MakeItFrom.com
Menu (ESC)

AZ63A Magnesium vs. Titanium 6-2-4-2

AZ63A magnesium belongs to the magnesium alloys classification, while titanium 6-2-4-2 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 titanium 6-2-4-2.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
110
Elongation at Break, % 2.2 to 8.0
8.6
Fatigue Strength, MPa 76 to 83
490
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 18
40
Shear Strength, MPa 110 to 160
560
Tensile Strength: Ultimate (UTS), MPa 190 to 270
950
Tensile Strength: Yield (Proof), MPa 81 to 120
880

Thermal Properties

Latent Heat of Fusion, J/g 350
400
Maximum Temperature: Mechanical, °C 120
300
Melting Completion (Liquidus), °C 610
1590
Melting Onset (Solidus), °C 450
1540
Specific Heat Capacity, J/kg-K 980
540
Thermal Conductivity, W/m-K 52 to 65
6.9
Thermal Expansion, µm/m-K 26
9.5

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12 to 15
0.9
Electrical Conductivity: Equal Weight (Specific), % IACS 59 to 74
1.8

Otherwise Unclassified Properties

Base Metal Price, % relative 12
42
Density, g/cm3 1.8
4.6
Embodied Carbon, kg CO2/kg material 22
32
Embodied Energy, MJ/kg 150
520
Embodied Water, L/kg 970
210

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.7 to 16
79
Resilience: Unit (Modulus of Resilience), kJ/m3 71 to 160
3640
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 66
34
Strength to Weight: Axial, points 29 to 41
57
Strength to Weight: Bending, points 40 to 51
46
Thermal Diffusivity, mm2/s 29 to 37
2.8
Thermal Shock Resistance, points 11 to 16
67

Alloy Composition

Aluminum (Al), % 5.3 to 6.7
5.5 to 6.5
Carbon (C), % 0
0 to 0.050
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
Molybdenum (Mo), % 0
1.8 to 2.2
Nickel (Ni), % 0 to 0.010
0
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.15
Silicon (Si), % 0 to 0.3
0.060 to 0.12
Tin (Sn), % 0
1.8 to 2.2
Titanium (Ti), % 0
83.7 to 87.2
Zinc (Zn), % 2.5 to 3.5
0
Zirconium (Zr), % 0
3.6 to 4.4
Residuals, % 0
0 to 0.4