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AZ81A Magnesium vs. S15700 Stainless Steel

AZ81A magnesium belongs to the magnesium alloys classification, while S15700 stainless steel belongs to the iron alloys. There are 31 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 AZ81A magnesium and the bottom bar is S15700 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 55
200 to 460
Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 3.0 to 8.8
1.1 to 29
Fatigue Strength, MPa 78 to 80
370 to 770
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
77
Shear Strength, MPa 91 to 130
770 to 1070
Tensile Strength: Ultimate (UTS), MPa 160 to 240
1180 to 1890
Tensile Strength: Yield (Proof), MPa 84
500 to 1770

Thermal Properties

Latent Heat of Fusion, J/g 350
290
Maximum Temperature: Mechanical, °C 130
870
Melting Completion (Liquidus), °C 600
1440
Melting Onset (Solidus), °C 500
1400
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 84
16
Thermal Expansion, µm/m-K 27
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 65
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 12
15
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 23
3.4
Embodied Energy, MJ/kg 160
47
Embodied Water, L/kg 990
140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.0 to 17
17 to 270
Resilience: Unit (Modulus of Resilience), kJ/m3 77 to 78
640 to 4660
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 70
25
Strength to Weight: Axial, points 26 to 39
42 to 67
Strength to Weight: Bending, points 38 to 50
32 to 43
Thermal Diffusivity, mm2/s 50
4.2
Thermal Shock Resistance, points 9.1 to 14
39 to 63

Alloy Composition


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Aluminum (Al), % 7.0 to 8.1
0.75 to 1.5
Carbon (C), % 0
0 to 0.090
Chromium (Cr), % 0
14 to 16
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0
69.6 to 76.8
Magnesium (Mg), % 89.8 to 92.5
0
Manganese (Mn), % 0.13 to 0.35
0 to 1.0
Molybdenum (Mo), % 0
2.0 to 3.0
Nickel (Ni), % 0 to 0.010
6.5 to 7.7
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), % 0.4 to 1.0
0
Residuals, % 0 to 0.3
0