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EN 1.4401 Stainless Steel vs. K1A Magnesium

EN 1.4401 stainless steel belongs to the iron alloys classification, while K1A magnesium belongs to the magnesium 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 EN 1.4401 stainless steel and the bottom bar is K1A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
43
Elongation at Break, % 14 to 40
13
Fatigue Strength, MPa 200 to 320
39
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 78
17
Shear Strength, MPa 410 to 550
55
Tensile Strength: Ultimate (UTS), MPa 600 to 900
180
Tensile Strength: Yield (Proof), MPa 230 to 570
51

Thermal Properties

Latent Heat of Fusion, J/g 290
350
Maximum Temperature: Mechanical, °C 950
120
Melting Completion (Liquidus), °C 1440
650
Melting Onset (Solidus), °C 1400
650
Specific Heat Capacity, J/kg-K 470
1000
Thermal Conductivity, W/m-K 15
120
Thermal Expansion, µm/m-K 16
27

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
30
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
170

Otherwise Unclassified Properties

Base Metal Price, % relative 19
13
Density, g/cm3 7.9
1.6
Embodied Carbon, kg CO2/kg material 3.8
24
Embodied Energy, MJ/kg 52
170
Embodied Water, L/kg 150
970

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110 to 190
17
Resilience: Unit (Modulus of Resilience), kJ/m3 130 to 800
30
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
73
Strength to Weight: Axial, points 21 to 32
31
Strength to Weight: Bending, points 20 to 26
43
Thermal Diffusivity, mm2/s 4.0
75
Thermal Shock Resistance, points 13 to 20
11

Alloy Composition


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Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 16.5 to 18.5
0
Iron (Fe), % 62.8 to 71.5
0
Magnesium (Mg), % 0
98.7 to 99.6
Manganese (Mn), % 0 to 2.0
0
Molybdenum (Mo), % 2.0 to 2.5
0
Nickel (Ni), % 10 to 13
0
Nitrogen (N), % 0 to 0.1
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
0
Sulfur (S), % 0 to 0.015
0
Zirconium (Zr), % 0
0.4 to 1.0
Residuals, % 0
0 to 0.3