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ASTM A182 Grade F122 vs. ISO-WD32260 Magnesium

ASTM A182 grade F122 belongs to the iron alloys classification, while ISO-WD32260 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 A182 grade F122 and the bottom bar is ISO-WD32260 magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
46
Elongation at Break, % 23
4.5 to 6.0
Fatigue Strength, MPa 320
150 to 190
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 76
18
Shear Strength, MPa 450
190 to 200
Tensile Strength: Ultimate (UTS), MPa 710
330 to 340
Tensile Strength: Yield (Proof), MPa 450
230 to 250

Thermal Properties

Latent Heat of Fusion, J/g 270
330
Maximum Temperature: Mechanical, °C 600
120
Melting Completion (Liquidus), °C 1490
600
Melting Onset (Solidus), °C 1440
520
Specific Heat Capacity, J/kg-K 470
970
Thermal Conductivity, W/m-K 24
110
Thermal Expansion, µm/m-K 13
27

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
28
Electrical Conductivity: Equal Weight (Specific), % IACS 12
140

Otherwise Unclassified Properties

Base Metal Price, % relative 12
13
Density, g/cm3 8.0
1.9
Embodied Carbon, kg CO2/kg material 3.0
23
Embodied Energy, MJ/kg 44
160
Embodied Water, L/kg 100
940

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
14 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 520
560 to 700
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
63
Strength to Weight: Axial, points 25
48 to 51
Strength to Weight: Bending, points 22
56 to 58
Thermal Diffusivity, mm2/s 6.4
63
Thermal Shock Resistance, points 19
19 to 20

Alloy Composition

Aluminum (Al), % 0 to 0.020
0
Boron (B), % 0 to 0.0050
0
Carbon (C), % 0.070 to 0.14
0
Chromium (Cr), % 10 to 11.5
0
Copper (Cu), % 0.3 to 1.7
0
Iron (Fe), % 81.3 to 87.7
0
Magnesium (Mg), % 0
92.7 to 94.8
Manganese (Mn), % 0 to 0.7
0
Molybdenum (Mo), % 0.25 to 0.6
0
Nickel (Ni), % 0 to 0.5
0
Niobium (Nb), % 0.040 to 0.1
0
Nitrogen (N), % 0.040 to 0.1
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.5
0
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 0.010
0
Tungsten (W), % 1.5 to 2.5
0
Vanadium (V), % 0.15 to 0.3
0
Zinc (Zn), % 0
4.8 to 6.2
Zirconium (Zr), % 0 to 0.010
0.45 to 0.8
Residuals, % 0
0 to 0.3