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ISO-WD32350 Magnesium vs. S15500 Stainless Steel

ISO-WD32350 magnesium belongs to the magnesium alloys classification, while S15500 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (6, 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 S15500 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 5.7 to 10
6.8 to 16
Fatigue Strength, MPa 120 to 130
350 to 650
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
75
Shear Strength, MPa 150 to 170
540 to 870
Tensile Strength: Ultimate (UTS), MPa 250 to 290
890 to 1490
Tensile Strength: Yield (Proof), MPa 140 to 180
590 to 1310

Thermal Properties

Latent Heat of Fusion, J/g 340
280
Maximum Temperature: Mechanical, °C 95
820
Melting Completion (Liquidus), °C 600
1430
Melting Onset (Solidus), °C 560
1380
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
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 130
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 12
13
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 23
2.7
Embodied Energy, MJ/kg 160
39
Embodied Water, L/kg 960
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 23
98 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 380
890 to 4460
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 68
25
Strength to Weight: Axial, points 39 to 46
32 to 53
Strength to Weight: Bending, points 50 to 55
26 to 37
Thermal Diffusivity, mm2/s 73
4.6
Thermal Shock Resistance, points 16 to 18
30 to 50

Alloy Composition

Aluminum (Al), % 0 to 0.1
0
Carbon (C), % 0
0 to 0.070
Chromium (Cr), % 0
14 to 15.5
Copper (Cu), % 0 to 0.1
2.5 to 4.5
Iron (Fe), % 0 to 0.060
71.9 to 79.9
Magnesium (Mg), % 95.7 to 97.7
0
Manganese (Mn), % 0.6 to 1.3
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 0.1
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Zinc (Zn), % 1.8 to 2.3
0
Residuals, % 0 to 0.3
0