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Titanium 6-7 vs. 201.0 Aluminum

Titanium 6-7 belongs to the titanium alloys classification, while 201.0 aluminum belongs to the aluminum alloys. There are 25 material properties with values for both materials. Properties with values for just one material (10, in this case) are not shown.

For each property being compared, the top bar is titanium 6-7 and the bottom bar is 201.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
71
Elongation at Break, % 11
4.4 to 20
Fatigue Strength, MPa 530
120 to 150
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 45
27
Shear Strength, MPa 610
290
Tensile Strength: Ultimate (UTS), MPa 1020
370 to 470
Tensile Strength: Yield (Proof), MPa 900
220 to 400

Thermal Properties

Latent Heat of Fusion, J/g 410
390
Maximum Temperature: Mechanical, °C 300
170
Melting Completion (Liquidus), °C 1700
650
Melting Onset (Solidus), °C 1650
570
Specific Heat Capacity, J/kg-K 520
870
Thermal Expansion, µm/m-K 9.3
19

Otherwise Unclassified Properties

Base Metal Price, % relative 75
38
Density, g/cm3 5.1
3.1
Embodied Carbon, kg CO2/kg material 34
8.7
Embodied Energy, MJ/kg 540
160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
19 to 63
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
330 to 1160
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 32
45
Strength to Weight: Axial, points 56
33 to 42
Strength to Weight: Bending, points 44
37 to 44
Thermal Shock Resistance, points 66
19 to 25

Alloy Composition

Aluminum (Al), % 5.5 to 6.5
92.1 to 95.1
Carbon (C), % 0 to 0.080
0
Copper (Cu), % 0
4.0 to 5.2
Hydrogen (H), % 0 to 0.0090
0
Iron (Fe), % 0 to 0.25
0 to 0.15
Magnesium (Mg), % 0
0.15 to 0.55
Manganese (Mn), % 0
0.2 to 0.5
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
0 to 0.1
Silver (Ag), % 0
0.4 to 1.0
Tantalum (Ta), % 0 to 0.5
0
Titanium (Ti), % 84.9 to 88
0.15 to 0.35
Residuals, % 0
0 to 0.1