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Nickel 625 vs. WE54A Magnesium

Nickel 625 belongs to the nickel alloys classification, while WE54A magnesium belongs to the magnesium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 625 and the bottom bar is WE54A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
44
Elongation at Break, % 33 to 34
4.3 to 5.6
Fatigue Strength, MPa 240 to 320
98 to 130
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 79
17
Shear Strength, MPa 530 to 600
150 to 170
Tensile Strength: Ultimate (UTS), MPa 790 to 910
270 to 300
Tensile Strength: Yield (Proof), MPa 320 to 450
180

Thermal Properties

Latent Heat of Fusion, J/g 330
330
Maximum Temperature: Mechanical, °C 980
170
Melting Completion (Liquidus), °C 1350
640
Melting Onset (Solidus), °C 1290
570
Specific Heat Capacity, J/kg-K 440
960
Thermal Conductivity, W/m-K 11
52
Thermal Expansion, µm/m-K 13
25

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.3
10
Electrical Conductivity: Equal Weight (Specific), % IACS 1.4
47

Otherwise Unclassified Properties

Base Metal Price, % relative 80
34
Density, g/cm3 8.6
1.9
Embodied Carbon, kg CO2/kg material 14
29
Embodied Energy, MJ/kg 190
260
Embodied Water, L/kg 290
900

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 220 to 250
10 to 14
Resilience: Unit (Modulus of Resilience), kJ/m3 260 to 490
360 to 380
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 23
62
Strength to Weight: Axial, points 26 to 29
39 to 43
Strength to Weight: Bending, points 22 to 24
49 to 51
Thermal Diffusivity, mm2/s 2.9
28
Thermal Shock Resistance, points 22 to 25
18 to 19

Alloy Composition

Aluminum (Al), % 0 to 0.4
0
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 20 to 23
0
Cobalt (Co), % 0 to 1.0
0
Copper (Cu), % 0
0 to 0.030
Iron (Fe), % 0 to 5.0
0 to 0.010
Lithium (Li), % 0
0 to 0.2
Magnesium (Mg), % 0
88.7 to 93.4
Manganese (Mn), % 0 to 0.5
0 to 0.030
Molybdenum (Mo), % 8.0 to 10
0
Nickel (Ni), % 58 to 68.9
0 to 0.0050
Niobium (Nb), % 3.2 to 4.2
0
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 0.5
0 to 0.010
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0 to 0.4
0
Unspecified Rare Earths, % 0
1.5 to 4.0
Yttrium (Y), % 0
4.8 to 5.5
Zinc (Zn), % 0
0 to 0.2
Zirconium (Zr), % 0
0.4 to 1.0
Residuals, % 0
0 to 0.3