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EN 1.7703 Steel vs. EN-MC21120 Magnesium

EN 1.7703 steel belongs to the iron alloys classification, while EN-MC21120 magnesium belongs to the magnesium alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 1.7703 steel and the bottom bar is EN-MC21120 magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 200 to 210
63 to 75
Elastic (Young's, Tensile) Modulus, GPa 190
46
Elongation at Break, % 20
2.2 to 6.7
Fatigue Strength, MPa 320 to 340
84 to 96
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 74
18
Shear Strength, MPa 420 to 430
110 to 160
Tensile Strength: Ultimate (UTS), MPa 670 to 690
200 to 270
Tensile Strength: Yield (Proof), MPa 460 to 500
130 to 170

Thermal Properties

Latent Heat of Fusion, J/g 250
350
Maximum Temperature: Mechanical, °C 460
130
Melting Completion (Liquidus), °C 1470
600
Melting Onset (Solidus), °C 1430
490
Specific Heat Capacity, J/kg-K 470
990
Thermal Conductivity, W/m-K 39
76
Thermal Expansion, µm/m-K 13
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.6
11
Electrical Conductivity: Equal Weight (Specific), % IACS 8.7
59

Otherwise Unclassified Properties

Base Metal Price, % relative 4.2
12
Density, g/cm3 7.9
1.7
Embodied Carbon, kg CO2/kg material 2.5
22
Embodied Energy, MJ/kg 35
160
Embodied Water, L/kg 61
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120 to 130
5.0 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 570 to 650
180 to 320
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 24
69
Strength to Weight: Axial, points 24
31 to 43
Strength to Weight: Bending, points 22
43 to 53
Thermal Diffusivity, mm2/s 11
44
Thermal Shock Resistance, points 19 to 20
11 to 16

Alloy Composition

Aluminum (Al), % 0
8.3 to 9.7
Carbon (C), % 0.11 to 0.15
0
Chromium (Cr), % 2.0 to 2.5
0
Copper (Cu), % 0 to 0.2
0 to 0.030
Iron (Fe), % 94.6 to 96.4
0 to 0.0050
Magnesium (Mg), % 0
88.6 to 91.3
Manganese (Mn), % 0.3 to 0.6
0.1 to 0.5
Molybdenum (Mo), % 0.9 to 1.1
0
Nickel (Ni), % 0 to 0.25
0 to 0.0020
Niobium (Nb), % 0 to 0.070
0
Nitrogen (N), % 0 to 0.012
0
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 0.1
0 to 0.2
Sulfur (S), % 0 to 0.0050
0
Titanium (Ti), % 0 to 0.030
0
Vanadium (V), % 0.25 to 0.35
0
Zinc (Zn), % 0
0.35 to 1.0
Residuals, % 0
0 to 0.010