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AZ63A Magnesium vs. EN 1.4415 Stainless Steel

AZ63A magnesium belongs to the magnesium alloys classification, while EN 1.4415 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 AZ63A magnesium and the bottom bar is EN 1.4415 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 2.2 to 8.0
17 to 20
Fatigue Strength, MPa 76 to 83
470 to 510
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
77
Shear Strength, MPa 110 to 160
520 to 570
Tensile Strength: Ultimate (UTS), MPa 190 to 270
830 to 930
Tensile Strength: Yield (Proof), MPa 81 to 120
730 to 840

Thermal Properties

Latent Heat of Fusion, J/g 350
280
Maximum Temperature: Mechanical, °C 120
790
Melting Completion (Liquidus), °C 610
1460
Melting Onset (Solidus), °C 450
1420
Specific Heat Capacity, J/kg-K 980
470
Thermal Conductivity, W/m-K 52 to 65
19
Thermal Expansion, µm/m-K 26
9.9

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12 to 15
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 59 to 74
2.8

Otherwise Unclassified Properties

Base Metal Price, % relative 12
13
Density, g/cm3 1.8
7.9
Embodied Carbon, kg CO2/kg material 22
3.6
Embodied Energy, MJ/kg 150
51
Embodied Water, L/kg 970
120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.7 to 16
150 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 71 to 160
1350 to 1790
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 66
25
Strength to Weight: Axial, points 29 to 41
29 to 33
Strength to Weight: Bending, points 40 to 51
25 to 27
Thermal Diffusivity, mm2/s 29 to 37
5.1
Thermal Shock Resistance, points 11 to 16
30 to 34

Alloy Composition


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Aluminum (Al), % 5.3 to 6.7
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
11.5 to 13.5
Copper (Cu), % 0 to 0.25
0
Iron (Fe), % 0
75.9 to 82.4
Magnesium (Mg), % 88.6 to 92.1
0
Manganese (Mn), % 0.15 to 0.35
0 to 0.5
Molybdenum (Mo), % 0
1.5 to 2.5
Nickel (Ni), % 0 to 0.010
4.5 to 6.5
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.3
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0
0 to 0.010
Vanadium (V), % 0
0.1 to 0.5
Zinc (Zn), % 2.5 to 3.5
0
Residuals, % 0 to 0.3
0

Comparable Variants