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EN-MC65120 Magnesium vs. N08800 Stainless Steel

EN-MC65120 magnesium belongs to the magnesium alloys classification, while N08800 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 EN-MC65120 magnesium and the bottom bar is N08800 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
200
Elongation at Break, % 3.1
4.5 to 34
Fatigue Strength, MPa 80
150 to 390
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
77
Shear Strength, MPa 92
340 to 580
Tensile Strength: Ultimate (UTS), MPa 160
500 to 1000
Tensile Strength: Yield (Proof), MPa 110
190 to 830

Thermal Properties

Latent Heat of Fusion, J/g 330
300
Maximum Temperature: Mechanical, °C 180
1100
Melting Completion (Liquidus), °C 590
1390
Melting Onset (Solidus), °C 520
1360
Specific Heat Capacity, J/kg-K 970
480
Thermal Conductivity, W/m-K 100
12
Thermal Expansion, µm/m-K 26
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 120
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 25
30
Density, g/cm3 1.9
8.0
Embodied Carbon, kg CO2/kg material 25
5.3
Embodied Energy, MJ/kg 190
76
Embodied Water, L/kg 930
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.4
42 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 140
96 to 1740
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 62
24
Strength to Weight: Axial, points 23
18 to 35
Strength to Weight: Bending, points 34
18 to 28
Thermal Diffusivity, mm2/s 56
3.0
Thermal Shock Resistance, points 9.8
13 to 25

Alloy Composition


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Aluminum (Al), % 0
0.15 to 0.6
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
19 to 23
Copper (Cu), % 0 to 0.030
0 to 0.75
Iron (Fe), % 0 to 0.010
39.5 to 50.7
Magnesium (Mg), % 91.8 to 95.1
0
Manganese (Mn), % 0 to 0.15
0 to 1.5
Nickel (Ni), % 0 to 0.0050
30 to 35
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.010
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0
0.15 to 0.6
Unspecified Rare Earths, % 2.5 to 4.0
0
Zinc (Zn), % 2.0 to 3.0
0
Zirconium (Zr), % 0.4 to 1.0
0
Residuals, % 0 to 0.010
0