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Titanium 6-7 vs. 4145 Aluminum

Titanium 6-7 belongs to the titanium alloys classification, while 4145 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 4145 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
73
Elongation at Break, % 11
2.2
Fatigue Strength, MPa 530
48
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 45
28
Shear Strength, MPa 610
69
Tensile Strength: Ultimate (UTS), MPa 1020
120
Tensile Strength: Yield (Proof), MPa 900
68

Thermal Properties

Latent Heat of Fusion, J/g 410
540
Maximum Temperature: Mechanical, °C 300
160
Melting Completion (Liquidus), °C 1700
590
Melting Onset (Solidus), °C 1650
520
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
7.6
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
31
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 32
50
Strength to Weight: Axial, points 56
12
Strength to Weight: Bending, points 44
19
Thermal Shock Resistance, points 66
5.5

Alloy Composition


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Aluminum (Al), % 5.5 to 6.5
83 to 87.4
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 0
0 to 0.15
Copper (Cu), % 0
3.3 to 4.7
Hydrogen (H), % 0 to 0.0090
0
Iron (Fe), % 0 to 0.25
0 to 0.8
Magnesium (Mg), % 0
0 to 0.15
Manganese (Mn), % 0
0 to 0.15
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
9.3 to 10.7
Tantalum (Ta), % 0 to 0.5
0
Titanium (Ti), % 84.9 to 88
0
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15