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Nickel 890 vs. C16200 Copper

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

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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