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ASTM Grade HT Steel vs. EN-MC21120 Magnesium

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

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition


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