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EN AC-48100 Aluminum vs. ASTM A369 Grade FP21

EN AC-48100 aluminum belongs to the aluminum alloys classification, while ASTM A369 grade FP21 belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 AC-48100 aluminum and the bottom bar is ASTM A369 grade FP21.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 100 to 140
140
Elastic (Young's, Tensile) Modulus, GPa 76
190
Elongation at Break, % 1.1
20
Fatigue Strength, MPa 120 to 130
160
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 29
74
Tensile Strength: Ultimate (UTS), MPa 240 to 330
470
Tensile Strength: Yield (Proof), MPa 190 to 300
240

Thermal Properties

Latent Heat of Fusion, J/g 640
260
Maximum Temperature: Mechanical, °C 170
470
Melting Completion (Liquidus), °C 580
1470
Melting Onset (Solidus), °C 470
1430
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 130
41
Thermal Expansion, µm/m-K 20
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 27
7.7
Electrical Conductivity: Equal Weight (Specific), % IACS 87
8.8

Otherwise Unclassified Properties

Base Metal Price, % relative 11
4.0
Density, g/cm3 2.8
7.8
Embodied Carbon, kg CO2/kg material 7.3
1.8
Embodied Energy, MJ/kg 130
23
Embodied Water, L/kg 940
61

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3 to 3.6
80
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 580
150
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 24 to 33
17
Strength to Weight: Bending, points 31 to 38
17
Thermal Diffusivity, mm2/s 55
11
Thermal Shock Resistance, points 11 to 16
14

Alloy Composition

Aluminum (Al), % 72.1 to 79.8
0
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0
2.7 to 3.4
Copper (Cu), % 4.0 to 5.0
0
Iron (Fe), % 0 to 1.3
94.3 to 96.2
Magnesium (Mg), % 0.25 to 0.65
0
Manganese (Mn), % 0 to 0.5
0.3 to 0.6
Molybdenum (Mo), % 0
0.8 to 1.1
Nickel (Ni), % 0 to 0.3
0
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 16 to 18
0 to 0.5
Sulfur (S), % 0
0 to 0.025
Tin (Sn), % 0 to 0.15
0
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 1.5
0
Residuals, % 0 to 0.25
0