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AZ92A Magnesium vs. Grade 29 Titanium

AZ92A magnesium belongs to the magnesium alloys classification, while grade 29 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 AZ92A magnesium and the bottom bar is grade 29 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 47
110
Elongation at Break, % 2.1 to 6.8
6.8 to 11
Fatigue Strength, MPa 76 to 90
460 to 510
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 18
40
Shear Strength, MPa 97 to 160
550 to 560
Tensile Strength: Ultimate (UTS), MPa 170 to 270
930 to 940
Tensile Strength: Yield (Proof), MPa 83 to 140
850 to 870

Thermal Properties

Latent Heat of Fusion, J/g 350
410
Maximum Temperature: Mechanical, °C 130
340
Melting Completion (Liquidus), °C 590
1610
Melting Onset (Solidus), °C 440
1560
Specific Heat Capacity, J/kg-K 980
560
Thermal Conductivity, W/m-K 44 to 58
7.3
Thermal Expansion, µm/m-K 26
9.3

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11 to 12
1.0
Electrical Conductivity: Equal Weight (Specific), % IACS 53 to 62
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 12
36
Density, g/cm3 1.8
4.5
Embodied Carbon, kg CO2/kg material 22
39
Embodied Energy, MJ/kg 160
640
Embodied Water, L/kg 980
410

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.0 to 14
62 to 100
Resilience: Unit (Modulus of Resilience), kJ/m3 73 to 220
3420 to 3540
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 67
35
Strength to Weight: Axial, points 26 to 41
58 to 59
Strength to Weight: Bending, points 38 to 51
47 to 48
Thermal Diffusivity, mm2/s 25 to 33
2.9
Thermal Shock Resistance, points 10 to 16
68 to 69

Alloy Composition

Aluminum (Al), % 8.3 to 9.7
5.5 to 6.5
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), % 86.7 to 90
0
Manganese (Mn), % 0.1 to 0.35
0
Nickel (Ni), % 0 to 0.010
0
Nitrogen (N), % 0
0 to 0.030
Oxygen (O), % 0
0 to 0.13
Ruthenium (Ru), % 0
0.080 to 0.14
Silicon (Si), % 0 to 0.3
0
Titanium (Ti), % 0
88 to 90.9
Vanadium (V), % 0
3.5 to 4.5
Zinc (Zn), % 1.6 to 2.4
0
Residuals, % 0
0 to 0.4