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852.0 Aluminum vs. Titanium 6-7

852.0 aluminum belongs to the aluminum alloys classification, while titanium 6-7 belongs to the titanium 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 852.0 aluminum and the bottom bar is titanium 6-7.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
120
Elongation at Break, % 3.4
11
Fatigue Strength, MPa 73
530
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
45
Shear Strength, MPa 130
610
Tensile Strength: Ultimate (UTS), MPa 200
1020
Tensile Strength: Yield (Proof), MPa 150
900

Thermal Properties

Latent Heat of Fusion, J/g 370
410
Maximum Temperature: Mechanical, °C 190
300
Melting Completion (Liquidus), °C 640
1700
Melting Onset (Solidus), °C 210
1650
Specific Heat Capacity, J/kg-K 840
520
Thermal Expansion, µm/m-K 23
9.3

Otherwise Unclassified Properties

Base Metal Price, % relative 15
75
Density, g/cm3 3.2
5.1
Embodied Carbon, kg CO2/kg material 8.5
34
Embodied Energy, MJ/kg 160
540
Embodied Water, L/kg 1150
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.2
110
Resilience: Unit (Modulus of Resilience), kJ/m3 160
3460
Stiffness to Weight: Axial, points 12
13
Stiffness to Weight: Bending, points 43
32
Strength to Weight: Axial, points 17
56
Strength to Weight: Bending, points 24
44
Thermal Shock Resistance, points 8.7
66

Alloy Composition

Aluminum (Al), % 86.6 to 91.3
5.5 to 6.5
Carbon (C), % 0
0 to 0.080
Copper (Cu), % 1.7 to 2.3
0
Hydrogen (H), % 0
0 to 0.0090
Iron (Fe), % 0 to 0.7
0 to 0.25
Magnesium (Mg), % 0.6 to 0.9
0
Manganese (Mn), % 0 to 0.1
0
Molybdenum (Mo), % 0
6.5 to 7.5
Nickel (Ni), % 0.9 to 1.5
0
Niobium (Nb), % 0
6.5 to 7.5
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Silicon (Si), % 0 to 0.4
0
Tantalum (Ta), % 0
0 to 0.5
Tin (Sn), % 5.5 to 7.0
0
Titanium (Ti), % 0 to 0.2
84.9 to 88
Residuals, % 0 to 0.3
0