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ZK61A Magnesium vs. EN 2.4668 Nickel

ZK61A magnesium belongs to the magnesium alloys classification, while EN 2.4668 nickel belongs to the nickel alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 EN 2.4668 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 5.8 to 7.1
14
Fatigue Strength, MPa 120 to 140
590
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
75
Shear Strength, MPa 170 to 180
840
Tensile Strength: Ultimate (UTS), MPa 290 to 310
1390
Tensile Strength: Yield (Proof), MPa 180 to 200
1160

Thermal Properties

Latent Heat of Fusion, J/g 330
310
Maximum Temperature: Mechanical, °C 120
980
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 530
1410
Specific Heat Capacity, J/kg-K 960
450
Thermal Conductivity, W/m-K 120
13
Thermal Expansion, µm/m-K 27
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 130
1.5

Otherwise Unclassified Properties

Base Metal Price, % relative 13
75
Density, g/cm3 1.9
8.3
Embodied Carbon, kg CO2/kg material 23
13
Embodied Energy, MJ/kg 160
190
Embodied Water, L/kg 940
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 19
180
Resilience: Unit (Modulus of Resilience), kJ/m3 370 to 420
3490
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 62
23
Strength to Weight: Axial, points 42 to 45
46
Strength to Weight: Bending, points 50 to 53
33
Thermal Diffusivity, mm2/s 65
3.5
Thermal Shock Resistance, points 17 to 18
40

Alloy Composition

Aluminum (Al), % 0
0.3 to 0.7
Boron (B), % 0
0.0020 to 0.0060
Carbon (C), % 0
0.020 to 0.080
Chromium (Cr), % 0
17 to 21
Cobalt (Co), % 0
0 to 1.0
Copper (Cu), % 0 to 0.1
0 to 0.3
Iron (Fe), % 0
11.2 to 24.6
Magnesium (Mg), % 92.1 to 93.9
0
Manganese (Mn), % 0
0 to 0.35
Molybdenum (Mo), % 0
2.8 to 3.3
Nickel (Ni), % 0 to 0.010
50 to 55
Niobium (Nb), % 0
4.7 to 5.5
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 0
0 to 0.35
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0
0.6 to 1.2
Zinc (Zn), % 5.5 to 6.5
0
Zirconium (Zr), % 0.6 to 1.0
0
Residuals, % 0 to 0.3
0