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ZK61A Magnesium vs. N06230 Nickel

ZK61A magnesium belongs to the magnesium alloys classification, while N06230 nickel belongs to the nickel 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 ZK61A magnesium and the bottom bar is N06230 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition


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