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Nickel 718 vs. WE43A Magnesium

Nickel 718 belongs to the nickel alloys classification, while WE43A magnesium belongs to the magnesium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (5, 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 nickel 718 and the bottom bar is WE43A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
44
Elongation at Break, % 12 to 50
5.2 to 5.4
Fatigue Strength, MPa 460 to 760
85 to 120
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 75
17
Shear Strength, MPa 660 to 950
160
Tensile Strength: Ultimate (UTS), MPa 930 to 1530
250 to 270
Tensile Strength: Yield (Proof), MPa 510 to 1330
160 to 170

Thermal Properties

Latent Heat of Fusion, J/g 310
330
Maximum Temperature: Mechanical, °C 980
180
Melting Completion (Liquidus), °C 1340
640
Melting Onset (Solidus), °C 1260
570
Specific Heat Capacity, J/kg-K 450
960
Thermal Conductivity, W/m-K 11
51
Thermal Expansion, µm/m-K 13
27

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
12
Electrical Conductivity: Equal Weight (Specific), % IACS 1.5
55

Otherwise Unclassified Properties

Base Metal Price, % relative 75
34
Density, g/cm3 8.3
1.9
Embodied Carbon, kg CO2/kg material 13
28
Embodied Energy, MJ/kg 190
250
Embodied Water, L/kg 250
910

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140 to 390
12
Resilience: Unit (Modulus of Resilience), kJ/m3 660 to 4560
280 to 310
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 23
61
Strength to Weight: Axial, points 31 to 51
36 to 39
Strength to Weight: Bending, points 25 to 35
46 to 48
Thermal Diffusivity, mm2/s 3.0
28
Thermal Shock Resistance, points 27 to 44
15 to 16

Alloy Composition


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Aluminum (Al), % 0.2 to 0.8
0
Boron (B), % 0 to 0.0060
0
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 17 to 21
0
Cobalt (Co), % 0 to 1.0
0
Copper (Cu), % 0 to 0.3
0 to 0.030
Iron (Fe), % 11.1 to 24.6
0 to 0.010
Lithium (Li), % 0
0 to 0.2
Magnesium (Mg), % 0
89.5 to 93.5
Manganese (Mn), % 0 to 0.35
0 to 0.15
Molybdenum (Mo), % 2.8 to 3.3
0
Nickel (Ni), % 50 to 55
0 to 0.0050
Niobium (Nb), % 4.8 to 5.5
0
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 0.35
0 to 0.010
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0.65 to 1.2
0
Unspecified Rare Earths, % 0
2.4 to 4.4
Yttrium (Y), % 0
3.7 to 4.3
Zinc (Zn), % 0
0 to 0.2
Zirconium (Zr), % 0
0.4 to 1.0
Residuals, % 0
0 to 0.3