MakeItFrom.com
Menu (ESC)

242.0 Aluminum vs. EN 1.7710 Steel

242.0 aluminum belongs to the aluminum alloys classification, while EN 1.7710 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 242.0 aluminum and the bottom bar is EN 1.7710 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 70 to 110
280 to 320
Elastic (Young's, Tensile) Modulus, GPa 73
190
Elongation at Break, % 0.5 to 1.5
6.8 to 11
Fatigue Strength, MPa 55 to 110
500 to 620
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
73
Tensile Strength: Ultimate (UTS), MPa 180 to 290
930 to 1070
Tensile Strength: Yield (Proof), MPa 120 to 220
800 to 1060

Thermal Properties

Latent Heat of Fusion, J/g 390
260
Maximum Temperature: Mechanical, °C 210
440
Melting Completion (Liquidus), °C 640
1470
Melting Onset (Solidus), °C 530
1430
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 130 to 170
41
Thermal Expansion, µm/m-K 22
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33 to 44
7.5
Electrical Conductivity: Equal Weight (Specific), % IACS 96 to 130
8.6

Otherwise Unclassified Properties

Base Metal Price, % relative 12
3.5
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 8.3
2.2
Embodied Energy, MJ/kg 150
30
Embodied Water, L/kg 1130
57

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.3 to 3.4
73 to 100
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 340
1680 to 2970
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 45
24
Strength to Weight: Axial, points 16 to 26
33 to 38
Strength to Weight: Bending, points 23 to 32
27 to 30
Thermal Diffusivity, mm2/s 50 to 62
11
Thermal Shock Resistance, points 8.0 to 13
27 to 31

Alloy Composition

Aluminum (Al), % 88.4 to 93.6
0
Carbon (C), % 0
0.12 to 0.18
Chromium (Cr), % 0 to 0.25
1.3 to 1.8
Copper (Cu), % 3.5 to 4.5
0
Iron (Fe), % 0 to 1.0
95.1 to 97
Magnesium (Mg), % 1.2 to 1.8
0
Manganese (Mn), % 0 to 0.35
0.6 to 1.0
Molybdenum (Mo), % 0
0.8 to 1.0
Nickel (Ni), % 1.7 to 2.3
0
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.7
0 to 0.6
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
0
Vanadium (V), % 0
0.15 to 0.25
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0

Comparable Variants