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C36200 Brass vs. R58150 Titanium

C36200 brass belongs to the copper alloys classification, while R58150 titanium belongs to the titanium alloys. There are 25 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 C36200 brass and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
140
Elongation at Break, % 20 to 53
13
Poisson's Ratio 0.31
0.32
Shear Modulus, GPa 39
52
Shear Strength, MPa 210 to 240
470
Tensile Strength: Ultimate (UTS), MPa 340 to 420
770
Tensile Strength: Yield (Proof), MPa 130 to 360
550

Thermal Properties

Latent Heat of Fusion, J/g 170
410
Maximum Temperature: Mechanical, °C 120
320
Melting Completion (Liquidus), °C 900
1760
Melting Onset (Solidus), °C 890
1700
Specific Heat Capacity, J/kg-K 380
500
Thermal Expansion, µm/m-K 21
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 23
48
Density, g/cm3 8.2
5.4
Embodied Carbon, kg CO2/kg material 2.6
31
Embodied Energy, MJ/kg 45
480
Embodied Water, L/kg 320
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 74 to 140
94
Resilience: Unit (Modulus of Resilience), kJ/m3 89 to 630
1110
Stiffness to Weight: Axial, points 6.9
14
Stiffness to Weight: Bending, points 19
32
Strength to Weight: Axial, points 11 to 14
40
Strength to Weight: Bending, points 13 to 15
35
Thermal Shock Resistance, points 11 to 14
48

Alloy Composition

Carbon (C), % 0
0 to 0.1
Copper (Cu), % 60 to 63
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.15
0 to 0.1
Lead (Pb), % 3.5 to 4.5
0
Molybdenum (Mo), % 0
14 to 16
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Titanium (Ti), % 0
83.5 to 86
Zinc (Zn), % 32.4 to 36.5
0