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5252 Aluminum vs. R58150 Titanium

5252 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 5252 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, % 4.5 to 11
13
Fatigue Strength, MPa 100 to 110
330
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 25
52
Shear Strength, MPa 140 to 160
470
Tensile Strength: Ultimate (UTS), MPa 230 to 290
770
Tensile Strength: Yield (Proof), MPa 170 to 240
550

Thermal Properties

Latent Heat of Fusion, J/g 400
410
Maximum Temperature: Mechanical, °C 180
320
Melting Completion (Liquidus), °C 650
1760
Melting Onset (Solidus), °C 610
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 8.7
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 210 to 430
1110
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
32
Strength to Weight: Axial, points 23 to 30
40
Strength to Weight: Bending, points 31 to 36
35
Thermal Shock Resistance, points 10 to 13
48

Alloy Composition

Aluminum (Al), % 96.6 to 97.8
0
Carbon (C), % 0
0 to 0.1
Copper (Cu), % 0 to 0.1
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.1
0 to 0.1
Magnesium (Mg), % 2.2 to 2.8
0
Manganese (Mn), % 0 to 0.1
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