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ISO-WD32250 Magnesium vs. R30556 Alloy

ISO-WD32250 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-WD32250 magnesium and the bottom bar is R30556 alloy.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
210
Elongation at Break, % 4.5 to 8.6
45
Fatigue Strength, MPa 170 to 210
320
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
81
Shear Strength, MPa 180 to 190
550
Tensile Strength: Ultimate (UTS), MPa 310 to 330
780
Tensile Strength: Yield (Proof), MPa 240 to 290
350

Thermal Properties

Latent Heat of Fusion, J/g 340
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 980
450
Thermal Conductivity, W/m-K 130
11
Thermal Expansion, µm/m-K 26
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
1.8
Electrical Conductivity: Equal Weight (Specific), % IACS 130
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 13
70
Density, g/cm3 1.8
8.4
Embodied Carbon, kg CO2/kg material 24
8.7
Embodied Energy, MJ/kg 160
130
Embodied Water, L/kg 950
300

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 26
290
Resilience: Unit (Modulus of Resilience), kJ/m3 630 to 930
290
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 67
23
Strength to Weight: Axial, points 49 to 51
26
Strength to Weight: Bending, points 58 to 60
22
Thermal Diffusivity, mm2/s 72
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), % 94.9 to 97.1
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), % 2.5 to 4.0
0.0010 to 0.1
Zirconium (Zr), % 0.45 to 0.8
0
Residuals, % 0 to 0.3
0