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Grade 28 Titanium vs. ISO-WD32350 Magnesium

Grade 28 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 28 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, % 11 to 17
5.7 to 10
Fatigue Strength, MPa 330 to 480
120 to 130
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 40
18
Shear Strength, MPa 420 to 590
150 to 170
Tensile Strength: Ultimate (UTS), MPa 690 to 980
250 to 290
Tensile Strength: Yield (Proof), MPa 540 to 810
140 to 180

Thermal Properties

Latent Heat of Fusion, J/g 410
340
Maximum Temperature: Mechanical, °C 330
95
Melting Completion (Liquidus), °C 1640
600
Melting Onset (Solidus), °C 1590
560
Specific Heat Capacity, J/kg-K 550
990
Thermal Conductivity, W/m-K 8.3
130
Thermal Expansion, µm/m-K 9.9
25

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.3
25
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
130

Otherwise Unclassified Properties

Base Metal Price, % relative 36
12
Density, g/cm3 4.5
1.7
Embodied Carbon, kg CO2/kg material 37
23
Embodied Energy, MJ/kg 600
160
Embodied Water, L/kg 370
960

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 87 to 110
14 to 23
Resilience: Unit (Modulus of Resilience), kJ/m3 1370 to 3100
210 to 380
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 35
68
Strength to Weight: Axial, points 43 to 61
39 to 46
Strength to Weight: Bending, points 39 to 49
50 to 55
Thermal Diffusivity, mm2/s 3.4
73
Thermal Shock Resistance, points 47 to 66
16 to 18

Alloy Composition

Aluminum (Al), % 2.5 to 3.5
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 0.15
0
Ruthenium (Ru), % 0.080 to 0.14
0
Silicon (Si), % 0
0 to 0.1
Titanium (Ti), % 92.4 to 95.4
0
Vanadium (V), % 2.0 to 3.0
0
Zinc (Zn), % 0
1.8 to 2.3
Residuals, % 0
0 to 0.3

Comparable Variants