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AM100A Magnesium vs. EN 1.4107 Stainless Steel

AM100A magnesium belongs to the magnesium alloys classification, while EN 1.4107 stainless steel belongs to the iron alloys. There are 29 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 EN 1.4107 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 1.0 to 6.8
18 to 21
Fatigue Strength, MPa 48 to 70
260 to 350
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
76
Tensile Strength: Ultimate (UTS), MPa 160 to 270
620 to 700
Tensile Strength: Yield (Proof), MPa 78 to 140
400 to 570

Thermal Properties

Latent Heat of Fusion, J/g 350
270
Maximum Temperature: Mechanical, °C 140
740
Melting Completion (Liquidus), °C 590
1450
Melting Onset (Solidus), °C 460
1410
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 73
27
Thermal Expansion, µm/m-K 25
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 59
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 12
7.5
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 22
2.1
Embodied Energy, MJ/kg 160
30
Embodied Water, L/kg 1000
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.3 to 15
110 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 66 to 210
420 to 840
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 70
25
Strength to Weight: Axial, points 25 to 44
22 to 25
Strength to Weight: Bending, points 38 to 54
21 to 22
Thermal Diffusivity, mm2/s 43
7.2
Thermal Shock Resistance, points 9.7 to 17
22 to 25

Alloy Composition

Aluminum (Al), % 9.3 to 10.7
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
11.5 to 12.5
Copper (Cu), % 0 to 0.1
0 to 0.3
Iron (Fe), % 0
83.8 to 87.2
Magnesium (Mg), % 87.9 to 90.6
0
Manganese (Mn), % 0.1 to 0.35
0.5 to 0.8
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0 to 0.010
0.8 to 1.5
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.3
0 to 0.4
Sulfur (S), % 0
0 to 0.020
Vanadium (V), % 0
0 to 0.080
Zinc (Zn), % 0 to 0.3
0
Residuals, % 0 to 0.3
0

Comparable Variants