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5086 Aluminum vs. R58150 Titanium

5086 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 (8, in this case) are not shown.

For each property being compared, the top bar is 5086 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, % 1.7 to 20
13
Fatigue Strength, MPa 88 to 180
330
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 26
52
Shear Strength, MPa 160 to 230
470
Tensile Strength: Ultimate (UTS), MPa 270 to 390
770
Tensile Strength: Yield (Proof), MPa 110 to 320
550

Thermal Properties

Latent Heat of Fusion, J/g 400
410
Maximum Temperature: Mechanical, °C 190
320
Melting Completion (Liquidus), °C 640
1760
Melting Onset (Solidus), °C 590
1700
Specific Heat Capacity, J/kg-K 900
500
Thermal Expansion, µm/m-K 24
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 8.8
31
Embodied Energy, MJ/kg 150
480
Embodied Water, L/kg 1180
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.8 to 42
94
Resilience: Unit (Modulus of Resilience), kJ/m3 86 to 770
1110
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
32
Strength to Weight: Axial, points 28 to 40
40
Strength to Weight: Bending, points 34 to 44
35
Thermal Shock Resistance, points 12 to 17
48

Alloy Composition


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Aluminum (Al), % 93 to 96.3
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0.050 to 0.25
0
Copper (Cu), % 0 to 0.1
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.5
0 to 0.1
Magnesium (Mg), % 3.5 to 4.5
0
Manganese (Mn), % 0.2 to 0.7
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 0.4
0
Titanium (Ti), % 0 to 0.15
83.5 to 86
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0