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EN-MC65220 Magnesium vs. SAE-AISI 6150 Steel

EN-MC65220 magnesium belongs to the magnesium alloys classification, while SAE-AISI 6150 steel belongs to the iron 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 EN-MC65220 magnesium and the bottom bar is SAE-AISI 6150 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 80
200 to 350
Elastic (Young's, Tensile) Modulus, GPa 44
190
Elongation at Break, % 2.2
15 to 23
Fatigue Strength, MPa 110
300 to 750
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 17
73
Shear Strength, MPa 150
400 to 730
Tensile Strength: Ultimate (UTS), MPa 270
630 to 1200
Tensile Strength: Yield (Proof), MPa 200
420 to 1160

Thermal Properties

Latent Heat of Fusion, J/g 340
250
Maximum Temperature: Mechanical, °C 160
420
Melting Completion (Liquidus), °C 610
1460
Melting Onset (Solidus), °C 550
1410
Specific Heat Capacity, J/kg-K 980
470
Thermal Conductivity, W/m-K 110
46
Thermal Expansion, µm/m-K 26
12 to 13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
7.3
Electrical Conductivity: Equal Weight (Specific), % IACS 120
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 80
2.3
Density, g/cm3 1.9
7.8
Embodied Carbon, kg CO2/kg material 27
2.0
Embodied Energy, MJ/kg 210
28

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.5
130 to 180
Resilience: Unit (Modulus of Resilience), kJ/m3 450
460 to 3590
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 62
24
Strength to Weight: Axial, points 40
22 to 43
Strength to Weight: Bending, points 49
21 to 32
Thermal Diffusivity, mm2/s 61
13
Thermal Shock Resistance, points 17
20 to 38

Alloy Composition


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Carbon (C), % 0
0.48 to 0.53
Chromium (Cr), % 0
0.8 to 1.1
Copper (Cu), % 0.050 to 0.1
0
Iron (Fe), % 0 to 0.010
96.7 to 97.7
Magnesium (Mg), % 93.8 to 96.8
0
Manganese (Mn), % 0 to 0.15
0.7 to 0.9
Nickel (Ni), % 0 to 0.0050
0
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.010
0.15 to 0.35
Silver (Ag), % 1.3 to 1.7
0
Sulfur (S), % 0
0 to 0.040
Unspecified Rare Earths, % 1.5 to 3.0
0
Vanadium (V), % 0
0.15 to 0.3
Zinc (Zn), % 0 to 0.2
0
Zirconium (Zr), % 0.4 to 1.0
0
Residuals, % 0 to 0.010
0