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ZK61A Magnesium vs. N10675 Nickel

ZK61A magnesium belongs to the magnesium alloys classification, while N10675 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 N10675 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
220
Elongation at Break, % 5.8 to 7.1
47
Fatigue Strength, MPa 120 to 140
350
Poisson's Ratio 0.29
0.31
Shear Modulus, GPa 18
85
Shear Strength, MPa 170 to 180
610
Tensile Strength: Ultimate (UTS), MPa 290 to 310
860
Tensile Strength: Yield (Proof), MPa 180 to 200
400

Thermal Properties

Latent Heat of Fusion, J/g 330
320
Maximum Temperature: Mechanical, °C 120
910
Melting Completion (Liquidus), °C 640
1420
Melting Onset (Solidus), °C 530
1370
Specific Heat Capacity, J/kg-K 960
380
Thermal Conductivity, W/m-K 120
11
Thermal Expansion, µm/m-K 27
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
1.3
Electrical Conductivity: Equal Weight (Specific), % IACS 130
1.2

Otherwise Unclassified Properties

Base Metal Price, % relative 13
80
Density, g/cm3 1.9
9.3
Embodied Carbon, kg CO2/kg material 23
16
Embodied Energy, MJ/kg 160
210
Embodied Water, L/kg 940
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 19
330
Resilience: Unit (Modulus of Resilience), kJ/m3 370 to 420
350
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 62
22
Strength to Weight: Axial, points 42 to 45
26
Strength to Weight: Bending, points 50 to 53
22
Thermal Diffusivity, mm2/s 65
3.1
Thermal Shock Resistance, points 17 to 18
26

Alloy Composition


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Aluminum (Al), % 0
0 to 0.5
Carbon (C), % 0
0 to 0.010
Chromium (Cr), % 0
1.0 to 3.0
Cobalt (Co), % 0
0 to 3.0
Copper (Cu), % 0 to 0.1
0 to 0.2
Iron (Fe), % 0
1.0 to 3.0
Magnesium (Mg), % 92.1 to 93.9
0
Manganese (Mn), % 0
0 to 3.0
Molybdenum (Mo), % 0
27 to 32
Nickel (Ni), % 0 to 0.010
51.3 to 71
Niobium (Nb), % 0
0 to 0.2
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0
0 to 0.1
Sulfur (S), % 0
0 to 0.010
Tantalum (Ta), % 0
0 to 0.2
Titanium (Ti), % 0
0 to 0.2
Tungsten (W), % 0
0 to 3.0
Vanadium (V), % 0
0 to 0.2
Zinc (Zn), % 5.5 to 6.5
0 to 0.1
Zirconium (Zr), % 0.6 to 1.0
0
Residuals, % 0 to 0.3
0