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AZ63A Magnesium vs. S15500 Stainless Steel

AZ63A magnesium belongs to the magnesium alloys classification, while S15500 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (7, 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 AZ63A magnesium and the bottom bar is S15500 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 2.2 to 8.0
6.8 to 16
Fatigue Strength, MPa 76 to 83
350 to 650
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
75
Shear Strength, MPa 110 to 160
540 to 870
Tensile Strength: Ultimate (UTS), MPa 190 to 270
890 to 1490
Tensile Strength: Yield (Proof), MPa 81 to 120
590 to 1310

Thermal Properties

Latent Heat of Fusion, J/g 350
280
Maximum Temperature: Mechanical, °C 120
820
Melting Completion (Liquidus), °C 610
1430
Melting Onset (Solidus), °C 450
1380
Specific Heat Capacity, J/kg-K 980
480
Thermal Conductivity, W/m-K 52 to 65
17
Thermal Expansion, µm/m-K 26
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12 to 15
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 59 to 74
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 12
13
Density, g/cm3 1.8
7.8
Embodied Carbon, kg CO2/kg material 22
2.7
Embodied Energy, MJ/kg 150
39
Embodied Water, L/kg 970
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.7 to 16
98 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 71 to 160
890 to 4460
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 66
25
Strength to Weight: Axial, points 29 to 41
32 to 53
Strength to Weight: Bending, points 40 to 51
26 to 37
Thermal Diffusivity, mm2/s 29 to 37
4.6
Thermal Shock Resistance, points 11 to 16
30 to 50

Alloy Composition

Aluminum (Al), % 5.3 to 6.7
0
Carbon (C), % 0
0 to 0.070
Chromium (Cr), % 0
14 to 15.5
Copper (Cu), % 0 to 0.25
2.5 to 4.5
Iron (Fe), % 0
71.9 to 79.9
Magnesium (Mg), % 88.6 to 92.1
0
Manganese (Mn), % 0.15 to 0.35
0 to 1.0
Nickel (Ni), % 0 to 0.010
3.5 to 5.5
Niobium (Nb), % 0
0.15 to 0.45
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.3
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Zinc (Zn), % 2.5 to 3.5
0
Residuals, % 0 to 0.3
0