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C66200 Brass vs. R58150 Titanium

C66200 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 (6, in this case) are not shown.

For each property being compared, the top bar is C66200 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, % 8.0 to 15
13
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 42
52
Shear Strength, MPa 270 to 300
470
Tensile Strength: Ultimate (UTS), MPa 450 to 520
770
Tensile Strength: Yield (Proof), MPa 410 to 480
550

Thermal Properties

Latent Heat of Fusion, J/g 200
410
Maximum Temperature: Mechanical, °C 180
320
Melting Completion (Liquidus), °C 1070
1760
Melting Onset (Solidus), °C 1030
1700
Specific Heat Capacity, J/kg-K 390
500
Thermal Expansion, µm/m-K 18
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 29
48
Density, g/cm3 8.7
5.4
Embodied Carbon, kg CO2/kg material 2.7
31
Embodied Energy, MJ/kg 43
480
Embodied Water, L/kg 320
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 40 to 66
94
Resilience: Unit (Modulus of Resilience), kJ/m3 760 to 1030
1110
Stiffness to Weight: Axial, points 7.2
14
Stiffness to Weight: Bending, points 19
32
Strength to Weight: Axial, points 14 to 17
40
Strength to Weight: Bending, points 15 to 16
35
Thermal Shock Resistance, points 16 to 18
48

Alloy Composition

Carbon (C), % 0
0 to 0.1
Copper (Cu), % 86.6 to 91
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.050
0 to 0.1
Lead (Pb), % 0 to 0.050
0
Molybdenum (Mo), % 0
14 to 16
Nickel (Ni), % 0.3 to 1.0
0
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Phosphorus (P), % 0.050 to 0.2
0
Tin (Sn), % 0.2 to 0.7
0
Titanium (Ti), % 0
83.5 to 86
Zinc (Zn), % 6.5 to 12.9
0
Residuals, % 0 to 0.5
0