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C69400 Brass vs. Grade 21 Titanium

C69400 brass belongs to the copper alloys classification, while grade 21 titanium belongs to the titanium alloys. There are 27 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.

For each property being compared, the top bar is C69400 brass and the bottom bar is grade 21 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
140
Elongation at Break, % 17
9.0 to 17
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 42
51
Shear Strength, MPa 350
550 to 790
Tensile Strength: Ultimate (UTS), MPa 570
890 to 1340
Tensile Strength: Yield (Proof), MPa 270
870 to 1170

Thermal Properties

Latent Heat of Fusion, J/g 260
410
Maximum Temperature: Mechanical, °C 170
310
Melting Completion (Liquidus), °C 920
1740
Melting Onset (Solidus), °C 820
1690
Specific Heat Capacity, J/kg-K 410
500
Thermal Conductivity, W/m-K 26
7.5
Thermal Expansion, µm/m-K 18
7.1

Otherwise Unclassified Properties

Base Metal Price, % relative 27
60
Density, g/cm3 8.3
5.4
Embodied Carbon, kg CO2/kg material 2.7
32
Embodied Energy, MJ/kg 44
490
Embodied Water, L/kg 300
180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 80
110 to 180
Resilience: Unit (Modulus of Resilience), kJ/m3 340
2760 to 5010
Stiffness to Weight: Axial, points 7.4
14
Stiffness to Weight: Bending, points 19
32
Strength to Weight: Axial, points 19
46 to 69
Strength to Weight: Bending, points 18
38 to 50
Thermal Diffusivity, mm2/s 7.7
2.8
Thermal Shock Resistance, points 20
66 to 100

Alloy Composition

Aluminum (Al), % 0
2.5 to 3.5
Carbon (C), % 0
0 to 0.050
Copper (Cu), % 80 to 83
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.2
0 to 0.4
Lead (Pb), % 0 to 0.3
0
Molybdenum (Mo), % 0
14 to 16
Niobium (Nb), % 0
2.2 to 3.2
Nitrogen (N), % 0
0 to 0.030
Oxygen (O), % 0
0 to 0.17
Silicon (Si), % 3.5 to 4.5
0.15 to 0.25
Titanium (Ti), % 0
76 to 81.2
Zinc (Zn), % 11.5 to 16.5
0
Residuals, % 0
0 to 0.4