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R58150 Titanium vs. 332.0 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 332.0 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 332.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
73
Elongation at Break, % 13
1.0
Fatigue Strength, MPa 330
90
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
27
Shear Strength, MPa 470
190
Tensile Strength: Ultimate (UTS), MPa 770
250
Tensile Strength: Yield (Proof), MPa 550
190

Thermal Properties

Latent Heat of Fusion, J/g 410
530
Maximum Temperature: Mechanical, °C 320
170
Melting Completion (Liquidus), °C 1760
580
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
7.8
Embodied Energy, MJ/kg 480
140
Embodied Water, L/kg 150
1040

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
2.3
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
250
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 32
50
Strength to Weight: Axial, points 40
24
Strength to Weight: Bending, points 35
31
Thermal Shock Resistance, points 48
12

Alloy Composition

Aluminum (Al), % 0
80.1 to 89
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
2.0 to 4.0
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 1.2
Magnesium (Mg), % 0
0.5 to 1.5
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
8.5 to 10.5
Titanium (Ti), % 83.5 to 86
0 to 0.25
Zinc (Zn), % 0
0 to 1.0
Residuals, % 0
0 to 0.5