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R58150 Titanium vs. B390.0 Aluminum

R58150 titanium belongs to the titanium alloys classification, while B390.0 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 B390.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
76
Elongation at Break, % 13
0.88
Fatigue Strength, MPa 330
170
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
29
Tensile Strength: Ultimate (UTS), MPa 770
320
Tensile Strength: Yield (Proof), MPa 550
250

Thermal Properties

Latent Heat of Fusion, J/g 410
640
Maximum Temperature: Mechanical, °C 320
170
Melting Completion (Liquidus), °C 1760
580
Melting Onset (Solidus), °C 1700
580
Specific Heat Capacity, J/kg-K 500
880
Thermal Expansion, µm/m-K 8.4
20

Otherwise Unclassified Properties

Base Metal Price, % relative 48
11
Density, g/cm3 5.4
2.8
Embodied Carbon, kg CO2/kg material 31
7.3
Embodied Energy, MJ/kg 480
130
Embodied Water, L/kg 150
940

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
2.6
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
410
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 32
51
Strength to Weight: Axial, points 40
32
Strength to Weight: Bending, points 35
38
Thermal Shock Resistance, points 48
15

Alloy Composition

Aluminum (Al), % 0
72.7 to 79.6
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
4.0 to 5.0
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 1.3
Magnesium (Mg), % 0
0.45 to 0.65
Manganese (Mn), % 0
0 to 0.5
Molybdenum (Mo), % 14 to 16
0
Nickel (Ni), % 0
0 to 0.1
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
16 to 18
Titanium (Ti), % 83.5 to 86
0 to 0.1
Zinc (Zn), % 0
0 to 1.5
Residuals, % 0
0 to 0.2