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C66700 Brass vs. R58150 Titanium

C66700 brass belongs to the copper alloys classification, while R58150 titanium belongs to the titanium alloys. There are 25 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 C66700 brass and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
140
Elongation at Break, % 2.0 to 58
13
Poisson's Ratio 0.31
0.32
Shear Modulus, GPa 41
52
Shear Strength, MPa 250 to 530
470
Tensile Strength: Ultimate (UTS), MPa 340 to 690
770
Tensile Strength: Yield (Proof), MPa 100 to 640
550

Thermal Properties

Latent Heat of Fusion, J/g 180
410
Maximum Temperature: Mechanical, °C 140
320
Melting Completion (Liquidus), °C 1090
1760
Melting Onset (Solidus), °C 1050
1700
Specific Heat Capacity, J/kg-K 390
500
Thermal Expansion, µm/m-K 20
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 25
48
Density, g/cm3 8.2
5.4
Embodied Carbon, kg CO2/kg material 2.7
31
Embodied Energy, MJ/kg 45
480
Embodied Water, L/kg 320
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 13 to 150
94
Resilience: Unit (Modulus of Resilience), kJ/m3 49 to 1900
1110
Stiffness to Weight: Axial, points 7.3
14
Stiffness to Weight: Bending, points 19
32
Strength to Weight: Axial, points 11 to 23
40
Strength to Weight: Bending, points 13 to 21
35
Thermal Shock Resistance, points 11 to 23
48

Alloy Composition

Carbon (C), % 0
0 to 0.1
Copper (Cu), % 68.5 to 71.5
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.1
0 to 0.1
Lead (Pb), % 0 to 0.070
0
Manganese (Mn), % 0.8 to 1.5
0
Molybdenum (Mo), % 0
14 to 16
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Titanium (Ti), % 0
83.5 to 86
Zinc (Zn), % 26.3 to 30.7
0
Residuals, % 0 to 0.5
0