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AZ63A Magnesium vs. Grade 28 Titanium

AZ63A magnesium belongs to the magnesium alloys classification, while grade 28 titanium belongs to the titanium alloys. There are 30 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 grade 28 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
110
Elongation at Break, % 2.2 to 8.0
11 to 17
Fatigue Strength, MPa 76 to 83
330 to 480
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 18
40
Shear Strength, MPa 110 to 160
420 to 590
Tensile Strength: Ultimate (UTS), MPa 190 to 270
690 to 980
Tensile Strength: Yield (Proof), MPa 81 to 120
540 to 810

Thermal Properties

Latent Heat of Fusion, J/g 350
410
Maximum Temperature: Mechanical, °C 120
330
Melting Completion (Liquidus), °C 610
1640
Melting Onset (Solidus), °C 450
1590
Specific Heat Capacity, J/kg-K 980
550
Thermal Conductivity, W/m-K 52 to 65
8.3
Thermal Expansion, µm/m-K 26
9.9

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12 to 15
1.3
Electrical Conductivity: Equal Weight (Specific), % IACS 59 to 74
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 12
36
Density, g/cm3 1.8
4.5
Embodied Carbon, kg CO2/kg material 22
37
Embodied Energy, MJ/kg 150
600
Embodied Water, L/kg 970
370

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.7 to 16
87 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 71 to 160
1370 to 3100
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 66
35
Strength to Weight: Axial, points 29 to 41
43 to 61
Strength to Weight: Bending, points 40 to 51
39 to 49
Thermal Diffusivity, mm2/s 29 to 37
3.4
Thermal Shock Resistance, points 11 to 16
47 to 66

Alloy Composition

Aluminum (Al), % 5.3 to 6.7
2.5 to 3.5
Carbon (C), % 0
0 to 0.080
Copper (Cu), % 0 to 0.25
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0
0 to 0.25
Magnesium (Mg), % 88.6 to 92.1
0
Manganese (Mn), % 0.15 to 0.35
0
Nickel (Ni), % 0 to 0.010
0
Nitrogen (N), % 0
0 to 0.030
Oxygen (O), % 0
0 to 0.15
Ruthenium (Ru), % 0
0.080 to 0.14
Silicon (Si), % 0 to 0.3
0
Titanium (Ti), % 0
92.4 to 95.4
Vanadium (V), % 0
2.0 to 3.0
Zinc (Zn), % 2.5 to 3.5
0
Residuals, % 0
0 to 0.4