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ISO-WD21150 Magnesium vs. Grade 32 Titanium

ISO-WD21150 magnesium belongs to the magnesium alloys classification, while grade 32 titanium belongs to the titanium 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 ISO-WD21150 magnesium and the bottom bar is grade 32 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
110
Elongation at Break, % 5.7 to 11
11
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 17
40
Shear Strength, MPa 150 to 170
460
Tensile Strength: Ultimate (UTS), MPa 240 to 290
770
Tensile Strength: Yield (Proof), MPa 120 to 200
670

Thermal Properties

Latent Heat of Fusion, J/g 350
410
Maximum Temperature: Mechanical, °C 110
310
Melting Completion (Liquidus), °C 600
1610
Melting Onset (Solidus), °C 550
1560
Specific Heat Capacity, J/kg-K 990
550
Thermal Conductivity, W/m-K 100
7.5
Thermal Expansion, µm/m-K 27
8.2

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 19
1.0
Electrical Conductivity: Equal Weight (Specific), % IACS 100
2.1

Otherwise Unclassified Properties

Base Metal Price, % relative 12
38
Density, g/cm3 1.7
4.5
Embodied Carbon, kg CO2/kg material 23
32
Embodied Energy, MJ/kg 160
530
Embodied Water, L/kg 980
180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 24
83
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 460
2100
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 70
35
Strength to Weight: Axial, points 40 to 48
47
Strength to Weight: Bending, points 52 to 58
41
Thermal Diffusivity, mm2/s 60
3.0
Thermal Shock Resistance, points 15 to 17
63

Alloy Composition

Aluminum (Al), % 2.4 to 3.6
4.5 to 5.5
Carbon (C), % 0
0 to 0.080
Copper (Cu), % 0 to 0.050
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.0050
0 to 0.25
Magnesium (Mg), % 94 to 97
0
Manganese (Mn), % 0.15 to 0.4
0
Molybdenum (Mo), % 0
0.6 to 1.2
Nickel (Ni), % 0 to 0.0050
0
Nitrogen (N), % 0
0 to 0.030
Oxygen (O), % 0
0 to 0.11
Silicon (Si), % 0 to 0.1
0.060 to 0.14
Tin (Sn), % 0
0.6 to 1.4
Titanium (Ti), % 0
88.1 to 93
Vanadium (V), % 0
0.6 to 1.4
Zinc (Zn), % 0.5 to 1.5
0
Zirconium (Zr), % 0
0.6 to 1.4
Residuals, % 0
0 to 0.4