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707.0 Aluminum vs. S15500 Stainless Steel

707.0 aluminum belongs to the aluminum alloys classification, while S15500 stainless steel belongs to the iron alloys. There are 29 material properties with values for both materials. Properties with values for just one material (8, 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 707.0 aluminum and the bottom bar is S15500 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 1.7 to 3.4
6.8 to 16
Fatigue Strength, MPa 75 to 140
350 to 650
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
75
Tensile Strength: Ultimate (UTS), MPa 270 to 300
890 to 1490
Tensile Strength: Yield (Proof), MPa 170 to 250
590 to 1310

Thermal Properties

Latent Heat of Fusion, J/g 380
280
Maximum Temperature: Mechanical, °C 180
820
Melting Completion (Liquidus), °C 630
1430
Melting Onset (Solidus), °C 600
1380
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 150
17
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 110
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
13
Density, g/cm3 2.9
7.8
Embodied Carbon, kg CO2/kg material 8.3
2.7
Embodied Energy, MJ/kg 150
39
Embodied Water, L/kg 1140
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.3 to 8.6
98 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 430
890 to 4460
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
25
Strength to Weight: Axial, points 26 to 29
32 to 53
Strength to Weight: Bending, points 32 to 34
26 to 37
Thermal Diffusivity, mm2/s 58
4.6
Thermal Shock Resistance, points 12 to 13
30 to 50

Alloy Composition

Aluminum (Al), % 90.5 to 93.6
0
Carbon (C), % 0
0 to 0.070
Chromium (Cr), % 0.2 to 0.4
14 to 15.5
Copper (Cu), % 0 to 0.2
2.5 to 4.5
Iron (Fe), % 0 to 0.8
71.9 to 79.9
Magnesium (Mg), % 1.8 to 2.4
0
Manganese (Mn), % 0.4 to 0.6
0 to 1.0
Nickel (Ni), % 0
3.5 to 5.5
Niobium (Nb), % 0
0.15 to 0.45
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.2
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 4.0 to 4.5
0
Residuals, % 0 to 0.15
0