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R58150 Titanium vs. 201.0 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 201.0 aluminum belongs to the aluminum alloys. There are 25 material properties with values for both materials. Properties with values for just one material (10, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is 201.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
71
Elongation at Break, % 13
4.4 to 20
Fatigue Strength, MPa 330
120 to 150
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
27
Shear Strength, MPa 470
290
Tensile Strength: Ultimate (UTS), MPa 770
370 to 470
Tensile Strength: Yield (Proof), MPa 550
220 to 400

Thermal Properties

Latent Heat of Fusion, J/g 410
390
Maximum Temperature: Mechanical, °C 320
170
Melting Completion (Liquidus), °C 1760
650
Melting Onset (Solidus), °C 1700
570
Specific Heat Capacity, J/kg-K 500
870
Thermal Expansion, µm/m-K 8.4
19

Otherwise Unclassified Properties

Base Metal Price, % relative 48
38
Density, g/cm3 5.4
3.1
Embodied Carbon, kg CO2/kg material 31
8.7
Embodied Energy, MJ/kg 480
160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
19 to 63
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
330 to 1160
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 32
45
Strength to Weight: Axial, points 40
33 to 42
Strength to Weight: Bending, points 35
37 to 44
Thermal Shock Resistance, points 48
19 to 25

Alloy Composition


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Aluminum (Al), % 0
92.1 to 95.1
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
4.0 to 5.2
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.15
Magnesium (Mg), % 0
0.15 to 0.55
Manganese (Mn), % 0
0.2 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 0.1
Silver (Ag), % 0
0.4 to 1.0
Titanium (Ti), % 83.5 to 86
0.15 to 0.35
Residuals, % 0
0 to 0.1