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707.0 Aluminum vs. N08800 Stainless Steel

707.0 aluminum belongs to the aluminum alloys classification, while N08800 stainless steel belongs to the iron alloys. There are 29 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 707.0 aluminum and the bottom bar is N08800 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 1.7 to 3.4
4.5 to 34
Fatigue Strength, MPa 75 to 140
150 to 390
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Tensile Strength: Ultimate (UTS), MPa 270 to 300
500 to 1000
Tensile Strength: Yield (Proof), MPa 170 to 250
190 to 830

Thermal Properties

Latent Heat of Fusion, J/g 380
300
Maximum Temperature: Mechanical, °C 180
1100
Melting Completion (Liquidus), °C 630
1390
Melting Onset (Solidus), °C 600
1360
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 150
12
Thermal Expansion, µm/m-K 24
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 110
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
30
Density, g/cm3 2.9
8.0
Embodied Carbon, kg CO2/kg material 8.3
5.3
Embodied Energy, MJ/kg 150
76
Embodied Water, L/kg 1140
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.3 to 8.6
42 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 430
96 to 1740
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
24
Strength to Weight: Axial, points 26 to 29
18 to 35
Strength to Weight: Bending, points 32 to 34
18 to 28
Thermal Diffusivity, mm2/s 58
3.0
Thermal Shock Resistance, points 12 to 13
13 to 25

Alloy Composition


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Aluminum (Al), % 90.5 to 93.6
0.15 to 0.6
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0.2 to 0.4
19 to 23
Copper (Cu), % 0 to 0.2
0 to 0.75
Iron (Fe), % 0 to 0.8
39.5 to 50.7
Magnesium (Mg), % 1.8 to 2.4
0
Manganese (Mn), % 0.4 to 0.6
0 to 1.5
Nickel (Ni), % 0
30 to 35
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.2
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.25
0.15 to 0.6
Zinc (Zn), % 4.0 to 4.5
0
Residuals, % 0 to 0.15
0