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Grade 29 Titanium vs. ISO-WD32350 Magnesium

Grade 29 titanium belongs to the titanium alloys classification, while ISO-WD32350 magnesium belongs to the magnesium 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 grade 29 titanium and the bottom bar is ISO-WD32350 magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

Aluminum (Al), % 5.5 to 6.5
0 to 0.1
Carbon (C), % 0 to 0.080
0
Copper (Cu), % 0
0 to 0.1
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.25
0 to 0.060
Magnesium (Mg), % 0
95.7 to 97.7
Manganese (Mn), % 0
0.6 to 1.3
Nickel (Ni), % 0
0 to 0.0050
Nitrogen (N), % 0 to 0.030
0
Oxygen (O), % 0 to 0.13
0
Ruthenium (Ru), % 0.080 to 0.14
0
Silicon (Si), % 0
0 to 0.1
Titanium (Ti), % 88 to 90.9
0
Vanadium (V), % 3.5 to 4.5
0
Zinc (Zn), % 0
1.8 to 2.3
Residuals, % 0
0 to 0.3

Comparable Variants