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ISO-WD21150 Magnesium vs. C69300 Brass

ISO-WD21150 magnesium belongs to the magnesium alloys classification, while C69300 brass belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (1, 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 ISO-WD21150 magnesium and the bottom bar is C69300 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
110
Elongation at Break, % 5.7 to 11
8.5 to 15
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 17
41
Shear Strength, MPa 150 to 170
330 to 370
Tensile Strength: Ultimate (UTS), MPa 240 to 290
550 to 630
Tensile Strength: Yield (Proof), MPa 120 to 200
300 to 390

Thermal Properties

Latent Heat of Fusion, J/g 350
240
Maximum Temperature: Mechanical, °C 110
160
Melting Completion (Liquidus), °C 600
880
Melting Onset (Solidus), °C 550
860
Specific Heat Capacity, J/kg-K 990
400
Thermal Conductivity, W/m-K 100
38
Thermal Expansion, µm/m-K 27
19

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 19
8.0
Electrical Conductivity: Equal Weight (Specific), % IACS 100
8.8

Otherwise Unclassified Properties

Base Metal Price, % relative 12
26
Density, g/cm3 1.7
8.2
Embodied Carbon, kg CO2/kg material 23
2.7
Embodied Energy, MJ/kg 160
45
Embodied Water, L/kg 980
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 24
47 to 70
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 460
400 to 700
Stiffness to Weight: Axial, points 15
7.4
Stiffness to Weight: Bending, points 70
19
Strength to Weight: Axial, points 40 to 48
19 to 21
Strength to Weight: Bending, points 52 to 58
18 to 20
Thermal Diffusivity, mm2/s 60
12
Thermal Shock Resistance, points 15 to 17
19 to 22

Alloy Composition

Aluminum (Al), % 2.4 to 3.6
0
Copper (Cu), % 0 to 0.050
73 to 77
Iron (Fe), % 0 to 0.0050
0 to 0.1
Lead (Pb), % 0
0 to 0.090
Magnesium (Mg), % 94 to 97
0
Manganese (Mn), % 0.15 to 0.4
0 to 0.1
Nickel (Ni), % 0 to 0.0050
0 to 0.1
Phosphorus (P), % 0
0.040 to 0.15
Silicon (Si), % 0 to 0.1
2.7 to 3.4
Tin (Sn), % 0
0 to 0.2
Zinc (Zn), % 0.5 to 1.5
18.4 to 24.3
Residuals, % 0
0 to 0.5