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C16200 Copper vs. Nickel 59

C16200 copper belongs to the copper alloys classification, while nickel 59 belongs to the nickel alloys. There are 28 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.

For each property being compared, the top bar is C16200 copper and the bottom bar is nickel 59.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
220
Elongation at Break, % 2.0 to 56
50
Fatigue Strength, MPa 100 to 210
320
Poisson's Ratio 0.34
0.29
Shear Modulus, GPa 43
84
Shear Strength, MPa 190 to 390
560
Tensile Strength: Ultimate (UTS), MPa 240 to 550
780
Tensile Strength: Yield (Proof), MPa 48 to 470
350

Thermal Properties

Latent Heat of Fusion, J/g 210
330
Maximum Temperature: Mechanical, °C 370
990
Melting Completion (Liquidus), °C 1080
1500
Melting Onset (Solidus), °C 1030
1450
Specific Heat Capacity, J/kg-K 380
430
Thermal Conductivity, W/m-K 360
10
Thermal Expansion, µm/m-K 17
17

Otherwise Unclassified Properties

Base Metal Price, % relative 30
65
Density, g/cm3 9.0
8.7
Embodied Carbon, kg CO2/kg material 2.6
12
Embodied Energy, MJ/kg 41
160
Embodied Water, L/kg 310
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 99
320
Resilience: Unit (Modulus of Resilience), kJ/m3 10 to 970
280
Stiffness to Weight: Axial, points 7.2
14
Stiffness to Weight: Bending, points 18
23
Strength to Weight: Axial, points 7.4 to 17
25
Strength to Weight: Bending, points 9.6 to 17
22
Thermal Diffusivity, mm2/s 100
2.7
Thermal Shock Resistance, points 8.7 to 20
15

Alloy Composition

Aluminum (Al), % 0
0.1 to 0.4
Cadmium (Cd), % 0.7 to 1.2
0
Carbon (C), % 0
0 to 0.010
Chromium (Cr), % 0
22 to 24
Cobalt (Co), % 0
0 to 0.3
Copper (Cu), % 98.6 to 99.3
0 to 0.5
Iron (Fe), % 0 to 0.2
0 to 1.5
Manganese (Mn), % 0
0 to 0.5
Molybdenum (Mo), % 0
15 to 16.5
Nickel (Ni), % 0
56.2 to 62.9
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 0
0 to 0.1
Sulfur (S), % 0
0 to 0.010