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AM60A Magnesium vs. EN 1.7380 Steel

AM60A magnesium belongs to the magnesium alloys classification, while EN 1.7380 steel belongs to the iron 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 AM60A magnesium and the bottom bar is EN 1.7380 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 62
160 to 170
Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 8.8
19 to 20
Fatigue Strength, MPa 70
200 to 230
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
74
Shear Strength, MPa 130
330 to 350
Tensile Strength: Ultimate (UTS), MPa 230
540 to 550
Tensile Strength: Yield (Proof), MPa 130
290 to 330

Thermal Properties

Latent Heat of Fusion, J/g 350
260
Maximum Temperature: Mechanical, °C 120
460
Melting Completion (Liquidus), °C 620
1470
Melting Onset (Solidus), °C 550
1430
Specific Heat Capacity, J/kg-K 1000
470
Thermal Conductivity, W/m-K 62
39
Thermal Expansion, µm/m-K 26
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 13
7.6
Electrical Conductivity: Equal Weight (Specific), % IACS 69
8.7

Otherwise Unclassified Properties

Base Metal Price, % relative 12
3.8
Density, g/cm3 1.7
7.9
Embodied Carbon, kg CO2/kg material 23
1.8
Embodied Energy, MJ/kg 160
23
Embodied Water, L/kg 990
59

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 17
87 to 98
Resilience: Unit (Modulus of Resilience), kJ/m3 190
230 to 280
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 71
24
Strength to Weight: Axial, points 37
19 to 20
Strength to Weight: Bending, points 49
19
Thermal Diffusivity, mm2/s 37
11
Thermal Shock Resistance, points 14
15 to 16

Alloy Composition

Aluminum (Al), % 5.5 to 6.5
0
Carbon (C), % 0
0.080 to 0.14
Chromium (Cr), % 0
2.0 to 2.5
Copper (Cu), % 0 to 0.35
0 to 0.3
Iron (Fe), % 0
94.6 to 96.6
Magnesium (Mg), % 91.8 to 94.4
0
Manganese (Mn), % 0.13 to 0.6
0.4 to 0.8
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 0 to 0.030
0
Nitrogen (N), % 0
0 to 0.012
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.5
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Zinc (Zn), % 0 to 0.22
0