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R58150 Titanium vs. 240.0 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 240.0 aluminum belongs to the aluminum alloys. There are 25 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 240.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
72
Elongation at Break, % 13
1.0
Fatigue Strength, MPa 330
140
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
27
Tensile Strength: Ultimate (UTS), MPa 770
240
Tensile Strength: Yield (Proof), MPa 550
200

Thermal Properties

Latent Heat of Fusion, J/g 410
380
Maximum Temperature: Mechanical, °C 320
180
Melting Completion (Liquidus), °C 1760
600
Melting Onset (Solidus), °C 1700
520
Specific Heat Capacity, J/kg-K 500
860
Thermal Expansion, µm/m-K 8.4
22

Otherwise Unclassified Properties

Base Metal Price, % relative 48
12
Density, g/cm3 5.4
3.2
Embodied Carbon, kg CO2/kg material 31
8.7
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
2.2
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
280
Stiffness to Weight: Axial, points 14
12
Stiffness to Weight: Bending, points 32
43
Strength to Weight: Axial, points 40
20
Strength to Weight: Bending, points 35
26
Thermal Shock Resistance, points 48
11

Alloy Composition


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Aluminum (Al), % 0
81.7 to 86.9
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
7.0 to 9.0
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.5
Magnesium (Mg), % 0
5.5 to 6.5
Manganese (Mn), % 0
0.3 to 0.7
Molybdenum (Mo), % 14 to 16
0
Nickel (Ni), % 0
0.3 to 0.7
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
0 to 0.5
Titanium (Ti), % 83.5 to 86
0 to 0.2
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15