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CC767S Brass vs. R58150 Titanium

CC767S 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 (8, in this case) are not shown.

For each property being compared, the top bar is CC767S 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, % 34
13
Poisson's Ratio 0.31
0.32
Shear Modulus, GPa 40
52
Tensile Strength: Ultimate (UTS), MPa 430
770
Tensile Strength: Yield (Proof), MPa 150
550

Thermal Properties

Latent Heat of Fusion, J/g 180
410
Maximum Temperature: Mechanical, °C 120
320
Melting Completion (Liquidus), °C 840
1760
Melting Onset (Solidus), °C 790
1700
Specific Heat Capacity, J/kg-K 390
500
Thermal Expansion, µm/m-K 21
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 23
48
Density, g/cm3 8.0
5.4
Embodied Carbon, kg CO2/kg material 2.7
31
Embodied Energy, MJ/kg 47
480
Embodied Water, L/kg 330
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
94
Resilience: Unit (Modulus of Resilience), kJ/m3 100
1110
Stiffness to Weight: Axial, points 7.3
14
Stiffness to Weight: Bending, points 20
32
Strength to Weight: Axial, points 15
40
Strength to Weight: Bending, points 16
35
Thermal Shock Resistance, points 14
48

Alloy Composition

Aluminum (Al), % 0.1 to 0.8
0
Carbon (C), % 0
0 to 0.1
Copper (Cu), % 58 to 64
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.5
0 to 0.1
Lead (Pb), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.5
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
Silicon (Si), % 0 to 0.2
0
Tin (Sn), % 0 to 0.1
0
Titanium (Ti), % 0
83.5 to 86
Zinc (Zn), % 32.8 to 41.9
0