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Titanium 6-7 vs. 852.0 Aluminum

Titanium 6-7 belongs to the titanium alloys classification, while 852.0 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 852.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition


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Aluminum (Al), % 5.5 to 6.5
86.6 to 91.3
Carbon (C), % 0 to 0.080
0
Copper (Cu), % 0
1.7 to 2.3
Hydrogen (H), % 0 to 0.0090
0
Iron (Fe), % 0 to 0.25
0 to 0.7
Magnesium (Mg), % 0
0.6 to 0.9
Manganese (Mn), % 0
0 to 0.1
Molybdenum (Mo), % 6.5 to 7.5
0
Nickel (Ni), % 0
0.9 to 1.5
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 0.4
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