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5457 Aluminum vs. R58150 Titanium

5457 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 5457 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, % 6.0 to 22
13
Fatigue Strength, MPa 55 to 98
330
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 26
52
Shear Strength, MPa 85 to 130
470
Tensile Strength: Ultimate (UTS), MPa 130 to 210
770
Tensile Strength: Yield (Proof), MPa 50 to 190
550

Thermal Properties

Latent Heat of Fusion, J/g 400
410
Maximum Temperature: Mechanical, °C 180
320
Melting Completion (Liquidus), °C 660
1760
Melting Onset (Solidus), °C 630
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 8.4
31
Embodied Energy, MJ/kg 160
480
Embodied Water, L/kg 1190
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 23
94
Resilience: Unit (Modulus of Resilience), kJ/m3 18 to 250
1110
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
32
Strength to Weight: Axial, points 13 to 21
40
Strength to Weight: Bending, points 21 to 28
35
Thermal Shock Resistance, points 5.7 to 9.0
48

Alloy Composition


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Aluminum (Al), % 97.8 to 99.05
0
Carbon (C), % 0
0 to 0.1
Copper (Cu), % 0 to 0.2
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.1
0 to 0.1
Magnesium (Mg), % 0.8 to 1.2
0
Manganese (Mn), % 0.15 to 0.45
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 0.080
0
Titanium (Ti), % 0
83.5 to 86
Vanadium (V), % 0 to 0.050
0
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.1
0