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2218 Aluminum vs. R58150 Titanium

2218 aluminum belongs to the aluminum alloys classification, while R58150 titanium belongs to the titanium 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 2218 aluminum and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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