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ZK61A Magnesium vs. EN 1.6368 Steel

ZK61A magnesium belongs to the magnesium alloys classification, while EN 1.6368 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 ZK61A magnesium and the bottom bar is EN 1.6368 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 5.8 to 7.1
18
Fatigue Strength, MPa 120 to 140
310 to 330
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
73
Shear Strength, MPa 170 to 180
410 to 430
Tensile Strength: Ultimate (UTS), MPa 290 to 310
660 to 690
Tensile Strength: Yield (Proof), MPa 180 to 200
460 to 490

Thermal Properties

Latent Heat of Fusion, J/g 330
250
Maximum Temperature: Mechanical, °C 120
410
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 530
1420
Specific Heat Capacity, J/kg-K 960
470
Thermal Conductivity, W/m-K 120
40
Thermal Expansion, µm/m-K 27
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
7.5
Electrical Conductivity: Equal Weight (Specific), % IACS 130
8.6

Otherwise Unclassified Properties

Base Metal Price, % relative 13
3.4
Density, g/cm3 1.9
7.9
Embodied Carbon, kg CO2/kg material 23
1.7
Embodied Energy, MJ/kg 160
22
Embodied Water, L/kg 940
53

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 19
110
Resilience: Unit (Modulus of Resilience), kJ/m3 370 to 420
580 to 650
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 62
24
Strength to Weight: Axial, points 42 to 45
23 to 24
Strength to Weight: Bending, points 50 to 53
21 to 22
Thermal Diffusivity, mm2/s 65
11
Thermal Shock Resistance, points 17 to 18
20

Alloy Composition

Aluminum (Al), % 0
0.015 to 0.040
Carbon (C), % 0
0 to 0.17
Chromium (Cr), % 0
0 to 0.3
Copper (Cu), % 0 to 0.1
0.5 to 0.8
Iron (Fe), % 0
95.1 to 97.2
Magnesium (Mg), % 92.1 to 93.9
0
Manganese (Mn), % 0
0.8 to 1.2
Molybdenum (Mo), % 0
0.25 to 0.5
Nickel (Ni), % 0 to 0.010
1.0 to 1.3
Niobium (Nb), % 0
0.015 to 0.045
Nitrogen (N), % 0
0 to 0.020
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0
0.25 to 0.5
Sulfur (S), % 0
0 to 0.010
Zinc (Zn), % 5.5 to 6.5
0
Zirconium (Zr), % 0.6 to 1.0
0
Residuals, % 0 to 0.3
0