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S15500 Stainless Steel vs. WE54A Magnesium

S15500 stainless steel belongs to the iron alloys classification, while WE54A magnesium belongs to the magnesium alloys. There are 31 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 S15500 stainless steel and the bottom bar is WE54A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 290 to 430
85
Elastic (Young's, Tensile) Modulus, GPa 190
44
Elongation at Break, % 6.8 to 16
4.3 to 5.6
Fatigue Strength, MPa 350 to 650
98 to 130
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 75
17
Shear Strength, MPa 540 to 870
150 to 170
Tensile Strength: Ultimate (UTS), MPa 890 to 1490
270 to 300
Tensile Strength: Yield (Proof), MPa 590 to 1310
180

Thermal Properties

Latent Heat of Fusion, J/g 280
330
Maximum Temperature: Mechanical, °C 820
170
Melting Completion (Liquidus), °C 1430
640
Melting Onset (Solidus), °C 1380
570
Specific Heat Capacity, J/kg-K 480
960
Thermal Conductivity, W/m-K 17
52
Thermal Expansion, µm/m-K 11
25

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
10
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
47

Otherwise Unclassified Properties

Base Metal Price, % relative 13
34
Density, g/cm3 7.8
1.9
Embodied Carbon, kg CO2/kg material 2.7
29
Embodied Energy, MJ/kg 39
260
Embodied Water, L/kg 130
900

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 98 to 120
10 to 14
Resilience: Unit (Modulus of Resilience), kJ/m3 890 to 4460
360 to 380
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
62
Strength to Weight: Axial, points 32 to 53
39 to 43
Strength to Weight: Bending, points 26 to 37
49 to 51
Thermal Diffusivity, mm2/s 4.6
28
Thermal Shock Resistance, points 30 to 50
18 to 19

Alloy Composition

Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 14 to 15.5
0
Copper (Cu), % 2.5 to 4.5
0 to 0.030
Iron (Fe), % 71.9 to 79.9
0 to 0.010
Lithium (Li), % 0
0 to 0.2
Magnesium (Mg), % 0
88.7 to 93.4
Manganese (Mn), % 0 to 1.0
0 to 0.030
Nickel (Ni), % 3.5 to 5.5
0 to 0.0050
Niobium (Nb), % 0.15 to 0.45
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0 to 0.010
Sulfur (S), % 0 to 0.030
0
Unspecified Rare Earths, % 0
1.5 to 4.0
Yttrium (Y), % 0
4.8 to 5.5
Zinc (Zn), % 0
0 to 0.2
Zirconium (Zr), % 0
0.4 to 1.0
Residuals, % 0
0 to 0.3