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ISO-WD21150 Magnesium vs. EN 1.4980 Stainless Steel

ISO-WD21150 magnesium belongs to the magnesium alloys classification, while EN 1.4980 stainless steel belongs to the iron alloys. There are 29 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 ISO-WD21150 magnesium and the bottom bar is EN 1.4980 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 5.7 to 11
17
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 17
75
Shear Strength, MPa 150 to 170
630
Tensile Strength: Ultimate (UTS), MPa 240 to 290
1030
Tensile Strength: Yield (Proof), MPa 120 to 200
680

Thermal Properties

Latent Heat of Fusion, J/g 350
300
Maximum Temperature: Mechanical, °C 110
920
Melting Completion (Liquidus), °C 600
1430
Melting Onset (Solidus), °C 550
1380
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 100
13
Thermal Expansion, µm/m-K 27
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 19
1.9
Electrical Conductivity: Equal Weight (Specific), % IACS 100
2.1

Otherwise Unclassified Properties

Base Metal Price, % relative 12
26
Density, g/cm3 1.7
7.9
Embodied Carbon, kg CO2/kg material 23
6.0
Embodied Energy, MJ/kg 160
87
Embodied Water, L/kg 980
170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 24
150
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 460
1180
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 70
24
Strength to Weight: Axial, points 40 to 48
36
Strength to Weight: Bending, points 52 to 58
28
Thermal Diffusivity, mm2/s 60
3.5
Thermal Shock Resistance, points 15 to 17
22

Alloy Composition


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Aluminum (Al), % 2.4 to 3.6
0 to 0.35
Boron (B), % 0
0.0030 to 0.010
Carbon (C), % 0
0.030 to 0.080
Chromium (Cr), % 0
13.5 to 16
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.0050
49.2 to 58.5
Magnesium (Mg), % 94 to 97
0
Manganese (Mn), % 0.15 to 0.4
1.0 to 2.0
Molybdenum (Mo), % 0
1.0 to 1.5
Nickel (Ni), % 0 to 0.0050
24 to 27
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.1
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0
1.9 to 2.3
Vanadium (V), % 0
0.1 to 0.5
Zinc (Zn), % 0.5 to 1.5
0
Residuals, % 0 to 0.3
0