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ISO-WD32350 Magnesium vs. EN 1.4592 Stainless Steel

ISO-WD32350 magnesium belongs to the magnesium alloys classification, while EN 1.4592 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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-WD32350 magnesium and the bottom bar is EN 1.4592 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
210
Elongation at Break, % 5.7 to 10
23
Fatigue Strength, MPa 120 to 130
340
Poisson's Ratio 0.29
0.27
Shear Modulus, GPa 18
82
Shear Strength, MPa 150 to 170
400
Tensile Strength: Ultimate (UTS), MPa 250 to 290
630
Tensile Strength: Yield (Proof), MPa 140 to 180
500

Thermal Properties

Latent Heat of Fusion, J/g 340
310
Maximum Temperature: Mechanical, °C 95
1100
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 560
1410
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 130
17
Thermal Expansion, µm/m-K 25
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
2.6
Electrical Conductivity: Equal Weight (Specific), % IACS 130
3.0

Otherwise Unclassified Properties

Base Metal Price, % relative 12
18
Density, g/cm3 1.7
7.7
Embodied Carbon, kg CO2/kg material 23
3.8
Embodied Energy, MJ/kg 160
52
Embodied Water, L/kg 960
180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 23
130
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 380
610
Stiffness to Weight: Axial, points 15
15
Stiffness to Weight: Bending, points 68
26
Strength to Weight: Axial, points 39 to 46
23
Strength to Weight: Bending, points 50 to 55
21
Thermal Diffusivity, mm2/s 73
4.6
Thermal Shock Resistance, points 16 to 18
20

Alloy Composition

Aluminum (Al), % 0 to 0.1
0
Carbon (C), % 0
0 to 0.025
Chromium (Cr), % 0
28 to 30
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.060
62.6 to 68.4
Magnesium (Mg), % 95.7 to 97.7
0
Manganese (Mn), % 0.6 to 1.3
0 to 1.0
Molybdenum (Mo), % 0
3.5 to 4.5
Nickel (Ni), % 0 to 0.0050
0
Nitrogen (N), % 0
0 to 0.045
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.1
0 to 1.0
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0
0.15 to 0.8
Zinc (Zn), % 1.8 to 2.3
0
Residuals, % 0 to 0.3
0