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ZK60A Magnesium vs. Nickel 625

ZK60A magnesium belongs to the magnesium alloys classification, while nickel 625 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 ZK60A magnesium and the bottom bar is nickel 625.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 4.5 to 9.9
33 to 34
Fatigue Strength, MPa 150 to 180
240 to 320
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
79
Shear Strength, MPa 170 to 190
530 to 600
Tensile Strength: Ultimate (UTS), MPa 320 to 330
790 to 910
Tensile Strength: Yield (Proof), MPa 230 to 250
320 to 450

Thermal Properties

Latent Heat of Fusion, J/g 330
330
Maximum Temperature: Mechanical, °C 120
980
Melting Completion (Liquidus), °C 600
1350
Melting Onset (Solidus), °C 550
1290
Specific Heat Capacity, J/kg-K 960
440
Thermal Conductivity, W/m-K 120
11
Thermal Expansion, µm/m-K 26
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29 to 30
1.3
Electrical Conductivity: Equal Weight (Specific), % IACS 140
1.4

Otherwise Unclassified Properties

Base Metal Price, % relative 13
80
Density, g/cm3 1.9
8.6
Embodied Carbon, kg CO2/kg material 23
14
Embodied Energy, MJ/kg 160
190
Embodied Water, L/kg 940
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 29
220 to 250
Resilience: Unit (Modulus of Resilience), kJ/m3 570 to 690
260 to 490
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 63
23
Strength to Weight: Axial, points 47 to 49
26 to 29
Strength to Weight: Bending, points 55 to 56
22 to 24
Thermal Diffusivity, mm2/s 66
2.9
Thermal Shock Resistance, points 19 to 20
22 to 25

Alloy Composition

Aluminum (Al), % 0
0 to 0.4
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
20 to 23
Cobalt (Co), % 0
0 to 1.0
Iron (Fe), % 0
0 to 5.0
Magnesium (Mg), % 92.5 to 94.8
0
Manganese (Mn), % 0
0 to 0.5
Molybdenum (Mo), % 0
8.0 to 10
Nickel (Ni), % 0
58 to 68.9
Niobium (Nb), % 0
3.2 to 4.2
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 0
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0
0 to 0.4
Zinc (Zn), % 4.8 to 6.2
0
Zirconium (Zr), % 0.45 to 1.0
0
Residuals, % 0 to 0.3
0