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ISO-WD32260 Magnesium vs. R30556 Alloy

ISO-WD32260 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 ISO-WD32260 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 6.0
45
Fatigue Strength, MPa 150 to 190
320
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
81
Shear Strength, MPa 190 to 200
550
Tensile Strength: Ultimate (UTS), MPa 330 to 340
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 520
1330
Specific Heat Capacity, J/kg-K 970
450
Thermal Conductivity, W/m-K 110
11
Thermal Expansion, µm/m-K 27
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
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 19
290
Resilience: Unit (Modulus of Resilience), kJ/m3 560 to 700
290
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 63
23
Strength to Weight: Axial, points 48 to 51
26
Strength to Weight: Bending, points 56 to 58
22
Thermal Diffusivity, mm2/s 63
2.9
Thermal Shock Resistance, points 19 to 20
18

Alloy Composition

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), % 92.7 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 0.8
0
Residuals, % 0 to 0.3
0