Residuals, %		0
Residuals, %		0 to 0.5