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C85200 Brass vs. R58150 Titanium

C85200 brass belongs to the copper alloys classification, while R58150 titanium belongs to the titanium alloys. There are 24 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown.

For each property being compared, the top bar is C85200 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, % 28
13
Poisson's Ratio 0.32
0.32
Shear Modulus, GPa 40
52
Tensile Strength: Ultimate (UTS), MPa 270
770
Tensile Strength: Yield (Proof), MPa 95
550

Thermal Properties

Latent Heat of Fusion, J/g 180
410
Maximum Temperature: Mechanical, °C 140
320
Melting Completion (Liquidus), °C 940
1760
Melting Onset (Solidus), °C 930
1700
Specific Heat Capacity, J/kg-K 380
500
Thermal Expansion, µm/m-K 20
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 26
48
Density, g/cm3 8.4
5.4
Embodied Carbon, kg CO2/kg material 2.8
31
Embodied Energy, MJ/kg 46
480
Embodied Water, L/kg 330
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 59
94
Resilience: Unit (Modulus of Resilience), kJ/m3 42
1110
Stiffness to Weight: Axial, points 7.0
14
Stiffness to Weight: Bending, points 19
32
Strength to Weight: Axial, points 8.9
40
Strength to Weight: Bending, points 11
35
Thermal Shock Resistance, points 9.3
48

Alloy Composition

Aluminum (Al), % 0 to 0.0050
0
Antimony (Sb), % 0 to 0.2
0
Carbon (C), % 0
0 to 0.1
Copper (Cu), % 70 to 74
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.6
0 to 0.1
Lead (Pb), % 1.5 to 3.8
0
Molybdenum (Mo), % 0
14 to 16
Nickel (Ni), % 0 to 1.0
0
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.050
0
Sulfur (S), % 0 to 0.050
0
Tin (Sn), % 0.7 to 2.0
0
Titanium (Ti), % 0
83.5 to 86
Zinc (Zn), % 20 to 27
0
Residuals, % 0 to 0.9
0