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EN 1.4606 Stainless Steel vs. ZC63A Magnesium

EN 1.4606 stainless steel belongs to the iron alloys classification, while ZC63A magnesium belongs to the magnesium alloys. There are 30 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 EN 1.4606 stainless steel and the bottom bar is ZC63A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
48
Elongation at Break, % 23 to 39
3.3
Fatigue Strength, MPa 240 to 420
94
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 75
19
Shear Strength, MPa 410 to 640
130
Tensile Strength: Ultimate (UTS), MPa 600 to 1020
220
Tensile Strength: Yield (Proof), MPa 280 to 630
130

Thermal Properties

Latent Heat of Fusion, J/g 300
330
Maximum Temperature: Mechanical, °C 910
98
Melting Completion (Liquidus), °C 1430
550
Melting Onset (Solidus), °C 1380
470
Specific Heat Capacity, J/kg-K 470
950
Thermal Conductivity, W/m-K 14
120
Thermal Expansion, µm/m-K 11
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.9
32
Electrical Conductivity: Equal Weight (Specific), % IACS 2.2
140

Otherwise Unclassified Properties

Base Metal Price, % relative 26
13
Density, g/cm3 7.9
2.1
Embodied Carbon, kg CO2/kg material 6.0
22
Embodied Energy, MJ/kg 87
150
Embodied Water, L/kg 170
920

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 190 to 200
6.3
Resilience: Unit (Modulus of Resilience), kJ/m3 200 to 1010
190
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
58
Strength to Weight: Axial, points 21 to 36
29
Strength to Weight: Bending, points 20 to 28
38
Thermal Diffusivity, mm2/s 3.7
58
Thermal Shock Resistance, points 21 to 35
12

Alloy Composition

Aluminum (Al), % 0 to 0.35
0
Boron (B), % 0.0010 to 0.010
0
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 13 to 16
0
Copper (Cu), % 0
2.4 to 3.0
Iron (Fe), % 49.2 to 59
0
Magnesium (Mg), % 0
89.2 to 91.9
Manganese (Mn), % 1.0 to 2.0
0.25 to 0.75
Molybdenum (Mo), % 1.0 to 1.5
0
Nickel (Ni), % 24 to 27
0 to 0.010
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 1.0
0 to 0.2
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 1.9 to 2.3
0
Vanadium (V), % 0.1 to 0.5
0
Zinc (Zn), % 0
5.5 to 6.5
Residuals, % 0
0 to 0.3