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5110A Aluminum vs. R58150 Titanium

5110A 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 (5, in this case) are not shown.

For each property being compared, the top bar is 5110A aluminum and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
140
Elongation at Break, % 4.5 to 28
13
Fatigue Strength, MPa 37 to 77
330
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 26
52
Shear Strength, MPa 66 to 110
470
Tensile Strength: Ultimate (UTS), MPa 100 to 190
770
Tensile Strength: Yield (Proof), MPa 32 to 170
550

Thermal Properties

Latent Heat of Fusion, J/g 400
410
Maximum Temperature: Mechanical, °C 180
320
Melting Completion (Liquidus), °C 640
1760
Melting Onset (Solidus), °C 640
1700
Specific Heat Capacity, J/kg-K 900
500
Thermal Expansion, µm/m-K 23
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
48
Density, g/cm3 2.7
5.4
Embodied Carbon, kg CO2/kg material 8.3
31
Embodied Energy, MJ/kg 150
480
Embodied Water, L/kg 1190
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.8 to 22
94
Resilience: Unit (Modulus of Resilience), kJ/m3 7.6 to 200
1110
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
32
Strength to Weight: Axial, points 10 to 19
40
Strength to Weight: Bending, points 18 to 27
35
Thermal Shock Resistance, points 4.5 to 8.4
48

Alloy Composition

Aluminum (Al), % 98.5 to 99.8
0
Carbon (C), % 0
0 to 0.1
Copper (Cu), % 0 to 0.2
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.25
0 to 0.1
Magnesium (Mg), % 0.2 to 0.6
0
Manganese (Mn), % 0 to 0.2
0
Molybdenum (Mo), % 0
14 to 16
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Silicon (Si), % 0 to 0.15
0
Titanium (Ti), % 0
83.5 to 86
Zinc (Zn), % 0 to 0.030
0
Residuals, % 0 to 0.1
0