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AZ31B Magnesium vs. Grade 35 Titanium

AZ31B magnesium belongs to the magnesium alloys classification, while grade 35 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 AZ31B magnesium and the bottom bar is grade 35 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
110
Elongation at Break, % 5.6 to 12
5.6
Fatigue Strength, MPa 100 to 120
330
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 17
41
Shear Strength, MPa 130 to 160
580
Tensile Strength: Ultimate (UTS), MPa 240 to 270
1000
Tensile Strength: Yield (Proof), MPa 120 to 180
630

Thermal Properties

Latent Heat of Fusion, J/g 350
420
Maximum Temperature: Mechanical, °C 150
320
Melting Completion (Liquidus), °C 600
1630
Melting Onset (Solidus), °C 600
1580
Specific Heat Capacity, J/kg-K 990
550
Thermal Conductivity, W/m-K 100
7.4
Thermal Expansion, µm/m-K 26
9.3

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 18
1.1
Electrical Conductivity: Equal Weight (Specific), % IACS 95
2.2

Otherwise Unclassified Properties

Base Metal Price, % relative 12
37
Density, g/cm3 1.7
4.6
Embodied Carbon, kg CO2/kg material 23
33
Embodied Energy, MJ/kg 160
530
Embodied Water, L/kg 970
170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 13 to 25
49
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 370
1830
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 70
35
Strength to Weight: Axial, points 39 to 44
61
Strength to Weight: Bending, points 50 to 55
49
Thermal Diffusivity, mm2/s 62
3.0
Thermal Shock Resistance, points 14 to 16
70

Alloy Composition

Aluminum (Al), % 2.4 to 3.6
4.0 to 5.0
Calcium (Ca), % 0 to 0.040
0
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 0.050
0.2 to 0.8
Magnesium (Mg), % 93.6 to 97.1
0
Manganese (Mn), % 0.050 to 1.0
0
Molybdenum (Mo), % 0
1.5 to 2.5
Nickel (Ni), % 0 to 0.0050
0
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.25
Silicon (Si), % 0 to 0.1
0.2 to 0.4
Titanium (Ti), % 0
88.4 to 93
Vanadium (V), % 0
1.1 to 2.1
Zinc (Zn), % 0.5 to 1.5
0
Residuals, % 0
0 to 0.4