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Titanium 6-7 vs. 354.0 Aluminum

Titanium 6-7 belongs to the titanium alloys classification, while 354.0 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 titanium 6-7 and the bottom bar is 354.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
71
Elongation at Break, % 11
2.4 to 3.0
Fatigue Strength, MPa 530
92 to 120
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 45
27
Tensile Strength: Ultimate (UTS), MPa 1020
360 to 380
Tensile Strength: Yield (Proof), MPa 900
280 to 310

Thermal Properties

Latent Heat of Fusion, J/g 410
530
Maximum Temperature: Mechanical, °C 300
170
Melting Completion (Liquidus), °C 1700
600
Melting Onset (Solidus), °C 1650
550
Specific Heat Capacity, J/kg-K 520
900
Thermal Expansion, µm/m-K 9.3
21

Otherwise Unclassified Properties

Base Metal Price, % relative 75
9.5
Density, g/cm3 5.1
2.7
Embodied Carbon, kg CO2/kg material 34
7.8
Embodied Energy, MJ/kg 540
150
Embodied Water, L/kg 190
1070

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
8.6 to 9.8
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
540 to 670
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 32
52
Strength to Weight: Axial, points 56
37 to 39
Strength to Weight: Bending, points 44
42 to 44
Thermal Shock Resistance, points 66
17 to 18

Alloy Composition

Aluminum (Al), % 5.5 to 6.5
87.3 to 89.4
Carbon (C), % 0 to 0.080
0
Copper (Cu), % 0
1.6 to 2.0
Hydrogen (H), % 0 to 0.0090
0
Iron (Fe), % 0 to 0.25
0 to 0.2
Magnesium (Mg), % 0
0.4 to 0.6
Manganese (Mn), % 0
0 to 0.1
Molybdenum (Mo), % 6.5 to 7.5
0
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
8.6 to 9.4
Tantalum (Ta), % 0 to 0.5
0
Titanium (Ti), % 84.9 to 88
0 to 0.2
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15