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EN-MC65120 Magnesium vs. S15500 Stainless Steel

EN-MC65120 magnesium belongs to the magnesium alloys classification, while S15500 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (5, 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 S15500 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 55
290 to 430
Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 3.1
6.8 to 16
Fatigue Strength, MPa 80
350 to 650
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
75
Shear Strength, MPa 92
540 to 870
Tensile Strength: Ultimate (UTS), MPa 160
890 to 1490
Tensile Strength: Yield (Proof), MPa 110
590 to 1310

Thermal Properties

Latent Heat of Fusion, J/g 330
280
Maximum Temperature: Mechanical, °C 180
820
Melting Completion (Liquidus), °C 590
1430
Melting Onset (Solidus), °C 520
1380
Specific Heat Capacity, J/kg-K 970
480
Thermal Conductivity, W/m-K 100
17
Thermal Expansion, µm/m-K 26
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 120
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 25
13
Density, g/cm3 1.9
7.8
Embodied Carbon, kg CO2/kg material 25
2.7
Embodied Energy, MJ/kg 190
39
Embodied Water, L/kg 930
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.4
98 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 140
890 to 4460
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 62
25
Strength to Weight: Axial, points 23
32 to 53
Strength to Weight: Bending, points 34
26 to 37
Thermal Diffusivity, mm2/s 56
4.6
Thermal Shock Resistance, points 9.8
30 to 50

Alloy Composition

Carbon (C), % 0
0 to 0.070
Chromium (Cr), % 0
14 to 15.5
Copper (Cu), % 0 to 0.030
2.5 to 4.5
Iron (Fe), % 0 to 0.010
71.9 to 79.9
Magnesium (Mg), % 91.8 to 95.1
0
Manganese (Mn), % 0 to 0.15
0 to 1.0
Nickel (Ni), % 0 to 0.0050
3.5 to 5.5
Niobium (Nb), % 0
0.15 to 0.45
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.010
0 to 1.0
Sulfur (S), % 0
0 to 0.030
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