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R58150 Titanium vs. C66200 Brass

R58150 titanium belongs to the titanium alloys classification, while C66200 brass belongs to the copper 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 R58150 titanium and the bottom bar is C66200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
110
Elongation at Break, % 13
8.0 to 15
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
42
Shear Strength, MPa 470
270 to 300
Tensile Strength: Ultimate (UTS), MPa 770
450 to 520
Tensile Strength: Yield (Proof), MPa 550
410 to 480

Thermal Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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