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Titanium 6-7 vs. A201.0 Aluminum

Titanium 6-7 belongs to the titanium alloys classification, while A201.0 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 A201.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
71
Elongation at Break, % 11
4.7
Fatigue Strength, MPa 530
97
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 45
27
Tensile Strength: Ultimate (UTS), MPa 1020
480
Tensile Strength: Yield (Proof), MPa 900
420

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
880
Thermal Expansion, µm/m-K 9.3
23

Otherwise Unclassified Properties

Base Metal Price, % relative 75
11
Density, g/cm3 5.1
3.0
Embodied Carbon, kg CO2/kg material 34
8.1
Embodied Energy, MJ/kg 540
150
Embodied Water, L/kg 190
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
22
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
1250
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 32
46
Strength to Weight: Axial, points 56
44
Strength to Weight: Bending, points 44
45
Thermal Shock Resistance, points 66
21

Alloy Composition


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Aluminum (Al), % 5.5 to 6.5
93.7 to 95.5
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 0.1
Magnesium (Mg), % 0
0.15 to 0.35
Manganese (Mn), % 0
0.2 to 0.4
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 0.050
Tantalum (Ta), % 0 to 0.5
0
Titanium (Ti), % 84.9 to 88
0.15 to 0.35
Residuals, % 0
0 to 0.1