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AZ63A Magnesium vs. C42600 Brass

AZ63A magnesium belongs to the magnesium alloys classification, while C42600 brass belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (2, 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 AZ63A magnesium and the bottom bar is C42600 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
110
Elongation at Break, % 2.2 to 8.0
1.1 to 40
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 18
42
Shear Strength, MPa 110 to 160
280 to 470
Tensile Strength: Ultimate (UTS), MPa 190 to 270
410 to 830
Tensile Strength: Yield (Proof), MPa 81 to 120
220 to 810

Thermal Properties

Latent Heat of Fusion, J/g 350
200
Maximum Temperature: Mechanical, °C 120
180
Melting Completion (Liquidus), °C 610
1030
Melting Onset (Solidus), °C 450
1010
Specific Heat Capacity, J/kg-K 980
380
Thermal Conductivity, W/m-K 52 to 65
110
Thermal Expansion, µm/m-K 26
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12 to 15
25
Electrical Conductivity: Equal Weight (Specific), % IACS 59 to 74
26

Otherwise Unclassified Properties

Base Metal Price, % relative 12
31
Density, g/cm3 1.8
8.7
Embodied Carbon, kg CO2/kg material 22
2.9
Embodied Energy, MJ/kg 150
48
Embodied Water, L/kg 970
340

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.7 to 16
9.4 to 140
Resilience: Unit (Modulus of Resilience), kJ/m3 71 to 160
230 to 2970
Stiffness to Weight: Axial, points 14
7.1
Stiffness to Weight: Bending, points 66
18
Strength to Weight: Axial, points 29 to 41
13 to 27
Strength to Weight: Bending, points 40 to 51
14 to 23
Thermal Diffusivity, mm2/s 29 to 37
33
Thermal Shock Resistance, points 11 to 16
15 to 29

Alloy Composition

Aluminum (Al), % 5.3 to 6.7
0
Copper (Cu), % 0 to 0.25
87 to 90
Iron (Fe), % 0
0.050 to 0.2
Lead (Pb), % 0
0 to 0.050
Magnesium (Mg), % 88.6 to 92.1
0
Manganese (Mn), % 0.15 to 0.35
0
Nickel (Ni), % 0 to 0.010
0.050 to 0.2
Phosphorus (P), % 0
0.020 to 0.050
Silicon (Si), % 0 to 0.3
0
Tin (Sn), % 0
2.5 to 4.0
Zinc (Zn), % 2.5 to 3.5
5.3 to 10.4
Residuals, % 0
0 to 0.2