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ISO-WD32350 Magnesium vs. EN 2.4952 Nickel

ISO-WD32350 magnesium belongs to the magnesium alloys classification, while EN 2.4952 nickel belongs to the nickel alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 ISO-WD32350 magnesium and the bottom bar is EN 2.4952 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 5.7 to 10
17
Fatigue Strength, MPa 120 to 130
370
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
74
Shear Strength, MPa 150 to 170
700
Tensile Strength: Ultimate (UTS), MPa 250 to 290
1150
Tensile Strength: Yield (Proof), MPa 140 to 180
670

Thermal Properties

Latent Heat of Fusion, J/g 340
330
Maximum Temperature: Mechanical, °C 95
980
Melting Completion (Liquidus), °C 600
1350
Melting Onset (Solidus), °C 560
1300
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 130
12
Thermal Expansion, µm/m-K 25
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 130
1.5

Otherwise Unclassified Properties

Base Metal Price, % relative 12
55
Density, g/cm3 1.7
8.3
Embodied Carbon, kg CO2/kg material 23
9.8
Embodied Energy, MJ/kg 160
140
Embodied Water, L/kg 960
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 23
170
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 380
1180
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 68
23
Strength to Weight: Axial, points 39 to 46
38
Strength to Weight: Bending, points 50 to 55
29
Thermal Diffusivity, mm2/s 73
3.1
Thermal Shock Resistance, points 16 to 18
33

Alloy Composition

Aluminum (Al), % 0 to 0.1
1.0 to 1.8
Boron (B), % 0
0 to 0.0080
Carbon (C), % 0
0.040 to 0.1
Chromium (Cr), % 0
18 to 21
Cobalt (Co), % 0
0 to 1.0
Copper (Cu), % 0 to 0.1
0 to 0.2
Iron (Fe), % 0 to 0.060
0 to 1.5
Magnesium (Mg), % 95.7 to 97.7
0
Manganese (Mn), % 0.6 to 1.3
0 to 1.0
Nickel (Ni), % 0 to 0.0050
65 to 79.2
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.1
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0
1.8 to 2.7
Zinc (Zn), % 1.8 to 2.3
0
Residuals, % 0 to 0.3
0