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R58150 Titanium vs. 2218 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 2218 aluminum belongs to the aluminum alloys. There are 26 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is 2218 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
73
Elongation at Break, % 13
6.8 to 10
Fatigue Strength, MPa 330
110
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
27
Shear Strength, MPa 470
210 to 250
Tensile Strength: Ultimate (UTS), MPa 770
330 to 430
Tensile Strength: Yield (Proof), MPa 550
260 to 310

Thermal Properties

Latent Heat of Fusion, J/g 410
390
Maximum Temperature: Mechanical, °C 320
220
Melting Completion (Liquidus), °C 1760
640
Melting Onset (Solidus), °C 1700
510
Specific Heat Capacity, J/kg-K 500
870
Thermal Expansion, µm/m-K 8.4
22

Otherwise Unclassified Properties

Base Metal Price, % relative 48
11
Density, g/cm3 5.4
3.1
Embodied Carbon, kg CO2/kg material 31
8.2
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
27 to 31
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
450 to 650
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 32
45
Strength to Weight: Axial, points 40
30 to 39
Strength to Weight: Bending, points 35
34 to 41
Thermal Shock Resistance, points 48
15 to 19

Alloy Composition

Aluminum (Al), % 0
88.8 to 93.6
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 0
3.5 to 4.5
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 1.0
Magnesium (Mg), % 0
1.2 to 1.8
Manganese (Mn), % 0
0 to 0.2
Molybdenum (Mo), % 14 to 16
0
Nickel (Ni), % 0
1.7 to 2.3
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
0 to 0.9
Titanium (Ti), % 83.5 to 86
0
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15