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Titanium 6-7 vs. CC765S Brass

Titanium 6-7 belongs to the titanium alloys classification, while CC765S 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 CC765S brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
110
Elongation at Break, % 11
21
Poisson's Ratio 0.33
0.31
Shear Modulus, GPa 45
42
Tensile Strength: Ultimate (UTS), MPa 1020
540
Tensile Strength: Yield (Proof), MPa 900
220

Thermal Properties

Latent Heat of Fusion, J/g 410
180
Maximum Temperature: Mechanical, °C 300
140
Melting Completion (Liquidus), °C 1700
860
Melting Onset (Solidus), °C 1650
820
Specific Heat Capacity, J/kg-K 520
400
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
3.0
Embodied Energy, MJ/kg 540
51
Embodied Water, L/kg 190
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
90
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
220
Stiffness to Weight: Axial, points 13
7.6
Stiffness to Weight: Bending, points 32
20
Strength to Weight: Axial, points 56
19
Strength to Weight: Bending, points 44
18
Thermal Shock Resistance, points 66
17

Alloy Composition

Aluminum (Al), % 5.5 to 6.5
0.5 to 2.5
Antimony (Sb), % 0
0 to 0.080
Carbon (C), % 0 to 0.080
0
Copper (Cu), % 0
51 to 65
Hydrogen (H), % 0 to 0.0090
0
Iron (Fe), % 0 to 0.25
0.5 to 2.0
Lead (Pb), % 0
0 to 0.5
Manganese (Mn), % 0
0.3 to 3.0
Molybdenum (Mo), % 6.5 to 7.5
0
Nickel (Ni), % 0
0 to 6.0
Niobium (Nb), % 6.5 to 7.5
0
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0
0 to 0.1
Tantalum (Ta), % 0 to 0.5
0
Tin (Sn), % 0
0 to 1.0
Titanium (Ti), % 84.9 to 88
0
Zinc (Zn), % 0
19.8 to 47.7