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AZ80A Magnesium vs. EN 2.4951 Nickel

AZ80A magnesium belongs to the magnesium alloys classification, while EN 2.4951 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 AZ80A magnesium and the bottom bar is EN 2.4951 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 3.9 to 8.5
34
Fatigue Strength, MPa 140 to 170
200
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
76
Shear Strength, MPa 160 to 190
500
Tensile Strength: Ultimate (UTS), MPa 320 to 340
750
Tensile Strength: Yield (Proof), MPa 210 to 230
270

Thermal Properties

Latent Heat of Fusion, J/g 350
320
Maximum Temperature: Mechanical, °C 130
1150
Melting Completion (Liquidus), °C 600
1360
Melting Onset (Solidus), °C 490
1310
Specific Heat Capacity, J/kg-K 990
460
Thermal Conductivity, W/m-K 77
12
Thermal Expansion, µm/m-K 26
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
1.6
Electrical Conductivity: Equal Weight (Specific), % IACS 59
1.7

Otherwise Unclassified Properties

Base Metal Price, % relative 12
60
Density, g/cm3 1.7
8.5
Embodied Carbon, kg CO2/kg material 23
9.3
Embodied Energy, MJ/kg 160
130
Embodied Water, L/kg 990
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 24
200
Resilience: Unit (Modulus of Resilience), kJ/m3 500 to 600
190
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 69
23
Strength to Weight: Axial, points 51 to 55
25
Strength to Weight: Bending, points 60 to 63
22
Thermal Diffusivity, mm2/s 45
3.1
Thermal Shock Resistance, points 19 to 20
23

Alloy Composition

Aluminum (Al), % 7.8 to 9.2
0 to 0.3
Carbon (C), % 0
0.080 to 0.15
Chromium (Cr), % 0
18 to 21
Cobalt (Co), % 0
0 to 5.0
Copper (Cu), % 0 to 0.050
0 to 0.5
Iron (Fe), % 0 to 0.0050
0 to 5.0
Magnesium (Mg), % 89 to 91.9
0
Manganese (Mn), % 0.12 to 0.5
0 to 1.0
Nickel (Ni), % 0 to 0.0050
65.4 to 81.7
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
0.2 to 0.6
Zinc (Zn), % 0.2 to 0.8
0
Residuals, % 0 to 0.3
0