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Titanium 6-7 vs. EN AC-21100 Aluminum

Titanium 6-7 belongs to the titanium alloys classification, while EN AC-21100 aluminum belongs to the aluminum alloys. There are 25 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown.

For each property being compared, the top bar is titanium 6-7 and the bottom bar is EN AC-21100 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
71
Elongation at Break, % 11
6.2 to 7.3
Fatigue Strength, MPa 530
79 to 87
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 45
27
Tensile Strength: Ultimate (UTS), MPa 1020
340 to 350
Tensile Strength: Yield (Proof), MPa 900
210 to 240

Thermal Properties

Latent Heat of Fusion, J/g 410
390
Maximum Temperature: Mechanical, °C 300
170
Melting Completion (Liquidus), °C 1700
670
Melting Onset (Solidus), °C 1650
550
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
8.0
Embodied Energy, MJ/kg 540
150
Embodied Water, L/kg 190
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
19 to 21
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
300 to 400
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 32
46
Strength to Weight: Axial, points 56
31 to 33
Strength to Weight: Bending, points 44
36 to 37
Thermal Shock Resistance, points 66
15

Alloy Composition

Aluminum (Al), % 5.5 to 6.5
93.4 to 95.7
Carbon (C), % 0 to 0.080
0
Copper (Cu), % 0
4.2 to 5.2
Hydrogen (H), % 0 to 0.0090
0
Iron (Fe), % 0 to 0.25
0 to 0.19
Manganese (Mn), % 0
0 to 0.55
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 0.18
Tantalum (Ta), % 0 to 0.5
0
Titanium (Ti), % 84.9 to 88
0.15 to 0.3
Zinc (Zn), % 0
0 to 0.070
Residuals, % 0
0 to 0.1