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AISI 302 Stainless Steel vs. AZ63A Magnesium

AISI 302 stainless steel belongs to the iron alloys classification, while AZ63A 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 AISI 302 stainless steel and the bottom bar is AZ63A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
46
Elongation at Break, % 4.5 to 46
2.2 to 8.0
Fatigue Strength, MPa 210 to 520
76 to 83
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 77
18
Shear Strength, MPa 400 to 830
110 to 160
Tensile Strength: Ultimate (UTS), MPa 580 to 1430
190 to 270
Tensile Strength: Yield (Proof), MPa 230 to 1100
81 to 120

Thermal Properties

Latent Heat of Fusion, J/g 280
350
Maximum Temperature: Mechanical, °C 710
120
Melting Completion (Liquidus), °C 1420
610
Melting Onset (Solidus), °C 1400
450
Specific Heat Capacity, J/kg-K 480
980
Thermal Conductivity, W/m-K 16
52 to 65
Thermal Expansion, µm/m-K 17
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
12 to 15
Electrical Conductivity: Equal Weight (Specific), % IACS 2.8
59 to 74

Otherwise Unclassified Properties

Base Metal Price, % relative 15
12
Density, g/cm3 7.8
1.8
Embodied Carbon, kg CO2/kg material 3.0
22
Embodied Energy, MJ/kg 42
150
Embodied Water, L/kg 140
970

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 59 to 260
3.7 to 16
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 3070
71 to 160
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
66
Strength to Weight: Axial, points 21 to 51
29 to 41
Strength to Weight: Bending, points 20 to 36
40 to 51
Thermal Diffusivity, mm2/s 4.4
29 to 37
Thermal Shock Resistance, points 12 to 31
11 to 16

Alloy Composition

Aluminum (Al), % 0
5.3 to 6.7
Carbon (C), % 0 to 0.15
0
Chromium (Cr), % 17 to 19
0
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 67.9 to 75
0
Magnesium (Mg), % 0
88.6 to 92.1
Manganese (Mn), % 0 to 2.0
0.15 to 0.35
Nickel (Ni), % 8.0 to 10
0 to 0.010
Nitrogen (N), % 0 to 0.1
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 0.75
0 to 0.3
Sulfur (S), % 0 to 0.030
0
Zinc (Zn), % 0
2.5 to 3.5
Residuals, % 0
0 to 0.3