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C66200 Brass vs. Titanium 6-7

C66200 brass belongs to the copper alloys classification, while titanium 6-7 belongs to the titanium alloys. There are 25 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.

For each property being compared, the top bar is C66200 brass and the bottom bar is titanium 6-7.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
120
Elongation at Break, % 8.0 to 15
11
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 42
45
Shear Strength, MPa 270 to 300
610
Tensile Strength: Ultimate (UTS), MPa 450 to 520
1020
Tensile Strength: Yield (Proof), MPa 410 to 480
900

Thermal Properties

Latent Heat of Fusion, J/g 200
410
Maximum Temperature: Mechanical, °C 180
300
Melting Completion (Liquidus), °C 1070
1700
Melting Onset (Solidus), °C 1030
1650
Specific Heat Capacity, J/kg-K 390
520
Thermal Expansion, µm/m-K 18
9.3

Otherwise Unclassified Properties

Base Metal Price, % relative 29
75
Density, g/cm3 8.7
5.1
Embodied Carbon, kg CO2/kg material 2.7
34
Embodied Energy, MJ/kg 43
540
Embodied Water, L/kg 320
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 40 to 66
110
Resilience: Unit (Modulus of Resilience), kJ/m3 760 to 1030
3460
Stiffness to Weight: Axial, points 7.2
13
Stiffness to Weight: Bending, points 19
32
Strength to Weight: Axial, points 14 to 17
56
Strength to Weight: Bending, points 15 to 16
44
Thermal Shock Resistance, points 16 to 18
66

Alloy Composition

Aluminum (Al), % 0
5.5 to 6.5
Carbon (C), % 0
0 to 0.080
Copper (Cu), % 86.6 to 91
0
Hydrogen (H), % 0
0 to 0.0090
Iron (Fe), % 0 to 0.050
0 to 0.25
Lead (Pb), % 0 to 0.050
0
Molybdenum (Mo), % 0
6.5 to 7.5
Nickel (Ni), % 0.3 to 1.0
0
Niobium (Nb), % 0
6.5 to 7.5
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Phosphorus (P), % 0.050 to 0.2
0
Tantalum (Ta), % 0
0 to 0.5
Tin (Sn), % 0.2 to 0.7
0
Titanium (Ti), % 0
84.9 to 88
Zinc (Zn), % 6.5 to 12.9
0
Residuals, % 0 to 0.5
0