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AM100A Magnesium vs. EN 2.4665 Nickel

AM100A magnesium belongs to the magnesium alloys classification, while EN 2.4665 nickel belongs to the nickel alloys. There are 30 material properties with values for both materials. Properties with values for just one material (1, 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 AM100A magnesium and the bottom bar is EN 2.4665 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
210
Elongation at Break, % 1.0 to 6.8
34
Fatigue Strength, MPa 48 to 70
220
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
81
Shear Strength, MPa 90 to 150
520
Tensile Strength: Ultimate (UTS), MPa 160 to 270
790
Tensile Strength: Yield (Proof), MPa 78 to 140
300

Thermal Properties

Latent Heat of Fusion, J/g 350
320
Maximum Temperature: Mechanical, °C 140
990
Melting Completion (Liquidus), °C 590
1460
Melting Onset (Solidus), °C 460
1410
Specific Heat Capacity, J/kg-K 990
450
Thermal Conductivity, W/m-K 73
12
Thermal Expansion, µm/m-K 25
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 59
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 12
55
Density, g/cm3 1.7
8.4
Embodied Carbon, kg CO2/kg material 22
9.2
Embodied Energy, MJ/kg 160
130
Embodied Water, L/kg 1000
270

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.3 to 15
210
Resilience: Unit (Modulus of Resilience), kJ/m3 66 to 210
220
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 70
23
Strength to Weight: Axial, points 25 to 44
26
Strength to Weight: Bending, points 38 to 54
22
Thermal Diffusivity, mm2/s 43
3.2
Thermal Shock Resistance, points 9.7 to 17
20

Alloy Composition

Aluminum (Al), % 9.3 to 10.7
0 to 0.5
Boron (B), % 0
0 to 0.010
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0
20.5 to 23
Cobalt (Co), % 0
0.5 to 2.5
Copper (Cu), % 0 to 0.1
0 to 0.5
Iron (Fe), % 0
17 to 20
Magnesium (Mg), % 87.9 to 90.6
0
Manganese (Mn), % 0.1 to 0.35
0 to 1.0
Molybdenum (Mo), % 0
8.0 to 10
Nickel (Ni), % 0 to 0.010
40.3 to 53.8
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.3
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Tungsten (W), % 0
0.2 to 1.0
Zinc (Zn), % 0 to 0.3
0
Residuals, % 0 to 0.3
0