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Titanium 6-7 vs. C85500 Brass

Titanium 6-7 belongs to the titanium alloys classification, while C85500 brass belongs to the copper alloys. There are 24 material properties with values for both materials. Properties with values for just one material (9, in this case) are not shown.

For each property being compared, the top bar is titanium 6-7 and the bottom bar is C85500 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
100
Elongation at Break, % 11
40
Poisson's Ratio 0.33
0.31
Shear Modulus, GPa 45
40
Tensile Strength: Ultimate (UTS), MPa 1020
410
Tensile Strength: Yield (Proof), MPa 900
160

Thermal Properties

Latent Heat of Fusion, J/g 410
170
Maximum Temperature: Mechanical, °C 300
120
Melting Completion (Liquidus), °C 1700
900
Melting Onset (Solidus), °C 1650
890
Specific Heat Capacity, J/kg-K 520
390
Thermal Expansion, µm/m-K 9.3
21

Otherwise Unclassified Properties

Base Metal Price, % relative 75
23
Density, g/cm3 5.1
8.0
Embodied Carbon, kg CO2/kg material 34
2.7
Embodied Energy, MJ/kg 540
46
Embodied Water, L/kg 190
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
130
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
120
Stiffness to Weight: Axial, points 13
7.3
Stiffness to Weight: Bending, points 32
20
Strength to Weight: Axial, points 56
14
Strength to Weight: Bending, points 44
15
Thermal Shock Resistance, points 66
14

Alloy Composition

Aluminum (Al), % 5.5 to 6.5
0
Carbon (C), % 0 to 0.080
0
Copper (Cu), % 0
59 to 63
Hydrogen (H), % 0 to 0.0090
0
Iron (Fe), % 0 to 0.25
0 to 0.2
Lead (Pb), % 0
0 to 0.2
Manganese (Mn), % 0
0 to 0.2
Molybdenum (Mo), % 6.5 to 7.5
0
Nickel (Ni), % 0
0 to 0.2
Niobium (Nb), % 6.5 to 7.5
0
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Tantalum (Ta), % 0 to 0.5
0
Tin (Sn), % 0
0 to 0.2
Titanium (Ti), % 84.9 to 88
0
Zinc (Zn), % 0
35.1 to 41
Residuals, % 0
0 to 0.9