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EN 1.4655 Stainless Steel vs. 7204 Aluminum

EN 1.4655 stainless steel belongs to the iron alloys classification, while 7204 aluminum belongs to the aluminum 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 1.4655 stainless steel and the bottom bar is 7204 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 23 to 25
11 to 13
Fatigue Strength, MPa 320
110 to 130
Poisson's Ratio 0.27
0.33
Shear Modulus, GPa 78
26
Shear Strength, MPa 460
130 to 220
Tensile Strength: Ultimate (UTS), MPa 720 to 730
220 to 380
Tensile Strength: Yield (Proof), MPa 450 to 480
120 to 310

Thermal Properties

Latent Heat of Fusion, J/g 290
380
Maximum Temperature: Mechanical, °C 1050
210
Melting Completion (Liquidus), °C 1420
640
Melting Onset (Solidus), °C 1370
520
Specific Heat Capacity, J/kg-K 480
880
Thermal Conductivity, W/m-K 15
150
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
39
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
120

Otherwise Unclassified Properties

Base Metal Price, % relative 15
9.5
Density, g/cm3 7.7
2.9
Embodied Carbon, kg CO2/kg material 2.9
8.4
Embodied Energy, MJ/kg 41
150
Embodied Water, L/kg 160
1140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 150 to 160
25 to 40
Resilience: Unit (Modulus of Resilience), kJ/m3 510 to 580
110 to 710
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
47
Strength to Weight: Axial, points 26
21 to 36
Strength to Weight: Bending, points 23
28 to 40
Thermal Diffusivity, mm2/s 4.0
58
Thermal Shock Resistance, points 20
9.4 to 16

Alloy Composition


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Aluminum (Al), % 0
90.5 to 94.8
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 22 to 24
0 to 0.3
Copper (Cu), % 1.0 to 3.0
0 to 0.2
Iron (Fe), % 63.6 to 73.4
0 to 0.35
Magnesium (Mg), % 0
1.0 to 2.0
Manganese (Mn), % 0 to 2.0
0.2 to 0.7
Molybdenum (Mo), % 0.1 to 0.6
0
Nickel (Ni), % 3.5 to 5.5
0
Nitrogen (N), % 0.050 to 0.2
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 1.0
0 to 0.3
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.2
Vanadium (V), % 0
0 to 0.1
Zinc (Zn), % 0
4.0 to 5.0
Zirconium (Zr), % 0
0 to 0.25
Residuals, % 0
0 to 0.15