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R58150 Titanium vs. CC755S Brass

R58150 titanium belongs to the titanium alloys classification, while CC755S 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 CC755S brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
100
Elongation at Break, % 13
9.5
Poisson's Ratio 0.32
0.31
Shear Modulus, GPa 52
40
Tensile Strength: Ultimate (UTS), MPa 770
390
Tensile Strength: Yield (Proof), MPa 550
250

Thermal Properties

Latent Heat of Fusion, J/g 410
170
Maximum Temperature: Mechanical, °C 320
120
Melting Completion (Liquidus), °C 1760
820
Melting Onset (Solidus), °C 1700
780
Specific Heat Capacity, J/kg-K 500
390
Thermal Expansion, µm/m-K 8.4
21

Otherwise Unclassified Properties

Base Metal Price, % relative 48
23
Density, g/cm3 5.4
8.1
Embodied Carbon, kg CO2/kg material 31
2.7
Embodied Energy, MJ/kg 480
46
Embodied Water, L/kg 150
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
33
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
290
Stiffness to Weight: Axial, points 14
7.1
Stiffness to Weight: Bending, points 32
19
Strength to Weight: Axial, points 40
14
Strength to Weight: Bending, points 35
15
Thermal Shock Resistance, points 48
13

Alloy Composition

Aluminum (Al), % 0
0.4 to 0.7
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
59.5 to 61
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0.050 to 0.2
Lead (Pb), % 0
1.2 to 1.7
Manganese (Mn), % 0
0 to 0.050
Molybdenum (Mo), % 14 to 16
0
Nickel (Ni), % 0
0 to 0.2
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
0 to 0.050
Tin (Sn), % 0
0 to 0.3
Titanium (Ti), % 83.5 to 86
0
Zinc (Zn), % 0
35.8 to 38.9