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AZ80A Magnesium vs. N08904 Stainless Steel

AZ80A magnesium belongs to the magnesium alloys classification, while N08904 stainless steel belongs to the iron alloys. There are 30 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 AZ80A magnesium and the bottom bar is N08904 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 3.9 to 8.5
38
Fatigue Strength, MPa 140 to 170
200
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
79
Shear Strength, MPa 160 to 190
370
Tensile Strength: Ultimate (UTS), MPa 320 to 340
540
Tensile Strength: Yield (Proof), MPa 210 to 230
240

Thermal Properties

Latent Heat of Fusion, J/g 350
300
Maximum Temperature: Mechanical, °C 130
1100
Melting Completion (Liquidus), °C 600
1440
Melting Onset (Solidus), °C 490
1390
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 77
12
Thermal Expansion, µm/m-K 26
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 59
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 12
32
Density, g/cm3 1.7
8.1
Embodied Carbon, kg CO2/kg material 23
5.8
Embodied Energy, MJ/kg 160
79
Embodied Water, L/kg 990
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 24
170
Resilience: Unit (Modulus of Resilience), kJ/m3 500 to 600
150
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 69
24
Strength to Weight: Axial, points 51 to 55
19
Strength to Weight: Bending, points 60 to 63
18
Thermal Diffusivity, mm2/s 45
3.1
Thermal Shock Resistance, points 19 to 20
12

Alloy Composition

Aluminum (Al), % 7.8 to 9.2
0
Carbon (C), % 0
0 to 0.020
Chromium (Cr), % 0
19 to 23
Copper (Cu), % 0 to 0.050
1.0 to 2.0
Iron (Fe), % 0 to 0.0050
38.8 to 53
Magnesium (Mg), % 89 to 91.9
0
Manganese (Mn), % 0.12 to 0.5
0 to 2.0
Molybdenum (Mo), % 0
4.0 to 5.0
Nickel (Ni), % 0 to 0.0050
23 to 28
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.1
0 to 1.0
Sulfur (S), % 0
0 to 0.035
Zinc (Zn), % 0.2 to 0.8
0
Residuals, % 0 to 0.3
0