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AZ63A Magnesium vs. ASTM A387 Grade 21L Class 1

AZ63A magnesium belongs to the magnesium alloys classification, while ASTM A387 grade 21L class 1 belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 AZ63A magnesium and the bottom bar is ASTM A387 grade 21L class 1.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 2.2 to 8.0
21
Fatigue Strength, MPa 76 to 83
160
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
74
Shear Strength, MPa 110 to 160
310
Tensile Strength: Ultimate (UTS), MPa 190 to 270
500
Tensile Strength: Yield (Proof), MPa 81 to 120
230

Thermal Properties

Latent Heat of Fusion, J/g 350
260
Maximum Temperature: Mechanical, °C 120
480
Melting Completion (Liquidus), °C 610
1470
Melting Onset (Solidus), °C 450
1430
Specific Heat Capacity, J/kg-K 980
470
Thermal Conductivity, W/m-K 52 to 65
41
Thermal Expansion, µm/m-K 26
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12 to 15
7.6
Electrical Conductivity: Equal Weight (Specific), % IACS 59 to 74
8.8

Otherwise Unclassified Properties

Base Metal Price, % relative 12
4.1
Density, g/cm3 1.8
7.9
Embodied Carbon, kg CO2/kg material 22
1.8
Embodied Energy, MJ/kg 150
23
Embodied Water, L/kg 970
62

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.7 to 16
84
Resilience: Unit (Modulus of Resilience), kJ/m3 71 to 160
140
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 66
24
Strength to Weight: Axial, points 29 to 41
18
Strength to Weight: Bending, points 40 to 51
18
Thermal Diffusivity, mm2/s 29 to 37
11
Thermal Shock Resistance, points 11 to 16
14

Alloy Composition


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Aluminum (Al), % 5.3 to 6.7
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
2.8 to 3.3
Copper (Cu), % 0 to 0.25
0
Iron (Fe), % 0
94.4 to 96.1
Magnesium (Mg), % 88.6 to 92.1
0
Manganese (Mn), % 0.15 to 0.35
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 0 to 0.010
0
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.3
0 to 0.5
Sulfur (S), % 0
0 to 0.025
Zinc (Zn), % 2.5 to 3.5
0
Residuals, % 0 to 0.3
0