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Titanium 6-7 vs. 2618 Aluminum

Titanium 6-7 belongs to the titanium alloys classification, while 2618 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 2618 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
71
Elongation at Break, % 11
5.8
Fatigue Strength, MPa 530
110
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 45
27
Shear Strength, MPa 610
260
Tensile Strength: Ultimate (UTS), MPa 1020
420
Tensile Strength: Yield (Proof), MPa 900
350

Thermal Properties

Latent Heat of Fusion, J/g 410
390
Maximum Temperature: Mechanical, °C 300
210
Melting Completion (Liquidus), °C 1700
640
Melting Onset (Solidus), °C 1650
550
Specific Heat Capacity, J/kg-K 520
880
Thermal Expansion, µm/m-K 9.3
22

Otherwise Unclassified Properties

Base Metal Price, % relative 75
11
Density, g/cm3 5.1
2.9
Embodied Carbon, kg CO2/kg material 34
8.3
Embodied Energy, MJ/kg 540
150
Embodied Water, L/kg 190
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
23
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
850
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 32
47
Strength to Weight: Axial, points 56
40
Strength to Weight: Bending, points 44
42
Thermal Shock Resistance, points 66
19

Alloy Composition

Aluminum (Al), % 5.5 to 6.5
92.4 to 94.9
Carbon (C), % 0 to 0.080
0
Copper (Cu), % 0
1.9 to 2.7
Hydrogen (H), % 0 to 0.0090
0
Iron (Fe), % 0 to 0.25
0.9 to 1.3
Magnesium (Mg), % 0
1.3 to 1.8
Molybdenum (Mo), % 6.5 to 7.5
0
Nickel (Ni), % 0
0.9 to 1.2
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
0.1 to 0.25
Tantalum (Ta), % 0 to 0.5
0
Titanium (Ti), % 84.9 to 88
0.040 to 0.1
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15