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AZ80A Magnesium vs. Grade 32 Titanium

AZ80A magnesium belongs to the magnesium alloys classification, while grade 32 titanium belongs to the titanium alloys. There are 30 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 AZ80A magnesium and the bottom bar is grade 32 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
110
Elongation at Break, % 3.9 to 8.5
11
Fatigue Strength, MPa 140 to 170
390
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 18
40
Shear Strength, MPa 160 to 190
460
Tensile Strength: Ultimate (UTS), MPa 320 to 340
770
Tensile Strength: Yield (Proof), MPa 210 to 230
670

Thermal Properties

Latent Heat of Fusion, J/g 350
410
Maximum Temperature: Mechanical, °C 130
310
Melting Completion (Liquidus), °C 600
1610
Melting Onset (Solidus), °C 490
1560
Specific Heat Capacity, J/kg-K 990
550
Thermal Conductivity, W/m-K 77
7.5
Thermal Expansion, µm/m-K 26
8.2

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
1.0
Electrical Conductivity: Equal Weight (Specific), % IACS 59
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 990
180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 24
83
Resilience: Unit (Modulus of Resilience), kJ/m3 500 to 600
2100
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 69
35
Strength to Weight: Axial, points 51 to 55
47
Strength to Weight: Bending, points 60 to 63
41
Thermal Diffusivity, mm2/s 45
3.0
Thermal Shock Resistance, points 19 to 20
63

Alloy Composition

Aluminum (Al), % 7.8 to 9.2
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), % 89 to 91.9
0
Manganese (Mn), % 0.12 to 0.5
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), % 0.2 to 0.8
0
Zirconium (Zr), % 0
0.6 to 1.4
Residuals, % 0
0 to 0.4