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295.0 Aluminum vs. S44800 Stainless Steel

295.0 aluminum belongs to the aluminum alloys classification, while S44800 stainless steel belongs to the iron alloys. There are 31 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 295.0 aluminum and the bottom bar is S44800 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 60 to 93
190
Elastic (Young's, Tensile) Modulus, GPa 71
210
Elongation at Break, % 2.0 to 7.2
23
Fatigue Strength, MPa 44 to 55
300
Poisson's Ratio 0.33
0.27
Shear Modulus, GPa 27
82
Shear Strength, MPa 180 to 230
370
Tensile Strength: Ultimate (UTS), MPa 230 to 280
590
Tensile Strength: Yield (Proof), MPa 100 to 220
450

Thermal Properties

Latent Heat of Fusion, J/g 400
300
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 530
1410
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 140
17
Thermal Expansion, µm/m-K 23
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
2.6
Electrical Conductivity: Equal Weight (Specific), % IACS 100
3.0

Otherwise Unclassified Properties

Base Metal Price, % relative 10
19
Density, g/cm3 3.0
7.8
Embodied Carbon, kg CO2/kg material 7.9
3.8
Embodied Energy, MJ/kg 150
52
Embodied Water, L/kg 1140
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.2 to 13
120
Resilience: Unit (Modulus of Resilience), kJ/m3 77 to 340
480
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 46
25
Strength to Weight: Axial, points 21 to 26
21
Strength to Weight: Bending, points 27 to 32
20
Thermal Diffusivity, mm2/s 54
4.6
Thermal Shock Resistance, points 9.8 to 12
19

Alloy Composition

Aluminum (Al), % 91.4 to 95.3
0
Carbon (C), % 0
0 to 0.010
Chromium (Cr), % 0
28 to 30
Copper (Cu), % 4.0 to 5.0
0 to 0.15
Iron (Fe), % 0 to 1.0
62.6 to 66.5
Magnesium (Mg), % 0 to 0.030
0
Manganese (Mn), % 0 to 0.35
0 to 0.3
Molybdenum (Mo), % 0
3.5 to 4.2
Nickel (Ni), % 0
2.0 to 2.5
Nitrogen (N), % 0
0 to 0.020
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0.7 to 1.5
0 to 0.2
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0