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Titanium 6-7 vs. CC766S Brass

Titanium 6-7 belongs to the titanium alloys classification, while CC766S brass belongs to the copper alloys. There are 24 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 CC766S brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
110
Elongation at Break, % 11
28
Poisson's Ratio 0.33
0.31
Shear Modulus, GPa 45
40
Tensile Strength: Ultimate (UTS), MPa 1020
500
Tensile Strength: Yield (Proof), MPa 900
190

Thermal Properties

Latent Heat of Fusion, J/g 410
180
Maximum Temperature: Mechanical, °C 300
130
Melting Completion (Liquidus), °C 1700
840
Melting Onset (Solidus), °C 1650
800
Specific Heat Capacity, J/kg-K 520
390
Thermal Expansion, µm/m-K 9.3
20

Otherwise Unclassified Properties

Base Metal Price, % relative 75
24
Density, g/cm3 5.1
8.0
Embodied Carbon, kg CO2/kg material 34
2.8
Embodied Energy, MJ/kg 540
48
Embodied Water, L/kg 190
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
110
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
180
Stiffness to Weight: Axial, points 13
7.3
Stiffness to Weight: Bending, points 32
20
Strength to Weight: Axial, points 56
17
Strength to Weight: Bending, points 44
18
Thermal Shock Resistance, points 66
17

Alloy Composition

Aluminum (Al), % 5.5 to 6.5
0.3 to 1.8
Antimony (Sb), % 0
0 to 0.1
Carbon (C), % 0 to 0.080
0
Copper (Cu), % 0
58 to 64
Hydrogen (H), % 0 to 0.0090
0
Iron (Fe), % 0 to 0.25
0 to 0.5
Lead (Pb), % 0
0 to 0.5
Manganese (Mn), % 0
0 to 0.5
Molybdenum (Mo), % 6.5 to 7.5
0
Nickel (Ni), % 0
0 to 2.0
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 0.6
Tantalum (Ta), % 0 to 0.5
0
Tin (Sn), % 0
0 to 0.5
Titanium (Ti), % 84.9 to 88
0
Zinc (Zn), % 0
29.5 to 41.7