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Nickel 59 vs. C16200 Copper

Nickel 59 belongs to the nickel alloys classification, while C16200 copper belongs to the copper 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 nickel 59 and the bottom bar is C16200 copper.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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