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R58150 Titanium vs. CC765S Brass

R58150 titanium belongs to the titanium alloys classification, while CC765S brass belongs to the copper 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 R58150 titanium and the bottom bar is CC765S brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
110
Elongation at Break, % 13
21
Poisson's Ratio 0.32
0.31
Shear Modulus, GPa 52
42
Tensile Strength: Ultimate (UTS), MPa 770
540
Tensile Strength: Yield (Proof), MPa 550
220

Thermal Properties

Latent Heat of Fusion, J/g 410
180
Maximum Temperature: Mechanical, °C 320
140
Melting Completion (Liquidus), °C 1760
860
Melting Onset (Solidus), °C 1700
820
Specific Heat Capacity, J/kg-K 500
400
Thermal Expansion, µm/m-K 8.4
20

Otherwise Unclassified Properties

Base Metal Price, % relative 48
24
Density, g/cm3 5.4
8.0
Embodied Carbon, kg CO2/kg material 31
3.0
Embodied Energy, MJ/kg 480
51
Embodied Water, L/kg 150
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
90
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
220
Stiffness to Weight: Axial, points 14
7.6
Stiffness to Weight: Bending, points 32
20
Strength to Weight: Axial, points 40
19
Strength to Weight: Bending, points 35
18
Thermal Shock Resistance, points 48
17

Alloy Composition

Aluminum (Al), % 0
0.5 to 2.5
Antimony (Sb), % 0
0 to 0.080
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
51 to 65
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0.5 to 2.0
Lead (Pb), % 0
0 to 0.5
Manganese (Mn), % 0
0.3 to 3.0
Molybdenum (Mo), % 14 to 16
0
Nickel (Ni), % 0
0 to 6.0
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0
0 to 0.1
Tin (Sn), % 0
0 to 1.0
Titanium (Ti), % 83.5 to 86
0
Zinc (Zn), % 0
19.8 to 47.7