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R58150 Titanium vs. 5251 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 5251 aluminum belongs to the aluminum 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 R58150 titanium and the bottom bar is 5251 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
68
Elongation at Break, % 13
2.0 to 19
Fatigue Strength, MPa 330
59 to 110
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
26
Shear Strength, MPa 470
110 to 160
Tensile Strength: Ultimate (UTS), MPa 770
180 to 280
Tensile Strength: Yield (Proof), MPa 550
67 to 250

Thermal Properties

Latent Heat of Fusion, J/g 410
400
Maximum Temperature: Mechanical, °C 320
180
Melting Completion (Liquidus), °C 1760
650
Melting Onset (Solidus), °C 1700
610
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
8.5
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
5.4 to 27
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
33 to 450
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 32
50
Strength to Weight: Axial, points 40
18 to 29
Strength to Weight: Bending, points 35
26 to 35
Thermal Shock Resistance, points 48
7.9 to 13

Alloy Composition

Aluminum (Al), % 0
95.5 to 98.2
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 0
0 to 0.15
Copper (Cu), % 0
0 to 0.15
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.5
Magnesium (Mg), % 0
1.7 to 2.4
Manganese (Mn), % 0
0.1 to 0.5
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 0.4
Titanium (Ti), % 83.5 to 86
0 to 0.15
Zinc (Zn), % 0
0 to 0.15
Residuals, % 0
0 to 0.15