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WE54A Magnesium vs. Grade 29 Titanium

WE54A magnesium belongs to the magnesium alloys classification, while grade 29 titanium belongs to the titanium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 WE54A magnesium and the bottom bar is grade 29 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 44
110
Elongation at Break, % 4.3 to 5.6
6.8 to 11
Fatigue Strength, MPa 98 to 130
460 to 510
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 17
40
Shear Strength, MPa 150 to 170
550 to 560
Tensile Strength: Ultimate (UTS), MPa 270 to 300
930 to 940
Tensile Strength: Yield (Proof), MPa 180
850 to 870

Thermal Properties

Latent Heat of Fusion, J/g 330
410
Maximum Temperature: Mechanical, °C 170
340
Melting Completion (Liquidus), °C 640
1610
Melting Onset (Solidus), °C 570
1560
Specific Heat Capacity, J/kg-K 960
560
Thermal Conductivity, W/m-K 52
7.3
Thermal Expansion, µm/m-K 25
9.3

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
1.0
Electrical Conductivity: Equal Weight (Specific), % IACS 47
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 34
36
Density, g/cm3 1.9
4.5
Embodied Carbon, kg CO2/kg material 29
39
Embodied Energy, MJ/kg 260
640
Embodied Water, L/kg 900
410

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 14
62 to 100
Resilience: Unit (Modulus of Resilience), kJ/m3 360 to 380
3420 to 3540
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 62
35
Strength to Weight: Axial, points 39 to 43
58 to 59
Strength to Weight: Bending, points 49 to 51
47 to 48
Thermal Diffusivity, mm2/s 28
2.9
Thermal Shock Resistance, points 18 to 19
68 to 69

Alloy Composition

Aluminum (Al), % 0
5.5 to 6.5
Carbon (C), % 0
0 to 0.080
Copper (Cu), % 0 to 0.030
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.010
0 to 0.25
Lithium (Li), % 0 to 0.2
0
Magnesium (Mg), % 88.7 to 93.4
0
Manganese (Mn), % 0 to 0.030
0
Nickel (Ni), % 0 to 0.0050
0
Nitrogen (N), % 0
0 to 0.030
Oxygen (O), % 0
0 to 0.13
Ruthenium (Ru), % 0
0.080 to 0.14
Silicon (Si), % 0 to 0.010
0
Titanium (Ti), % 0
88 to 90.9
Unspecified Rare Earths, % 1.5 to 4.0
0
Vanadium (V), % 0
3.5 to 4.5
Yttrium (Y), % 4.8 to 5.5
0
Zinc (Zn), % 0 to 0.2
0
Zirconium (Zr), % 0.4 to 1.0
0
Residuals, % 0
0 to 0.4