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ZK61A Magnesium vs. Grade 6 Titanium

ZK61A magnesium belongs to the magnesium alloys classification, while grade 6 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 ZK61A magnesium and the bottom bar is grade 6 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
100
Elongation at Break, % 5.8 to 7.1
11
Fatigue Strength, MPa 120 to 140
290
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 18
39
Shear Strength, MPa 170 to 180
530
Tensile Strength: Ultimate (UTS), MPa 290 to 310
890
Tensile Strength: Yield (Proof), MPa 180 to 200
840

Thermal Properties

Latent Heat of Fusion, J/g 330
410
Maximum Temperature: Mechanical, °C 120
310
Melting Completion (Liquidus), °C 640
1580
Melting Onset (Solidus), °C 530
1530
Specific Heat Capacity, J/kg-K 960
550
Thermal Conductivity, W/m-K 120
7.8
Thermal Expansion, µm/m-K 27
9.4

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
1.2
Electrical Conductivity: Equal Weight (Specific), % IACS 130
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 13
36
Density, g/cm3 1.9
4.5
Embodied Carbon, kg CO2/kg material 23
30
Embodied Energy, MJ/kg 160
480
Embodied Water, L/kg 940
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 19
92
Resilience: Unit (Modulus of Resilience), kJ/m3 370 to 420
3390
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 62
35
Strength to Weight: Axial, points 42 to 45
55
Strength to Weight: Bending, points 50 to 53
46
Thermal Diffusivity, mm2/s 65
3.2
Thermal Shock Resistance, points 17 to 18
65

Alloy Composition


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Aluminum (Al), % 0
4.0 to 6.0
Carbon (C), % 0
0 to 0.080
Copper (Cu), % 0 to 0.1
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0
0 to 0.5
Magnesium (Mg), % 92.1 to 93.9
0
Nickel (Ni), % 0 to 0.010
0
Nitrogen (N), % 0
0 to 0.030
Oxygen (O), % 0
0 to 0.2
Tin (Sn), % 0
2.0 to 3.0
Titanium (Ti), % 0
89.8 to 94
Zinc (Zn), % 5.5 to 6.5
0
Zirconium (Zr), % 0.6 to 1.0
0
Residuals, % 0 to 0.3
0 to 0.4