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AZ91E Magnesium vs. C72800 Copper-nickel

AZ91E magnesium belongs to the magnesium alloys classification, while C72800 copper-nickel belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is AZ91E magnesium and the bottom bar is C72800 copper-nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
120
Elongation at Break, % 2.5 to 6.2
3.9 to 23
Poisson's Ratio 0.29
0.34
Shear Modulus, GPa 18
44
Shear Strength, MPa 89 to 150
330 to 740
Tensile Strength: Ultimate (UTS), MPa 160 to 260
520 to 1270
Tensile Strength: Yield (Proof), MPa 96 to 130
250 to 1210

Thermal Properties

Latent Heat of Fusion, J/g 350
210
Maximum Temperature: Mechanical, °C 130
200
Melting Completion (Liquidus), °C 600
1080
Melting Onset (Solidus), °C 500
920
Specific Heat Capacity, J/kg-K 990
380
Thermal Conductivity, W/m-K 84
55
Thermal Expansion, µm/m-K 27
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10 to 12
11
Electrical Conductivity: Equal Weight (Specific), % IACS 52 to 60
11

Otherwise Unclassified Properties

Base Metal Price, % relative 12
38
Density, g/cm3 1.7
8.8
Embodied Carbon, kg CO2/kg material 22
4.4
Embodied Energy, MJ/kg 160
68
Embodied Water, L/kg 990
360

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.4 to 12
37 to 99
Resilience: Unit (Modulus of Resilience), kJ/m3 100 to 190
260 to 5650
Stiffness to Weight: Axial, points 15
7.4
Stiffness to Weight: Bending, points 69
19
Strength to Weight: Axial, points 25 to 42
17 to 40
Strength to Weight: Bending, points 37 to 53
16 to 30
Thermal Diffusivity, mm2/s 49
17
Thermal Shock Resistance, points 9.0 to 15
19 to 45

Alloy Composition


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Aluminum (Al), % 8.1 to 9.3
0 to 0.1
Antimony (Sb), % 0
0 to 0.020
Bismuth (Bi), % 0
0 to 0.0010
Boron (B), % 0
0 to 0.0010
Copper (Cu), % 0 to 0.015
78.3 to 82.8
Iron (Fe), % 0 to 0.0050
0 to 0.5
Lead (Pb), % 0
0 to 0.0050
Magnesium (Mg), % 88.8 to 91.3
0.0050 to 0.15
Manganese (Mn), % 0.17 to 0.35
0.050 to 0.3
Nickel (Ni), % 0 to 0.0010
9.5 to 10.5
Niobium (Nb), % 0
0.1 to 0.3
Phosphorus (P), % 0
0 to 0.0050
Silicon (Si), % 0 to 0.2
0 to 0.050
Sulfur (S), % 0
0 to 0.0025
Tin (Sn), % 0
7.5 to 8.5
Titanium (Ti), % 0
0 to 0.010
Zinc (Zn), % 0.4 to 1.0
0 to 1.0
Residuals, % 0 to 0.3
0 to 0.3