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EN 2.4952 Nickel vs. ISO-WD32350 Magnesium

EN 2.4952 nickel belongs to the nickel alloys classification, while ISO-WD32350 magnesium belongs to the magnesium 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 EN 2.4952 nickel and the bottom bar is ISO-WD32350 magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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