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EN-MC21120 Magnesium vs. ASTM Grade HT Steel

EN-MC21120 magnesium belongs to the magnesium alloys classification, while ASTM grade HT 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 EN-MC21120 magnesium and the bottom bar is ASTM grade HT steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 63 to 75
150
Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 2.2 to 6.7
4.6
Fatigue Strength, MPa 84 to 96
130
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
76
Tensile Strength: Ultimate (UTS), MPa 200 to 270
500
Tensile Strength: Yield (Proof), MPa 130 to 170
270

Thermal Properties

Latent Heat of Fusion, J/g 350
310
Maximum Temperature: Mechanical, °C 130
1010
Melting Completion (Liquidus), °C 600
1390
Melting Onset (Solidus), °C 490
1340
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 76
12
Thermal Expansion, µm/m-K 26
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 59
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 12
31
Density, g/cm3 1.7
8.0
Embodied Carbon, kg CO2/kg material 22
5.4
Embodied Energy, MJ/kg 160
76
Embodied Water, L/kg 990
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.0 to 15
19
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 320
180
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 69
24
Strength to Weight: Axial, points 31 to 43
18
Strength to Weight: Bending, points 43 to 53
18
Thermal Diffusivity, mm2/s 44
3.2
Thermal Shock Resistance, points 11 to 16
12

Alloy Composition

Aluminum (Al), % 8.3 to 9.7
0
Carbon (C), % 0
0.35 to 0.75
Chromium (Cr), % 0
15 to 19
Copper (Cu), % 0 to 0.030
0
Iron (Fe), % 0 to 0.0050
38.2 to 51.7
Magnesium (Mg), % 88.6 to 91.3
0
Manganese (Mn), % 0.1 to 0.5
0 to 2.0
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0 to 0.0020
33 to 37
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.2
0 to 2.5
Sulfur (S), % 0
0 to 0.040
Zinc (Zn), % 0.35 to 1.0
0
Residuals, % 0 to 0.010
0