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EN-MC21110 Magnesium vs. ASTM A369 Grade FP92

EN-MC21110 magnesium belongs to the magnesium alloys classification, while ASTM A369 grade FP92 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-MC21110 magnesium and the bottom bar is ASTM A369 grade FP92.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 58 to 63
210
Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 2.8 to 6.7
19
Fatigue Strength, MPa 75 to 78
330
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
76
Shear Strength, MPa 120 to 160
440
Tensile Strength: Ultimate (UTS), MPa 200 to 270
710
Tensile Strength: Yield (Proof), MPa 100 to 120
490

Thermal Properties

Latent Heat of Fusion, J/g 350
260
Maximum Temperature: Mechanical, °C 130
590
Melting Completion (Liquidus), °C 600
1490
Melting Onset (Solidus), °C 500
1450
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 80
26
Thermal Expansion, µm/m-K 26
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12
9.3
Electrical Conductivity: Equal Weight (Specific), % IACS 61
10

Otherwise Unclassified Properties

Base Metal Price, % relative 12
11
Density, g/cm3 1.7
7.9
Embodied Carbon, kg CO2/kg material 23
2.8
Embodied Energy, MJ/kg 160
40
Embodied Water, L/kg 990
89

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.9 to 14
120
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 150
620
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 69
24
Strength to Weight: Axial, points 33 to 44
25
Strength to Weight: Bending, points 45 to 54
22
Thermal Diffusivity, mm2/s 47
6.9
Thermal Shock Resistance, points 12 to 16
19

Alloy Composition

Aluminum (Al), % 7.0 to 8.7
0 to 0.020
Boron (B), % 0
0.0010 to 0.0060
Carbon (C), % 0
0.070 to 0.13
Chromium (Cr), % 0
8.5 to 9.5
Copper (Cu), % 0 to 0.030
0
Iron (Fe), % 0 to 0.0050
85.8 to 89.1
Magnesium (Mg), % 89.6 to 92.6
0
Manganese (Mn), % 0.1 to 0.35
0.3 to 0.6
Molybdenum (Mo), % 0
0.3 to 0.6
Nickel (Ni), % 0 to 0.0020
0 to 0.4
Niobium (Nb), % 0
0.040 to 0.090
Nitrogen (N), % 0
0.030 to 0.070
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.2
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0
0 to 0.010
Tungsten (W), % 0
1.5 to 2.0
Vanadium (V), % 0
0.15 to 0.25
Zinc (Zn), % 0.35 to 1.0
0
Zirconium (Zr), % 0
0 to 0.010
Residuals, % 0 to 0.010
0