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6023 Aluminum vs. R58150 Titanium

6023 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 6023 aluminum and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
140
Elongation at Break, % 11
13
Fatigue Strength, MPa 120 to 130
330
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 26
52
Shear Strength, MPa 210 to 220
470
Tensile Strength: Ultimate (UTS), MPa 360
770
Tensile Strength: Yield (Proof), MPa 300 to 310
550

Thermal Properties

Latent Heat of Fusion, J/g 400
410
Maximum Temperature: Mechanical, °C 160
320
Melting Completion (Liquidus), °C 640
1760
Melting Onset (Solidus), °C 580
1700
Specific Heat Capacity, J/kg-K 890
500
Thermal Expansion, µm/m-K 23
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 11
48
Density, g/cm3 2.8
5.4
Embodied Carbon, kg CO2/kg material 8.3
31
Embodied Energy, MJ/kg 150
480
Embodied Water, L/kg 1180
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 38 to 39
94
Resilience: Unit (Modulus of Resilience), kJ/m3 670 to 690
1110
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 49
32
Strength to Weight: Axial, points 35 to 36
40
Strength to Weight: Bending, points 40
35
Thermal Shock Resistance, points 16
48

Alloy Composition


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Aluminum (Al), % 94 to 97.7
0
Bismuth (Bi), % 0.3 to 0.8
0
Carbon (C), % 0
0 to 0.1
Copper (Cu), % 0.2 to 0.5
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.5
0 to 0.1
Magnesium (Mg), % 0.4 to 0.9
0
Manganese (Mn), % 0.2 to 0.6
0
Molybdenum (Mo), % 0
14 to 16
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Silicon (Si), % 0.6 to 1.4
0
Tin (Sn), % 0.6 to 1.2
0
Titanium (Ti), % 0
83.5 to 86
Residuals, % 0 to 0.15
0