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Grade 21 Titanium vs. C69400 Brass

Grade 21 titanium belongs to the titanium alloys classification, while C69400 brass belongs to the copper 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 grade 21 titanium and the bottom bar is C69400 brass.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

Aluminum (Al), % 2.5 to 3.5
0
Carbon (C), % 0 to 0.050
0
Copper (Cu), % 0
80 to 83
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.4
0 to 0.2
Lead (Pb), % 0
0 to 0.3
Molybdenum (Mo), % 14 to 16
0
Niobium (Nb), % 2.2 to 3.2
0
Nitrogen (N), % 0 to 0.030
0
Oxygen (O), % 0 to 0.17
0
Silicon (Si), % 0.15 to 0.25
3.5 to 4.5
Titanium (Ti), % 76 to 81.2
0
Zinc (Zn), % 0
11.5 to 16.5
Residuals, % 0
0 to 0.5