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WE54A Magnesium vs. Nickel 718

WE54A magnesium belongs to the magnesium alloys classification, while nickel 718 belongs to the nickel alloys. There are 30 material properties with values for both materials. Properties with values for just one material (6, 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 WE54A magnesium and the bottom bar is nickel 718.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 44
190
Elongation at Break, % 4.3 to 5.6
12 to 50
Fatigue Strength, MPa 98 to 130
460 to 760
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 17
75
Shear Strength, MPa 150 to 170
660 to 950
Tensile Strength: Ultimate (UTS), MPa 270 to 300
930 to 1530
Tensile Strength: Yield (Proof), MPa 180
510 to 1330

Thermal Properties

Latent Heat of Fusion, J/g 330
310
Maximum Temperature: Mechanical, °C 170
980
Melting Completion (Liquidus), °C 640
1340
Melting Onset (Solidus), °C 570
1260
Specific Heat Capacity, J/kg-K 960
450
Thermal Conductivity, W/m-K 52
11
Thermal Expansion, µm/m-K 25
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 47
1.5

Otherwise Unclassified Properties

Base Metal Price, % relative 34
75
Density, g/cm3 1.9
8.3
Embodied Carbon, kg CO2/kg material 29
13
Embodied Energy, MJ/kg 260
190
Embodied Water, L/kg 900
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 14
140 to 390
Resilience: Unit (Modulus of Resilience), kJ/m3 360 to 380
660 to 4560
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 62
23
Strength to Weight: Axial, points 39 to 43
31 to 51
Strength to Weight: Bending, points 49 to 51
25 to 35
Thermal Diffusivity, mm2/s 28
3.0
Thermal Shock Resistance, points 18 to 19
27 to 44

Alloy Composition


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Aluminum (Al), % 0
0.2 to 0.8
Boron (B), % 0
0 to 0.0060
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
17 to 21
Cobalt (Co), % 0
0 to 1.0
Copper (Cu), % 0 to 0.030
0 to 0.3
Iron (Fe), % 0 to 0.010
11.1 to 24.6
Lithium (Li), % 0 to 0.2
0
Magnesium (Mg), % 88.7 to 93.4
0
Manganese (Mn), % 0 to 0.030
0 to 0.35
Molybdenum (Mo), % 0
2.8 to 3.3
Nickel (Ni), % 0 to 0.0050
50 to 55
Niobium (Nb), % 0
4.8 to 5.5
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 0 to 0.010
0 to 0.35
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0
0.65 to 1.2
Unspecified Rare Earths, % 1.5 to 4.0
0
Yttrium (Y), % 4.8 to 5.5
0
Zinc (Zn), % 0 to 0.2
0
Zirconium (Zr), % 0.4 to 1.0
0
Residuals, % 0 to 0.3
0