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Titanium 6-7 vs. 850.0 Aluminum

Titanium 6-7 belongs to the titanium alloys classification, while 850.0 aluminum belongs to the aluminum alloys. There are 26 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 850.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
69
Elongation at Break, % 11
7.9
Fatigue Strength, MPa 530
59
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 45
26
Shear Strength, MPa 610
100
Tensile Strength: Ultimate (UTS), MPa 1020
140
Tensile Strength: Yield (Proof), MPa 900
76

Thermal Properties

Latent Heat of Fusion, J/g 410
380
Maximum Temperature: Mechanical, °C 300
190
Melting Completion (Liquidus), °C 1700
650
Melting Onset (Solidus), °C 1650
370
Specific Heat Capacity, J/kg-K 520
850
Thermal Expansion, µm/m-K 9.3
23

Otherwise Unclassified Properties

Base Metal Price, % relative 75
14
Density, g/cm3 5.1
3.1
Embodied Carbon, kg CO2/kg material 34
8.5
Embodied Energy, MJ/kg 540
160
Embodied Water, L/kg 190
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
9.1
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
42
Stiffness to Weight: Axial, points 13
12
Stiffness to Weight: Bending, points 32
44
Strength to Weight: Axial, points 56
12
Strength to Weight: Bending, points 44
19
Thermal Shock Resistance, points 66
6.1

Alloy Composition


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Aluminum (Al), % 5.5 to 6.5
88.3 to 93.1
Carbon (C), % 0 to 0.080
0
Copper (Cu), % 0
0.7 to 1.3
Hydrogen (H), % 0 to 0.0090
0
Iron (Fe), % 0 to 0.25
0 to 0.7
Magnesium (Mg), % 0
0 to 0.1
Manganese (Mn), % 0
0 to 0.1
Molybdenum (Mo), % 6.5 to 7.5
0
Nickel (Ni), % 0
0.7 to 1.3
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 0.7
Tantalum (Ta), % 0 to 0.5
0
Tin (Sn), % 0
5.5 to 7.0
Titanium (Ti), % 84.9 to 88
0 to 0.2
Residuals, % 0
0 to 0.3