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R58150 Titanium vs. 6013 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 6013 aluminum belongs to the aluminum 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 R58150 titanium and the bottom bar is 6013 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
69
Elongation at Break, % 13
3.4 to 22
Fatigue Strength, MPa 330
98 to 140
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
26
Shear Strength, MPa 470
190 to 240
Tensile Strength: Ultimate (UTS), MPa 770
310 to 410
Tensile Strength: Yield (Proof), MPa 550
170 to 350

Thermal Properties

Latent Heat of Fusion, J/g 410
410
Maximum Temperature: Mechanical, °C 320
160
Melting Completion (Liquidus), °C 1760
650
Melting Onset (Solidus), °C 1700
580
Specific Heat Capacity, J/kg-K 500
900
Thermal Expansion, µm/m-K 8.4
23

Otherwise Unclassified Properties

Base Metal Price, % relative 48
9.5
Density, g/cm3 5.4
2.8
Embodied Carbon, kg CO2/kg material 31
8.3
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
13 to 58
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
200 to 900
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 32
49
Strength to Weight: Axial, points 40
31 to 41
Strength to Weight: Bending, points 35
37 to 44
Thermal Shock Resistance, points 48
14 to 18

Alloy Composition

Aluminum (Al), % 0
94.8 to 97.8
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 0
0.6 to 1.1
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.5
Magnesium (Mg), % 0
0.8 to 1.2
Manganese (Mn), % 0
0.2 to 0.8
Molybdenum (Mo), % 14 to 16
0
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
0.6 to 1.0
Titanium (Ti), % 83.5 to 86
0 to 0.1
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15