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332.0 Aluminum vs. R58150 Titanium

332.0 aluminum belongs to the aluminum alloys classification, while R58150 titanium belongs to the titanium 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 332.0 aluminum and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

Latent Heat of Fusion, J/g 530
410
Maximum Temperature: Mechanical, °C 170
320
Melting Completion (Liquidus), °C 580
1760
Melting Onset (Solidus), °C 530
1700
Specific Heat Capacity, J/kg-K 880
500
Thermal Expansion, µm/m-K 21
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 10
48
Density, g/cm3 2.8
5.4
Embodied Carbon, kg CO2/kg material 7.8
31
Embodied Energy, MJ/kg 140
480
Embodied Water, L/kg 1040
150

Common Calculations

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

Alloy Composition

Aluminum (Al), % 80.1 to 89
0
Carbon (C), % 0
0 to 0.1
Copper (Cu), % 2.0 to 4.0
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 1.2
0 to 0.1
Magnesium (Mg), % 0.5 to 1.5
0
Manganese (Mn), % 0 to 0.5
0
Molybdenum (Mo), % 0
14 to 16
Nickel (Ni), % 0 to 0.5
0
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Silicon (Si), % 8.5 to 10.5
0
Titanium (Ti), % 0 to 0.25
83.5 to 86
Zinc (Zn), % 0 to 1.0
0
Residuals, % 0 to 0.5
0