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Titanium 6-7 vs. C355.0 Aluminum

Titanium 6-7 belongs to the titanium alloys classification, while C355.0 aluminum belongs to the aluminum alloys. There are 25 material properties with values for both materials. Properties with values for just one material (8, in this case) are not shown.

For each property being compared, the top bar is titanium 6-7 and the bottom bar is C355.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
70
Elongation at Break, % 11
2.7 to 3.8
Fatigue Strength, MPa 530
76 to 84
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 45
26
Tensile Strength: Ultimate (UTS), MPa 1020
290 to 310
Tensile Strength: Yield (Proof), MPa 900
200 to 230

Thermal Properties

Latent Heat of Fusion, J/g 410
470
Maximum Temperature: Mechanical, °C 300
170
Melting Completion (Liquidus), °C 1700
620
Melting Onset (Solidus), °C 1650
570
Specific Heat Capacity, J/kg-K 520
900
Thermal Expansion, µm/m-K 9.3
22

Otherwise Unclassified Properties

Base Metal Price, % relative 75
9.5
Density, g/cm3 5.1
2.7
Embodied Carbon, kg CO2/kg material 34
8.0
Embodied Energy, MJ/kg 540
150
Embodied Water, L/kg 190
1120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
7.5 to 9.8
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
290 to 380
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 32
51
Strength to Weight: Axial, points 56
30 to 32
Strength to Weight: Bending, points 44
36 to 37
Thermal Shock Resistance, points 66
13 to 14

Alloy Composition

Aluminum (Al), % 5.5 to 6.5
91.7 to 94.1
Carbon (C), % 0 to 0.080
0
Copper (Cu), % 0
1.0 to 1.5
Hydrogen (H), % 0 to 0.0090
0
Iron (Fe), % 0 to 0.25
0 to 0.2
Magnesium (Mg), % 0
0.4 to 0.6
Manganese (Mn), % 0
0 to 0.1
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
4.5 to 5.5
Tantalum (Ta), % 0 to 0.5
0
Titanium (Ti), % 84.9 to 88
0 to 0.2
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15