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C66900 Brass vs. R56406 Titanium

C66900 brass belongs to the copper alloys classification, while R56406 titanium belongs to the titanium alloys. There are 26 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 C66900 brass and the bottom bar is R56406 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
110
Elongation at Break, % 1.1 to 26
9.1
Poisson's Ratio 0.32
0.32
Shear Modulus, GPa 45
40
Tensile Strength: Ultimate (UTS), MPa 460 to 770
980
Tensile Strength: Yield (Proof), MPa 330 to 760
850

Thermal Properties

Latent Heat of Fusion, J/g 190
410
Maximum Temperature: Mechanical, °C 150
340
Melting Completion (Liquidus), °C 860
1610
Melting Onset (Solidus), °C 850
1560
Specific Heat Capacity, J/kg-K 400
560
Thermal Expansion, µm/m-K 20
9.6

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.4
1.0
Electrical Conductivity: Equal Weight (Specific), % IACS 3.8
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 23
36
Density, g/cm3 8.2
4.5
Embodied Carbon, kg CO2/kg material 2.8
38
Embodied Energy, MJ/kg 46
610
Embodied Water, L/kg 310
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.6 to 200
85
Resilience: Unit (Modulus of Resilience), kJ/m3 460 to 2450
3420
Stiffness to Weight: Axial, points 8.1
13
Stiffness to Weight: Bending, points 20
35
Strength to Weight: Axial, points 15 to 26
61
Strength to Weight: Bending, points 16 to 23
49
Thermal Shock Resistance, points 14 to 23
69

Alloy Composition

Aluminum (Al), % 0
5.5 to 6.8
Carbon (C), % 0
0 to 0.1
Copper (Cu), % 62.5 to 64.5
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.25
0 to 0.3
Lead (Pb), % 0 to 0.050
0
Manganese (Mn), % 11.5 to 12.5
0
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Titanium (Ti), % 0
88.1 to 91
Vanadium (V), % 0
3.5 to 4.5
Zinc (Zn), % 22.5 to 26
0
Residuals, % 0 to 0.2
0