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AZ92A Magnesium vs. EN 1.4542 Stainless Steel

AZ92A magnesium belongs to the magnesium alloys classification, while EN 1.4542 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 EN 1.4542 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 47
190
Elongation at Break, % 2.1 to 6.8
5.7 to 20
Fatigue Strength, MPa 76 to 90
370 to 640
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
76
Shear Strength, MPa 97 to 160
550 to 860
Tensile Strength: Ultimate (UTS), MPa 170 to 270
880 to 1470
Tensile Strength: Yield (Proof), MPa 83 to 140
580 to 1300

Thermal Properties

Latent Heat of Fusion, J/g 350
280
Maximum Temperature: Mechanical, °C 130
860
Melting Completion (Liquidus), °C 590
1430
Melting Onset (Solidus), °C 440
1380
Specific Heat Capacity, J/kg-K 980
470
Thermal Conductivity, W/m-K 44 to 58
16
Thermal Expansion, µm/m-K 26
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11 to 12
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 53 to 62
2.8

Otherwise Unclassified Properties

Base Metal Price, % relative 12
13
Density, g/cm3 1.8
7.8
Embodied Carbon, kg CO2/kg material 22
2.7
Embodied Energy, MJ/kg 160
39
Embodied Water, L/kg 980
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.0 to 14
62 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 73 to 220
880 to 4360
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 67
25
Strength to Weight: Axial, points 26 to 41
31 to 52
Strength to Weight: Bending, points 38 to 51
26 to 37
Thermal Diffusivity, mm2/s 25 to 33
4.3
Thermal Shock Resistance, points 10 to 16
29 to 49

Alloy Composition

Aluminum (Al), % 8.3 to 9.7
0
Carbon (C), % 0
0 to 0.070
Chromium (Cr), % 0
15 to 17
Copper (Cu), % 0 to 0.25
3.0 to 5.0
Iron (Fe), % 0
69.6 to 79
Magnesium (Mg), % 86.7 to 90
0
Manganese (Mn), % 0.1 to 0.35
0 to 1.5
Molybdenum (Mo), % 0
0 to 0.6
Nickel (Ni), % 0 to 0.010
3.0 to 5.0
Niobium (Nb), % 0
0 to 0.45
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.3
0 to 0.7
Sulfur (S), % 0
0 to 0.015
Zinc (Zn), % 1.6 to 2.4
0
Residuals, % 0 to 0.3
0