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7075-T6 Aluminum vs. AISI 304 Stainless Steel

7075-T6 aluminum belongs to the aluminum alloys classification, while AISI 304 stainless steel belongs to the iron alloys. There are 32 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 7075-T6 aluminum and the bottom bar is AISI 304 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 150
170 to 360
Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 7.9
8.0 to 43
Fatigue Strength, MPa 160
210 to 440
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 330
400 to 690
Tensile Strength: Ultimate (UTS), MPa 560
580 to 1180
Tensile Strength: Yield (Proof), MPa 480
230 to 860

Thermal Properties

Latent Heat of Fusion, J/g 380
290
Maximum Temperature: Mechanical, °C 200
710
Melting Completion (Liquidus), °C 640
1450
Melting Onset (Solidus), °C 480
1400
Specific Heat Capacity, J/kg-K 870
480
Thermal Conductivity, W/m-K 130
16
Thermal Expansion, µm/m-K 23
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 98
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 10
15
Calomel Potential, mV -750
-80
Density, g/cm3 3.0
7.8
Embodied Carbon, kg CO2/kg material 8.3
3.0
Embodied Energy, MJ/kg 150
43
Embodied Water, L/kg 1120
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 42
86 to 250
Resilience: Unit (Modulus of Resilience), kJ/m3 1630
140 to 1870
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
25
Strength to Weight: Axial, points 51
21 to 42
Strength to Weight: Bending, points 50
20 to 32
Thermal Diffusivity, mm2/s 50
4.2
Thermal Shock Resistance, points 24
12 to 25

Alloy Composition

Aluminum (Al), % 86.9 to 91.4
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0.18 to 0.28
18 to 20
Copper (Cu), % 1.2 to 2.0
0
Iron (Fe), % 0 to 0.5
66.5 to 74
Magnesium (Mg), % 2.1 to 2.9
0
Manganese (Mn), % 0 to 0.3
0 to 2.0
Nickel (Ni), % 0
8.0 to 10.5
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.4
0 to 0.75
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 5.1 to 6.1
0
Zirconium (Zr), % 0 to 0.25
0
Residuals, % 0 to 0.15
0