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5082 Aluminum vs. R58150 Titanium

5082 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 5082 aluminum and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 67
140
Elongation at Break, % 1.1
13
Fatigue Strength, MPa 110 to 130
330
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 25
52
Shear Strength, MPa 210 to 230
470
Tensile Strength: Ultimate (UTS), MPa 380 to 400
770
Tensile Strength: Yield (Proof), MPa 300 to 340
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 560
1700
Specific Heat Capacity, J/kg-K 910
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 8.9
31
Embodied Energy, MJ/kg 150
480
Embodied Water, L/kg 1180
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.0 to 4.3
94
Resilience: Unit (Modulus of Resilience), kJ/m3 670 to 870
1110
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
32
Strength to Weight: Axial, points 39 to 41
40
Strength to Weight: Bending, points 43 to 45
35
Thermal Shock Resistance, points 17 to 18
48

Alloy Composition

Aluminum (Al), % 93.5 to 96
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0 to 0.15
0
Copper (Cu), % 0 to 0.15
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.35
0 to 0.1
Magnesium (Mg), % 4.0 to 5.0
0
Manganese (Mn), % 0 to 0.15
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 0.2
0
Titanium (Ti), % 0 to 0.1
83.5 to 86
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0