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ZK60A Magnesium vs. R30556 Alloy

ZK60A magnesium belongs to the magnesium alloys classification, while R30556 alloy belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 ZK60A magnesium and the bottom bar is R30556 alloy.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
210
Elongation at Break, % 4.5 to 9.9
45
Fatigue Strength, MPa 150 to 180
320
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
81
Shear Strength, MPa 170 to 190
550
Tensile Strength: Ultimate (UTS), MPa 320 to 330
780
Tensile Strength: Yield (Proof), MPa 230 to 250
350

Thermal Properties

Latent Heat of Fusion, J/g 330
300
Maximum Temperature: Mechanical, °C 120
1100
Melting Completion (Liquidus), °C 600
1420
Melting Onset (Solidus), °C 550
1330
Specific Heat Capacity, J/kg-K 960
450
Thermal Conductivity, W/m-K 120
11
Thermal Expansion, µm/m-K 26
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29 to 30
1.8
Electrical Conductivity: Equal Weight (Specific), % IACS 140
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 13
70
Density, g/cm3 1.9
8.4
Embodied Carbon, kg CO2/kg material 23
8.7
Embodied Energy, MJ/kg 160
130
Embodied Water, L/kg 940
300

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 29
290
Resilience: Unit (Modulus of Resilience), kJ/m3 570 to 690
290
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 63
23
Strength to Weight: Axial, points 47 to 49
26
Strength to Weight: Bending, points 55 to 56
22
Thermal Diffusivity, mm2/s 66
2.9
Thermal Shock Resistance, points 19 to 20
18

Alloy Composition


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Aluminum (Al), % 0
0.1 to 0.5
Boron (B), % 0
0 to 0.020
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0
21 to 23
Cobalt (Co), % 0
16 to 21
Iron (Fe), % 0
20.4 to 38.2
Lanthanum (La), % 0
0.0050 to 0.1
Magnesium (Mg), % 92.5 to 94.8
0
Manganese (Mn), % 0
0.5 to 2.0
Molybdenum (Mo), % 0
2.5 to 4.0
Nickel (Ni), % 0
19 to 22.5
Niobium (Nb), % 0
0 to 0.3
Nitrogen (N), % 0
0.1 to 0.3
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0
0.2 to 0.8
Sulfur (S), % 0
0 to 0.015
Tantalum (Ta), % 0
0.3 to 1.3
Tungsten (W), % 0
2.0 to 3.5
Zinc (Zn), % 4.8 to 6.2
0.0010 to 0.1
Zirconium (Zr), % 0.45 to 1.0
0
Residuals, % 0 to 0.3
0