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ASTM A182 Grade F122 vs. ZK61A Magnesium

ASTM A182 grade F122 belongs to the iron alloys classification, while ZK61A magnesium belongs to the magnesium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 ZK61A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
46
Elongation at Break, % 23
5.8 to 7.1
Fatigue Strength, MPa 320
120 to 140
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 76
18
Shear Strength, MPa 450
170 to 180
Tensile Strength: Ultimate (UTS), MPa 710
290 to 310
Tensile Strength: Yield (Proof), MPa 450
180 to 200

Thermal Properties

Latent Heat of Fusion, J/g 270
330
Maximum Temperature: Mechanical, °C 600
120
Melting Completion (Liquidus), °C 1490
640
Melting Onset (Solidus), °C 1440
530
Specific Heat Capacity, J/kg-K 470
960
Thermal Conductivity, W/m-K 24
120
Thermal Expansion, µm/m-K 13
27

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
29
Electrical Conductivity: Equal Weight (Specific), % IACS 12
130

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
15 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 520
370 to 420
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
62
Strength to Weight: Axial, points 25
42 to 45
Strength to Weight: Bending, points 22
50 to 53
Thermal Diffusivity, mm2/s 6.4
65
Thermal Shock Resistance, points 19
17 to 18

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 to 0.1
Iron (Fe), % 81.3 to 87.7
0
Magnesium (Mg), % 0
92.1 to 93.9
Manganese (Mn), % 0 to 0.7
0
Molybdenum (Mo), % 0.25 to 0.6
0
Nickel (Ni), % 0 to 0.5
0 to 0.010
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
5.5 to 6.5
Zirconium (Zr), % 0 to 0.010
0.6 to 1.0
Residuals, % 0
0 to 0.3