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ISO-WD32250 Magnesium vs. ASTM A182 Grade F23

ISO-WD32250 magnesium belongs to the magnesium alloys classification, while ASTM A182 grade F23 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 ISO-WD32250 magnesium and the bottom bar is ASTM A182 grade F23.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 4.5 to 8.6
22
Fatigue Strength, MPa 170 to 210
320
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 17
74
Shear Strength, MPa 180 to 190
360
Tensile Strength: Ultimate (UTS), MPa 310 to 330
570
Tensile Strength: Yield (Proof), MPa 240 to 290
460

Thermal Properties

Latent Heat of Fusion, J/g 340
250
Maximum Temperature: Mechanical, °C 120
450
Melting Completion (Liquidus), °C 600
1500
Melting Onset (Solidus), °C 550
1450
Specific Heat Capacity, J/kg-K 980
470
Thermal Conductivity, W/m-K 130
41
Thermal Expansion, µm/m-K 26
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 130
8.9

Otherwise Unclassified Properties

Base Metal Price, % relative 13
7.0
Density, g/cm3 1.8
8.0
Embodied Carbon, kg CO2/kg material 24
2.5
Embodied Energy, MJ/kg 160
36
Embodied Water, L/kg 950
59

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 26
120
Resilience: Unit (Modulus of Resilience), kJ/m3 630 to 930
550
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 67
24
Strength to Weight: Axial, points 49 to 51
20
Strength to Weight: Bending, points 58 to 60
19
Thermal Diffusivity, mm2/s 72
11
Thermal Shock Resistance, points 19 to 20
17

Alloy Composition

Aluminum (Al), % 0
0 to 0.030
Boron (B), % 0
0.0010 to 0.0060
Carbon (C), % 0
0.040 to 0.1
Chromium (Cr), % 0
1.9 to 2.6
Iron (Fe), % 0
93.2 to 96.2
Magnesium (Mg), % 94.9 to 97.1
0
Manganese (Mn), % 0
0.1 to 0.6
Molybdenum (Mo), % 0
0.050 to 0.3
Nickel (Ni), % 0
0 to 0.4
Niobium (Nb), % 0
0.020 to 0.080
Nitrogen (N), % 0
0 to 0.015
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0
0.0050 to 0.060
Tungsten (W), % 0
1.5 to 1.8
Vanadium (V), % 0
0.2 to 0.3
Zinc (Zn), % 2.5 to 4.0
0
Zirconium (Zr), % 0.45 to 0.8
0
Residuals, % 0 to 0.3
0