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ISO-WD21150 Magnesium vs. EN 1.4945 Stainless Steel

ISO-WD21150 magnesium belongs to the magnesium alloys classification, while EN 1.4945 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 1.4945 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
200
Elongation at Break, % 5.7 to 11
19 to 34
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
77
Shear Strength, MPa 150 to 170
430 to 460
Tensile Strength: Ultimate (UTS), MPa 240 to 290
640 to 740
Tensile Strength: Yield (Proof), MPa 120 to 200
290 to 550

Thermal Properties

Latent Heat of Fusion, J/g 350
290
Maximum Temperature: Mechanical, °C 110
920
Melting Completion (Liquidus), °C 600
1490
Melting Onset (Solidus), °C 550
1440
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 100
14
Thermal Expansion, µm/m-K 27
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 19
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 100
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 12
30
Density, g/cm3 1.7
8.1
Embodied Carbon, kg CO2/kg material 23
5.0
Embodied Energy, MJ/kg 160
73
Embodied Water, L/kg 980
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 24
130 to 180
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 460
210 to 760
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 70
24
Strength to Weight: Axial, points 40 to 48
22 to 25
Strength to Weight: Bending, points 52 to 58
20 to 22
Thermal Diffusivity, mm2/s 60
3.7
Thermal Shock Resistance, points 15 to 17
14 to 16

Alloy Composition

Aluminum (Al), % 2.4 to 3.6
0
Carbon (C), % 0
0.040 to 0.1
Chromium (Cr), % 0
15.5 to 17.5
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.0050
57.9 to 65.7
Magnesium (Mg), % 94 to 97
0
Manganese (Mn), % 0.15 to 0.4
0 to 1.5
Nickel (Ni), % 0 to 0.0050
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 0.1
0.3 to 0.6
Sulfur (S), % 0
0 to 0.015
Tungsten (W), % 0
2.5 to 3.5
Zinc (Zn), % 0.5 to 1.5
0
Residuals, % 0 to 0.3
0