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WE54A Magnesium vs. Monel K-500

WE54A magnesium belongs to the magnesium alloys classification, while Monel K-500 belongs to the nickel alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 Monel K-500.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 44
160
Elongation at Break, % 4.3 to 5.6
25 to 36
Fatigue Strength, MPa 98 to 130
260 to 560
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 17
61
Shear Strength, MPa 150 to 170
430 to 700
Tensile Strength: Ultimate (UTS), MPa 270 to 300
640 to 1100
Tensile Strength: Yield (Proof), MPa 180
310 to 880

Thermal Properties

Latent Heat of Fusion, J/g 330
270
Maximum Temperature: Mechanical, °C 170
900
Melting Completion (Liquidus), °C 640
1350
Melting Onset (Solidus), °C 570
1320
Specific Heat Capacity, J/kg-K 960
440
Thermal Conductivity, W/m-K 52
18
Thermal Expansion, µm/m-K 25
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
3.1
Electrical Conductivity: Equal Weight (Specific), % IACS 47
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 34
50
Density, g/cm3 1.9
8.7
Embodied Carbon, kg CO2/kg material 29
8.1
Embodied Energy, MJ/kg 260
120
Embodied Water, L/kg 900
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 14
180 to 260
Resilience: Unit (Modulus of Resilience), kJ/m3 360 to 380
300 to 2420
Stiffness to Weight: Axial, points 13
10
Stiffness to Weight: Bending, points 62
21
Strength to Weight: Axial, points 39 to 43
21 to 35
Strength to Weight: Bending, points 49 to 51
19 to 27
Thermal Diffusivity, mm2/s 28
4.8
Thermal Shock Resistance, points 18 to 19
21 to 36

Alloy Composition


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Aluminum (Al), % 0
2.3 to 3.2
Carbon (C), % 0
0 to 0.18
Copper (Cu), % 0 to 0.030
27 to 33
Iron (Fe), % 0 to 0.010
0 to 2.0
Lithium (Li), % 0 to 0.2
0
Magnesium (Mg), % 88.7 to 93.4
0
Manganese (Mn), % 0 to 0.030
0 to 1.5
Nickel (Ni), % 0 to 0.0050
63 to 70.4
Silicon (Si), % 0 to 0.010
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0
0.35 to 0.85
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