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C16200 Copper vs. Nickel 890

C16200 copper belongs to the copper alloys classification, while nickel 890 belongs to the nickel alloys. There are 26 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 C16200 copper and the bottom bar is nickel 890.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
200
Elongation at Break, % 2.0 to 56
39
Fatigue Strength, MPa 100 to 210
180
Poisson's Ratio 0.34
0.28
Shear Modulus, GPa 43
78
Shear Strength, MPa 190 to 390
400
Tensile Strength: Ultimate (UTS), MPa 240 to 550
590
Tensile Strength: Yield (Proof), MPa 48 to 470
230

Thermal Properties

Latent Heat of Fusion, J/g 210
330
Maximum Temperature: Mechanical, °C 370
1000
Melting Completion (Liquidus), °C 1080
1390
Melting Onset (Solidus), °C 1030
1340
Specific Heat Capacity, J/kg-K 380
480
Thermal Expansion, µm/m-K 17
14

Otherwise Unclassified Properties

Base Metal Price, % relative 30
47
Density, g/cm3 9.0
8.1
Embodied Carbon, kg CO2/kg material 2.6
8.2
Embodied Energy, MJ/kg 41
120
Embodied Water, L/kg 310
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 99
180
Resilience: Unit (Modulus of Resilience), kJ/m3 10 to 970
140
Stiffness to Weight: Axial, points 7.2
14
Stiffness to Weight: Bending, points 18
24
Strength to Weight: Axial, points 7.4 to 17
20
Strength to Weight: Bending, points 9.6 to 17
19
Thermal Shock Resistance, points 8.7 to 20
15

Alloy Composition

Aluminum (Al), % 0
0.050 to 0.6
Cadmium (Cd), % 0.7 to 1.2
0
Carbon (C), % 0
0.060 to 0.14
Chromium (Cr), % 0
23.5 to 28.5
Copper (Cu), % 98.6 to 99.3
0 to 0.75
Iron (Fe), % 0 to 0.2
17.3 to 33.9
Manganese (Mn), % 0
0 to 1.5
Molybdenum (Mo), % 0
1.0 to 2.0
Nickel (Ni), % 0
40 to 45
Niobium (Nb), % 0
0.2 to 1.0
Silicon (Si), % 0
1.0 to 2.0
Sulfur (S), % 0
0 to 0.015
Tantalum (Ta), % 0
0.1 to 0.6
Titanium (Ti), % 0
0.15 to 0.6