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ISO-WD32350 Magnesium vs. AISI 410 Stainless Steel

ISO-WD32350 magnesium belongs to the magnesium alloys classification, while AISI 410 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 ISO-WD32350 magnesium and the bottom bar is AISI 410 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 5.7 to 10
16 to 22
Fatigue Strength, MPa 120 to 130
190 to 350
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
76
Shear Strength, MPa 150 to 170
330 to 470
Tensile Strength: Ultimate (UTS), MPa 250 to 290
520 to 770
Tensile Strength: Yield (Proof), MPa 140 to 180
290 to 580

Thermal Properties

Latent Heat of Fusion, J/g 340
270
Maximum Temperature: Mechanical, °C 95
710
Melting Completion (Liquidus), °C 600
1530
Melting Onset (Solidus), °C 560
1480
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 130
30
Thermal Expansion, µm/m-K 25
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 130
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 12
7.0
Density, g/cm3 1.7
7.7
Embodied Carbon, kg CO2/kg material 23
1.9
Embodied Energy, MJ/kg 160
27
Embodied Water, L/kg 960
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 23
97 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 380
210 to 860
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 68
25
Strength to Weight: Axial, points 39 to 46
19 to 28
Strength to Weight: Bending, points 50 to 55
19 to 24
Thermal Diffusivity, mm2/s 73
8.1
Thermal Shock Resistance, points 16 to 18
18 to 26

Alloy Composition

Aluminum (Al), % 0 to 0.1
0
Carbon (C), % 0
0.080 to 0.15
Chromium (Cr), % 0
11.5 to 13.5
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.060
83.5 to 88.4
Magnesium (Mg), % 95.7 to 97.7
0
Manganese (Mn), % 0.6 to 1.3
0 to 1.0
Nickel (Ni), % 0 to 0.0050
0 to 0.75
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.1
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Zinc (Zn), % 1.8 to 2.3
0
Residuals, % 0 to 0.3
0

Comparable Variants