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5154A Aluminum vs. R58150 Titanium

5154A 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 (6, in this case) are not shown.

For each property being compared, the top bar is 5154A 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, % 1.1 to 19
13
Fatigue Strength, MPa 83 to 160
330
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 26
52
Shear Strength, MPa 140 to 210
470
Tensile Strength: Ultimate (UTS), MPa 230 to 370
770
Tensile Strength: Yield (Proof), MPa 96 to 320
550

Thermal Properties

Latent Heat of Fusion, J/g 400
410
Maximum Temperature: Mechanical, °C 190
320
Melting Completion (Liquidus), °C 650
1760
Melting Onset (Solidus), °C 600
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 4.0 to 36
94
Resilience: Unit (Modulus of Resilience), kJ/m3 68 to 760
1110
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
32
Strength to Weight: Axial, points 24 to 38
40
Strength to Weight: Bending, points 31 to 43
35
Thermal Shock Resistance, points 10 to 16
48

Alloy Composition

Aluminum (Al), % 93.7 to 96.9
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0 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), % 3.1 to 3.9
0
Manganese (Mn), % 0 to 0.5
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 0.5
0
Titanium (Ti), % 0 to 0.2
83.5 to 86
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0