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N06230 Nickel vs. ZK61A Magnesium

N06230 nickel belongs to the nickel alloys classification, while ZK61A magnesium belongs to the magnesium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is N06230 nickel and the bottom bar is ZK61A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
46
Elongation at Break, % 38 to 48
5.8 to 7.1
Fatigue Strength, MPa 250 to 360
120 to 140
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 83
18
Shear Strength, MPa 420 to 600
170 to 180
Tensile Strength: Ultimate (UTS), MPa 620 to 840
290 to 310
Tensile Strength: Yield (Proof), MPa 330 to 400
180 to 200

Thermal Properties

Latent Heat of Fusion, J/g 310
330
Maximum Temperature: Mechanical, °C 990
120
Melting Completion (Liquidus), °C 1370
640
Melting Onset (Solidus), °C 1300
530
Specific Heat Capacity, J/kg-K 420
960
Thermal Conductivity, W/m-K 8.9
120
Thermal Expansion, µm/m-K 13
27

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
29
Electrical Conductivity: Equal Weight (Specific), % IACS 1.3
130

Otherwise Unclassified Properties

Base Metal Price, % relative 85
13
Density, g/cm3 9.5
1.9
Embodied Carbon, kg CO2/kg material 11
23
Embodied Energy, MJ/kg 160
160
Embodied Water, L/kg 290
940

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200 to 330
15 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 380
370 to 420
Stiffness to Weight: Axial, points 12
13
Stiffness to Weight: Bending, points 21
62
Strength to Weight: Axial, points 18 to 25
42 to 45
Strength to Weight: Bending, points 17 to 21
50 to 53
Thermal Diffusivity, mm2/s 2.3
65
Thermal Shock Resistance, points 17 to 23
17 to 18

Alloy Composition


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Aluminum (Al), % 0.2 to 0.5
0
Boron (B), % 0 to 0.015
0
Carbon (C), % 0.050 to 0.15
0
Chromium (Cr), % 20 to 24
0
Cobalt (Co), % 0 to 5.0
0
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 0 to 3.0
0
Lanthanum (La), % 0.0050 to 0.050
0
Magnesium (Mg), % 0
92.1 to 93.9
Manganese (Mn), % 0.3 to 1.0
0
Molybdenum (Mo), % 1.0 to 3.0
0
Nickel (Ni), % 47.5 to 65.2
0 to 0.010
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0.25 to 0.75
0
Sulfur (S), % 0 to 0.015
0
Tungsten (W), % 13 to 15
0
Zinc (Zn), % 0
5.5 to 6.5
Zirconium (Zr), % 0
0.6 to 1.0
Residuals, % 0
0 to 0.3