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Titanium 6-7 vs. B390.0 Aluminum

Titanium 6-7 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 titanium 6-7 and the bottom bar is B390.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
76
Elongation at Break, % 11
0.88
Fatigue Strength, MPa 530
170
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 45
29
Tensile Strength: Ultimate (UTS), MPa 1020
320
Tensile Strength: Yield (Proof), MPa 900
250

Thermal Properties

Latent Heat of Fusion, J/g 410
640
Maximum Temperature: Mechanical, °C 300
170
Melting Completion (Liquidus), °C 1700
580
Melting Onset (Solidus), °C 1650
580
Specific Heat Capacity, J/kg-K 520
880
Thermal Expansion, µm/m-K 9.3
20

Otherwise Unclassified Properties

Base Metal Price, % relative 75
11
Density, g/cm3 5.1
2.8
Embodied Carbon, kg CO2/kg material 34
7.3
Embodied Energy, MJ/kg 540
130
Embodied Water, L/kg 190
940

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
2.6
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
410
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 32
51
Strength to Weight: Axial, points 56
32
Strength to Weight: Bending, points 44
38
Thermal Shock Resistance, points 66
15

Alloy Composition

Aluminum (Al), % 5.5 to 6.5
72.7 to 79.6
Carbon (C), % 0 to 0.080
0
Copper (Cu), % 0
4.0 to 5.0
Hydrogen (H), % 0 to 0.0090
0
Iron (Fe), % 0 to 0.25
0 to 1.3
Magnesium (Mg), % 0
0.45 to 0.65
Manganese (Mn), % 0
0 to 0.5
Molybdenum (Mo), % 6.5 to 7.5
0
Nickel (Ni), % 0
0 to 0.1
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
16 to 18
Tantalum (Ta), % 0 to 0.5
0
Titanium (Ti), % 84.9 to 88
0 to 0.1
Zinc (Zn), % 0
0 to 1.5
Residuals, % 0
0 to 0.2