MakeItFrom.com
Menu (ESC)

ISO-WD32350 Magnesium vs. C49300 Brass

ISO-WD32350 magnesium belongs to the magnesium alloys classification, while C49300 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-WD32350 magnesium and the bottom bar is C49300 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
100
Elongation at Break, % 5.7 to 10
4.5 to 20
Poisson's Ratio 0.29
0.31
Shear Modulus, GPa 18
40
Shear Strength, MPa 150 to 170
270 to 290
Tensile Strength: Ultimate (UTS), MPa 250 to 290
430 to 520
Tensile Strength: Yield (Proof), MPa 140 to 180
210 to 410

Thermal Properties

Latent Heat of Fusion, J/g 340
170
Maximum Temperature: Mechanical, °C 95
120
Melting Completion (Liquidus), °C 600
880
Melting Onset (Solidus), °C 560
840
Specific Heat Capacity, J/kg-K 990
380
Thermal Conductivity, W/m-K 130
88
Thermal Expansion, µm/m-K 25
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
15
Electrical Conductivity: Equal Weight (Specific), % IACS 130
17

Otherwise Unclassified Properties

Base Metal Price, % relative 12
26
Density, g/cm3 1.7
8.0
Embodied Carbon, kg CO2/kg material 23
3.0
Embodied Energy, MJ/kg 160
50
Embodied Water, L/kg 960
370

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 23
21 to 71
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 380
220 to 800
Stiffness to Weight: Axial, points 15
7.2
Stiffness to Weight: Bending, points 68
19
Strength to Weight: Axial, points 39 to 46
15 to 18
Strength to Weight: Bending, points 50 to 55
16 to 18
Thermal Diffusivity, mm2/s 73
29
Thermal Shock Resistance, points 16 to 18
14 to 18

Alloy Composition

Aluminum (Al), % 0 to 0.1
0 to 0.5
Antimony (Sb), % 0
0 to 0.5
Bismuth (Bi), % 0
0.5 to 2.0
Copper (Cu), % 0 to 0.1
58 to 62
Iron (Fe), % 0 to 0.060
0 to 0.1
Lead (Pb), % 0
0 to 0.010
Magnesium (Mg), % 95.7 to 97.7
0
Manganese (Mn), % 0.6 to 1.3
0 to 0.030
Nickel (Ni), % 0 to 0.0050
0 to 1.5
Phosphorus (P), % 0
0 to 0.2
Selenium (Se), % 0
0 to 0.2
Silicon (Si), % 0 to 0.1
0 to 0.1
Tin (Sn), % 0
1.0 to 1.8
Zinc (Zn), % 1.8 to 2.3
30.6 to 40.5
Residuals, % 0
0 to 0.5