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ISO-WD32350 Magnesium vs. Grade 29 Titanium

ISO-WD32350 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 (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 ISO-WD32350 magnesium and the bottom bar is grade 29 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
110
Elongation at Break, % 5.7 to 10
6.8 to 11
Fatigue Strength, MPa 120 to 130
460 to 510
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 18
40
Shear Strength, MPa 150 to 170
550 to 560
Tensile Strength: Ultimate (UTS), MPa 250 to 290
930 to 940
Tensile Strength: Yield (Proof), MPa 140 to 180
850 to 870

Thermal Properties

Latent Heat of Fusion, J/g 340
410
Maximum Temperature: Mechanical, °C 95
340
Melting Completion (Liquidus), °C 600
1610
Melting Onset (Solidus), °C 560
1560
Specific Heat Capacity, J/kg-K 990
560
Thermal Conductivity, W/m-K 130
7.3
Thermal Expansion, µm/m-K 25
9.3

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
1.0
Electrical Conductivity: Equal Weight (Specific), % IACS 130
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 12
36
Density, g/cm3 1.7
4.5
Embodied Carbon, kg CO2/kg material 23
39
Embodied Energy, MJ/kg 160
640
Embodied Water, L/kg 960
410

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 23
62 to 100
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 380
3420 to 3540
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 68
35
Strength to Weight: Axial, points 39 to 46
58 to 59
Strength to Weight: Bending, points 50 to 55
47 to 48
Thermal Diffusivity, mm2/s 73
2.9
Thermal Shock Resistance, points 16 to 18
68 to 69

Alloy Composition

Aluminum (Al), % 0 to 0.1
5.5 to 6.5
Carbon (C), % 0
0 to 0.080
Copper (Cu), % 0 to 0.1
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.060
0 to 0.25
Magnesium (Mg), % 95.7 to 97.7
0
Manganese (Mn), % 0.6 to 1.3
0
Nickel (Ni), % 0 to 0.0050
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 0.1
0
Titanium (Ti), % 0
88 to 90.9
Vanadium (V), % 0
3.5 to 4.5
Zinc (Zn), % 1.8 to 2.3
0
Residuals, % 0
0 to 0.4

Comparable Variants