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Titanium 6-7 vs. 332.0 Aluminum

Titanium 6-7 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 titanium 6-7 and the bottom bar is 332.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
73
Elongation at Break, % 11
1.0
Fatigue Strength, MPa 530
90
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 45
27
Shear Strength, MPa 610
190
Tensile Strength: Ultimate (UTS), MPa 1020
250
Tensile Strength: Yield (Proof), MPa 900
190

Thermal Properties

Latent Heat of Fusion, J/g 410
530
Maximum Temperature: Mechanical, °C 300
170
Melting Completion (Liquidus), °C 1700
580
Melting Onset (Solidus), °C 1650
530
Specific Heat Capacity, J/kg-K 520
880
Thermal Expansion, µm/m-K 9.3
21

Otherwise Unclassified Properties

Base Metal Price, % relative 75
10
Density, g/cm3 5.1
2.8
Embodied Carbon, kg CO2/kg material 34
7.8
Embodied Energy, MJ/kg 540
140
Embodied Water, L/kg 190
1040

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
2.3
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
250
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 32
50
Strength to Weight: Axial, points 56
24
Strength to Weight: Bending, points 44
31
Thermal Shock Resistance, points 66
12

Alloy Composition

Aluminum (Al), % 5.5 to 6.5
80.1 to 89
Carbon (C), % 0 to 0.080
0
Copper (Cu), % 0
2.0 to 4.0
Hydrogen (H), % 0 to 0.0090
0
Iron (Fe), % 0 to 0.25
0 to 1.2
Magnesium (Mg), % 0
0.5 to 1.5
Manganese (Mn), % 0
0 to 0.5
Molybdenum (Mo), % 6.5 to 7.5
0
Nickel (Ni), % 0
0 to 0.5
Niobium (Nb), % 6.5 to 7.5
0
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
8.5 to 10.5
Tantalum (Ta), % 0 to 0.5
0
Titanium (Ti), % 84.9 to 88
0 to 0.25
Zinc (Zn), % 0
0 to 1.0
Residuals, % 0
0 to 0.5