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ISO-WD32250 Magnesium vs. EN 1.4905 Stainless Steel

ISO-WD32250 magnesium belongs to the magnesium alloys classification, while EN 1.4905 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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-WD32250 magnesium and the bottom bar is EN 1.4905 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 4.5 to 8.6
19
Fatigue Strength, MPa 170 to 210
330
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
76
Shear Strength, MPa 180 to 190
460
Tensile Strength: Ultimate (UTS), MPa 310 to 330
740
Tensile Strength: Yield (Proof), MPa 240 to 290
510

Thermal Properties

Latent Heat of Fusion, J/g 340
270
Maximum Temperature: Mechanical, °C 120
660
Melting Completion (Liquidus), °C 600
1480
Melting Onset (Solidus), °C 550
1440
Specific Heat Capacity, J/kg-K 980
470
Thermal Conductivity, W/m-K 130
26
Thermal Expansion, µm/m-K 26
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
3.7
Electrical Conductivity: Equal Weight (Specific), % IACS 130
4.2

Otherwise Unclassified Properties

Base Metal Price, % relative 13
9.5
Density, g/cm3 1.8
7.9
Embodied Carbon, kg CO2/kg material 24
2.8
Embodied Energy, MJ/kg 160
40
Embodied Water, L/kg 950
90

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 26
130
Resilience: Unit (Modulus of Resilience), kJ/m3 630 to 930
680
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 67
24
Strength to Weight: Axial, points 49 to 51
26
Strength to Weight: Bending, points 58 to 60
23
Thermal Diffusivity, mm2/s 72
7.0
Thermal Shock Resistance, points 19 to 20
25

Alloy Composition

Aluminum (Al), % 0
0 to 0.040
Boron (B), % 0
0.00050 to 0.0050
Carbon (C), % 0
0.090 to 0.13
Chromium (Cr), % 0
8.5 to 9.5
Iron (Fe), % 0
86.2 to 88.8
Magnesium (Mg), % 94.9 to 97.1
0
Manganese (Mn), % 0
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 0
0.1 to 0.4
Niobium (Nb), % 0
0.060 to 0.1
Nitrogen (N), % 0
0.050 to 0.090
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0
0.1 to 0.5
Sulfur (S), % 0
0 to 0.010
Tungsten (W), % 0
0.9 to 1.1
Vanadium (V), % 0
0.18 to 0.25
Zinc (Zn), % 2.5 to 4.0
0
Zirconium (Zr), % 0.45 to 0.8
0
Residuals, % 0 to 0.3
0