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AM100A Magnesium vs. N08320 Stainless Steel

AM100A magnesium belongs to the magnesium alloys classification, while N08320 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (5, 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 AM100A magnesium and the bottom bar is N08320 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 1.0 to 6.8
40
Fatigue Strength, MPa 48 to 70
190
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
78
Shear Strength, MPa 90 to 150
400
Tensile Strength: Ultimate (UTS), MPa 160 to 270
580
Tensile Strength: Yield (Proof), MPa 78 to 140
220

Thermal Properties

Latent Heat of Fusion, J/g 350
300
Maximum Temperature: Mechanical, °C 140
1100
Melting Completion (Liquidus), °C 590
1400
Melting Onset (Solidus), °C 460
1350
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 73
12
Thermal Expansion, µm/m-K 25
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 59
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 12
28
Density, g/cm3 1.7
8.0
Embodied Carbon, kg CO2/kg material 22
4.9
Embodied Energy, MJ/kg 160
69
Embodied Water, L/kg 1000
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.3 to 15
180
Resilience: Unit (Modulus of Resilience), kJ/m3 66 to 210
120
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 70
24
Strength to Weight: Axial, points 25 to 44
20
Strength to Weight: Bending, points 38 to 54
20
Thermal Diffusivity, mm2/s 43
3.3
Thermal Shock Resistance, points 9.7 to 17
13

Alloy Composition


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Aluminum (Al), % 9.3 to 10.7
0
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0
21 to 23
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0
40.4 to 50
Magnesium (Mg), % 87.9 to 90.6
0
Manganese (Mn), % 0.1 to 0.35
0 to 2.5
Nickel (Ni), % 0 to 0.010
25 to 27
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 to 0.3
0
Residuals, % 0 to 0.3
0