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S15500 Stainless Steel vs. 7049A Aluminum

S15500 stainless steel belongs to the iron alloys classification, while 7049A aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (6, 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 S15500 stainless steel and the bottom bar is 7049A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 6.8 to 16
5.0 to 5.7
Fatigue Strength, MPa 350 to 650
180
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 75
27
Shear Strength, MPa 540 to 870
340 to 350
Tensile Strength: Ultimate (UTS), MPa 890 to 1490
580 to 590
Tensile Strength: Yield (Proof), MPa 590 to 1310
500 to 530

Thermal Properties

Latent Heat of Fusion, J/g 280
370
Maximum Temperature: Mechanical, °C 820
200
Melting Completion (Liquidus), °C 1430
640
Melting Onset (Solidus), °C 1380
430
Specific Heat Capacity, J/kg-K 480
850
Thermal Conductivity, W/m-K 17
130
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
40
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
120

Otherwise Unclassified Properties

Base Metal Price, % relative 13
10
Density, g/cm3 7.8
3.1
Embodied Carbon, kg CO2/kg material 2.7
8.2
Embodied Energy, MJ/kg 39
150
Embodied Water, L/kg 130
1100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 98 to 120
28 to 32
Resilience: Unit (Modulus of Resilience), kJ/m3 890 to 4460
1800 to 1990
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
44
Strength to Weight: Axial, points 32 to 53
52 to 53
Strength to Weight: Bending, points 26 to 37
50 to 51
Thermal Diffusivity, mm2/s 4.6
50
Thermal Shock Resistance, points 30 to 50
25

Alloy Composition

Aluminum (Al), % 0
84.6 to 89.5
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 14 to 15.5
0.050 to 0.25
Copper (Cu), % 2.5 to 4.5
1.2 to 1.9
Iron (Fe), % 71.9 to 79.9
0 to 0.5
Magnesium (Mg), % 0
2.1 to 3.1
Manganese (Mn), % 0 to 1.0
0 to 0.5
Nickel (Ni), % 3.5 to 5.5
0
Niobium (Nb), % 0.15 to 0.45
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0 to 0.4
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
7.2 to 8.4
Zirconium (Zr), % 0
0 to 0.25
Residuals, % 0
0 to 0.15