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R58150 Titanium vs. 5254 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 5254 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 5254 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
68
Elongation at Break, % 13
3.4 to 22
Fatigue Strength, MPa 330
110 to 160
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
26
Shear Strength, MPa 470
150 to 200
Tensile Strength: Ultimate (UTS), MPa 770
240 to 350
Tensile Strength: Yield (Proof), MPa 550
100 to 270

Thermal Properties

Latent Heat of Fusion, J/g 410
400
Maximum Temperature: Mechanical, °C 320
190
Melting Completion (Liquidus), °C 1760
640
Melting Onset (Solidus), °C 1700
590
Specific Heat Capacity, J/kg-K 500
900
Thermal Expansion, µm/m-K 8.4
24

Otherwise Unclassified Properties

Base Metal Price, % relative 48
9.5
Density, g/cm3 5.4
2.7
Embodied Carbon, kg CO2/kg material 31
8.8
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
11 to 41
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
73 to 550
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 32
51
Strength to Weight: Axial, points 40
25 to 37
Strength to Weight: Bending, points 35
32 to 41
Thermal Shock Resistance, points 48
10 to 16

Alloy Composition

Aluminum (Al), % 0
94.4 to 96.8
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 0
0.15 to 0.35
Copper (Cu), % 0
0 to 0.050
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.45
Magnesium (Mg), % 0
3.1 to 3.9
Manganese (Mn), % 0
0 to 0.010
Molybdenum (Mo), % 14 to 16
0
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
0 to 0.45
Titanium (Ti), % 83.5 to 86
0 to 0.050
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15