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Nickel 80A vs. C16200 Copper

Nickel 80A belongs to the nickel alloys classification, while C16200 copper belongs to the copper alloys.

For each property being compared, the top bar is nickel 80A and the bottom bar is C16200 copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
120
Elongation at Break, % 22
2.0 to 56
Fatigue Strength, MPa 430
100 to 210
Poisson's Ratio 0.29
0.34
Shear Modulus, GPa 74
43
Shear Strength, MPa 660
190 to 390
Tensile Strength: Ultimate (UTS), MPa 1040
240 to 550
Tensile Strength: Yield (Proof), MPa 710
48 to 470

Thermal Properties

Latent Heat of Fusion, J/g 320
210
Maximum Temperature: Mechanical, °C 980
370
Melting Completion (Liquidus), °C 1360
1080
Melting Onset (Solidus), °C 1310
1030
Specific Heat Capacity, J/kg-K 470
380
Thermal Conductivity, W/m-K 11
360
Thermal Expansion, µm/m-K 13
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.5
90
Electrical Conductivity: Equal Weight (Specific), % IACS 1.6
90

Otherwise Unclassified Properties

Base Metal Price, % relative 55
30
Density, g/cm3 8.3
9.0
Embodied Carbon, kg CO2/kg material 9.8
2.6
Embodied Energy, MJ/kg 140
41
Embodied Water, L/kg 280
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 210
10 to 99
Resilience: Unit (Modulus of Resilience), kJ/m3 1300
10 to 970
Stiffness to Weight: Axial, points 13
7.2
Stiffness to Weight: Bending, points 23
18
Strength to Weight: Axial, points 35
7.4 to 17
Strength to Weight: Bending, points 27
9.6 to 17
Thermal Diffusivity, mm2/s 2.9
100
Thermal Shock Resistance, points 31
8.7 to 20

Alloy Composition

Aluminum (Al), % 0.5 to 1.8
0
Cadmium (Cd), % 0
0.7 to 1.2
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 18 to 21
0
Copper (Cu), % 0
98.6 to 99.3
Iron (Fe), % 0 to 3.0
0 to 0.2
Manganese (Mn), % 0 to 1.0
0
Nickel (Ni), % 69.4 to 79.7
0
Silicon (Si), % 0 to 1.0
0
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 1.8 to 2.7
0