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R58150 Titanium vs. 333.0 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 333.0 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 333.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
73
Elongation at Break, % 13
1.0 to 2.0
Fatigue Strength, MPa 330
83 to 100
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
28
Shear Strength, MPa 470
190 to 230
Tensile Strength: Ultimate (UTS), MPa 770
230 to 280
Tensile Strength: Yield (Proof), MPa 550
130 to 210

Thermal Properties

Latent Heat of Fusion, J/g 410
520
Maximum Temperature: Mechanical, °C 320
170
Melting Completion (Liquidus), °C 1760
590
Melting Onset (Solidus), °C 1700
530
Specific Heat Capacity, J/kg-K 500
880
Thermal Expansion, µm/m-K 8.4
21

Otherwise Unclassified Properties

Base Metal Price, % relative 48
10
Density, g/cm3 5.4
2.8
Embodied Carbon, kg CO2/kg material 31
7.6
Embodied Energy, MJ/kg 480
140
Embodied Water, L/kg 150
1040

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
2.1 to 4.6
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
120 to 290
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 32
49
Strength to Weight: Axial, points 40
22 to 27
Strength to Weight: Bending, points 35
29 to 34
Thermal Shock Resistance, points 48
11 to 13

Alloy Composition


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Aluminum (Al), % 0
81.8 to 89
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
3.0 to 4.0
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 1.0
Magnesium (Mg), % 0
0.050 to 0.5
Manganese (Mn), % 0
0 to 0.5
Molybdenum (Mo), % 14 to 16
0
Nickel (Ni), % 0
0 to 0.5
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
8.0 to 10
Titanium (Ti), % 83.5 to 86
0 to 0.25
Zinc (Zn), % 0
0 to 1.0
Residuals, % 0
0 to 0.5