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AZ92A Magnesium vs. Nickel 601

AZ92A magnesium belongs to the magnesium alloys classification, while nickel 601 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 AZ92A magnesium and the bottom bar is nickel 601.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 47
200
Elongation at Break, % 2.1 to 6.8
10 to 38
Fatigue Strength, MPa 76 to 90
220 to 380
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
76
Shear Strength, MPa 97 to 160
440 to 530
Tensile Strength: Ultimate (UTS), MPa 170 to 270
660 to 890
Tensile Strength: Yield (Proof), MPa 83 to 140
290 to 800

Thermal Properties

Latent Heat of Fusion, J/g 350
320
Maximum Temperature: Mechanical, °C 130
1100
Melting Completion (Liquidus), °C 590
1410
Melting Onset (Solidus), °C 440
1360
Specific Heat Capacity, J/kg-K 980
470
Thermal Conductivity, W/m-K 44 to 58
11
Thermal Expansion, µm/m-K 26
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11 to 12
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 53 to 62
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 12
49
Density, g/cm3 1.8
8.3
Embodied Carbon, kg CO2/kg material 22
8.0
Embodied Energy, MJ/kg 160
110
Embodied Water, L/kg 980
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.0 to 14
86 to 200
Resilience: Unit (Modulus of Resilience), kJ/m3 73 to 220
210 to 1630
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 67
23
Strength to Weight: Axial, points 26 to 41
22 to 30
Strength to Weight: Bending, points 38 to 51
20 to 25
Thermal Diffusivity, mm2/s 25 to 33
2.8
Thermal Shock Resistance, points 10 to 16
17 to 23

Alloy Composition


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Aluminum (Al), % 8.3 to 9.7
1.0 to 1.7
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
21 to 25
Copper (Cu), % 0 to 0.25
0 to 1.0
Iron (Fe), % 0
7.7 to 20
Magnesium (Mg), % 86.7 to 90
0
Manganese (Mn), % 0.1 to 0.35
0 to 1.0
Nickel (Ni), % 0 to 0.010
58 to 63
Silicon (Si), % 0 to 0.3
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Zinc (Zn), % 1.6 to 2.4
0
Residuals, % 0 to 0.3
0