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C17510 Copper vs. Grade 5 Titanium

C17510 copper belongs to the copper alloys classification, while grade 5 titanium belongs to the titanium alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is C17510 copper and the bottom bar is grade 5 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
110
Elongation at Break, % 5.4 to 37
8.6 to 11
Poisson's Ratio 0.34
0.32
Shear Modulus, GPa 44
40
Shear Strength, MPa 210 to 500
600 to 710
Tensile Strength: Ultimate (UTS), MPa 310 to 860
1000 to 1190
Tensile Strength: Yield (Proof), MPa 120 to 750
910 to 1110

Thermal Properties

Latent Heat of Fusion, J/g 220
410
Maximum Temperature: Mechanical, °C 220
330
Melting Completion (Liquidus), °C 1070
1610
Melting Onset (Solidus), °C 1030
1650
Specific Heat Capacity, J/kg-K 390
560
Thermal Conductivity, W/m-K 210
6.8
Thermal Expansion, µm/m-K 17
8.9

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 22 to 54
1.0
Electrical Conductivity: Equal Weight (Specific), % IACS 23 to 54
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 49
36
Density, g/cm3 8.9
4.4
Embodied Carbon, kg CO2/kg material 4.2
38
Embodied Energy, MJ/kg 65
610
Embodied Water, L/kg 310
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 39 to 92
100 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 64 to 2410
3980 to 5880
Stiffness to Weight: Axial, points 7.4
13
Stiffness to Weight: Bending, points 18
35
Strength to Weight: Axial, points 9.7 to 27
62 to 75
Strength to Weight: Bending, points 11 to 23
50 to 56
Thermal Diffusivity, mm2/s 60
2.7
Thermal Shock Resistance, points 11 to 30
76 to 91

Alloy Composition


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Aluminum (Al), % 0 to 0.2
5.5 to 6.8
Beryllium (Be), % 0.2 to 0.6
0
Carbon (C), % 0
0 to 0.080
Cobalt (Co), % 0 to 0.3
0
Copper (Cu), % 95.9 to 98.4
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.1
0 to 0.4
Nickel (Ni), % 1.4 to 2.2
0
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Silicon (Si), % 0 to 0.2
0
Titanium (Ti), % 0
87.4 to 91
Vanadium (V), % 0
3.5 to 4.5
Yttrium (Y), % 0
0 to 0.0050
Residuals, % 0 to 0.5
0 to 0.4