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AZ63A Magnesium vs. EN 1.4945 Stainless Steel

AZ63A magnesium belongs to the magnesium alloys classification, while EN 1.4945 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 1.4945 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 2.2 to 8.0
19 to 34
Fatigue Strength, MPa 76 to 83
230 to 350
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
77
Shear Strength, MPa 110 to 160
430 to 460
Tensile Strength: Ultimate (UTS), MPa 190 to 270
640 to 740
Tensile Strength: Yield (Proof), MPa 81 to 120
290 to 550

Thermal Properties

Latent Heat of Fusion, J/g 350
290
Maximum Temperature: Mechanical, °C 120
920
Melting Completion (Liquidus), °C 610
1490
Melting Onset (Solidus), °C 450
1440
Specific Heat Capacity, J/kg-K 980
470
Thermal Conductivity, W/m-K 52 to 65
14
Thermal Expansion, µm/m-K 26
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12 to 15
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 59 to 74
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 12
30
Density, g/cm3 1.8
8.1
Embodied Carbon, kg CO2/kg material 22
5.0
Embodied Energy, MJ/kg 150
73
Embodied Water, L/kg 970
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.7 to 16
130 to 180
Resilience: Unit (Modulus of Resilience), kJ/m3 71 to 160
210 to 760
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 66
24
Strength to Weight: Axial, points 29 to 41
22 to 25
Strength to Weight: Bending, points 40 to 51
20 to 22
Thermal Diffusivity, mm2/s 29 to 37
3.7
Thermal Shock Resistance, points 11 to 16
14 to 16

Alloy Composition

Aluminum (Al), % 5.3 to 6.7
0
Carbon (C), % 0
0.040 to 0.1
Chromium (Cr), % 0
15.5 to 17.5
Copper (Cu), % 0 to 0.25
0
Iron (Fe), % 0
57.9 to 65.7
Magnesium (Mg), % 88.6 to 92.1
0
Manganese (Mn), % 0.15 to 0.35
0 to 1.5
Nickel (Ni), % 0 to 0.010
15.5 to 17.5
Niobium (Nb), % 0
0.4 to 1.2
Nitrogen (N), % 0
0.060 to 0.14
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.3
0.3 to 0.6
Sulfur (S), % 0
0 to 0.015
Tungsten (W), % 0
2.5 to 3.5
Zinc (Zn), % 2.5 to 3.5
0
Residuals, % 0 to 0.3
0