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Titanium 6-7 vs. C66200 Brass

Titanium 6-7 belongs to the titanium alloys classification, while C66200 brass belongs to the copper 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 titanium 6-7 and the bottom bar is C66200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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