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EN-MC65120 Magnesium vs. ASTM A387 Grade 91 Class 2

EN-MC65120 magnesium belongs to the magnesium alloys classification, while ASTM A387 grade 91 class 2 belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (1, 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-MC65120 magnesium and the bottom bar is ASTM A387 grade 91 class 2.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 55
200
Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 3.1
20
Fatigue Strength, MPa 80
330
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
75
Shear Strength, MPa 92
420
Tensile Strength: Ultimate (UTS), MPa 160
670
Tensile Strength: Yield (Proof), MPa 110
470

Thermal Properties

Latent Heat of Fusion, J/g 330
270
Maximum Temperature: Mechanical, °C 180
600
Melting Completion (Liquidus), °C 590
1460
Melting Onset (Solidus), °C 520
1420
Specific Heat Capacity, J/kg-K 970
470
Thermal Conductivity, W/m-K 100
26
Thermal Expansion, µm/m-K 26
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
8.9
Electrical Conductivity: Equal Weight (Specific), % IACS 120
10

Otherwise Unclassified Properties

Base Metal Price, % relative 25
7.0
Density, g/cm3 1.9
7.8
Embodied Carbon, kg CO2/kg material 25
2.6
Embodied Energy, MJ/kg 190
37
Embodied Water, L/kg 930
88

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.4
120
Resilience: Unit (Modulus of Resilience), kJ/m3 140
580
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 62
25
Strength to Weight: Axial, points 23
24
Strength to Weight: Bending, points 34
22
Thermal Diffusivity, mm2/s 56
6.9
Thermal Shock Resistance, points 9.8
19

Alloy Composition


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Aluminum (Al), % 0
0 to 0.020
Carbon (C), % 0
0.080 to 0.12
Chromium (Cr), % 0
8.0 to 9.5
Copper (Cu), % 0 to 0.030
0
Iron (Fe), % 0 to 0.010
87.3 to 90.3
Magnesium (Mg), % 91.8 to 95.1
0
Manganese (Mn), % 0 to 0.15
0.3 to 0.6
Molybdenum (Mo), % 0
0.85 to 1.1
Nickel (Ni), % 0 to 0.0050
0 to 0.4
Niobium (Nb), % 0
0.060 to 0.1
Nitrogen (N), % 0
0.030 to 0.070
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.010
0.2 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0
0 to 0.010
Unspecified Rare Earths, % 2.5 to 4.0
0
Vanadium (V), % 0
0.18 to 0.25
Zinc (Zn), % 2.0 to 3.0
0
Zirconium (Zr), % 0.4 to 1.0
0 to 0.010
Residuals, % 0 to 0.010
0