C95400 Bronze vs. 50Cr-50Ni Alloy

C95400 bronze belongs to the copper alloys classification, while 50Cr-50Ni alloy belongs to the otherwise unclassified metals. 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 C95400 bronze and the bottom bar is 50Cr-50Ni alloy.

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

Metric UnitsUS Customary Units

Mechanical Properties

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

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

Poisson's Ratio		0.34
Poisson's Ratio		0.26

Shear Modulus, GPa		43
Shear Modulus, GPa		84

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

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

Thermal Properties

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

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

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

Otherwise Unclassified Properties

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

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

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

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

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

Common Calculations

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

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

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

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

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

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

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

Alloy Composition

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

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

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

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

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

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

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

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

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

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

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

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

Residuals, %		0 to 0.5
Residuals, %		0