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EN 1.4962 Stainless Steel vs. 7076 Aluminum

EN 1.4962 stainless steel belongs to the iron alloys classification, while 7076 aluminum belongs to the aluminum alloys. There are 31 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 EN 1.4962 stainless steel and the bottom bar is 7076 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 190 to 210
160
Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 22 to 34
6.2
Fatigue Strength, MPa 210 to 330
170
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 77
27
Shear Strength, MPa 420 to 440
310
Tensile Strength: Ultimate (UTS), MPa 630 to 690
530
Tensile Strength: Yield (Proof), MPa 260 to 490
460

Thermal Properties

Latent Heat of Fusion, J/g 280
380
Maximum Temperature: Mechanical, °C 910
170
Melting Completion (Liquidus), °C 1480
630
Melting Onset (Solidus), °C 1440
460
Specific Heat Capacity, J/kg-K 470
860
Thermal Conductivity, W/m-K 14
140
Thermal Expansion, µm/m-K 16
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
35
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
100

Otherwise Unclassified Properties

Base Metal Price, % relative 23
9.5
Density, g/cm3 8.1
3.0
Embodied Carbon, kg CO2/kg material 4.1
8.0
Embodied Energy, MJ/kg 59
150
Embodied Water, L/kg 150
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140 to 170
31
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 610
1510
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
45
Strength to Weight: Axial, points 21 to 24
49
Strength to Weight: Bending, points 20 to 21
48
Thermal Diffusivity, mm2/s 3.7
54
Thermal Shock Resistance, points 14 to 16
23

Alloy Composition

Aluminum (Al), % 0
86.9 to 91.2
Boron (B), % 0.0015 to 0.0060
0
Carbon (C), % 0.070 to 0.15
0
Chromium (Cr), % 15.5 to 17.5
0
Copper (Cu), % 0
0.3 to 1.0
Iron (Fe), % 62.1 to 69
0 to 0.6
Magnesium (Mg), % 0
1.2 to 2.0
Manganese (Mn), % 0 to 1.5
0.3 to 0.8
Nickel (Ni), % 12.5 to 14.5
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 0.5
0 to 0.4
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0.4 to 0.7
0 to 0.2
Tungsten (W), % 2.5 to 3.0
0
Zinc (Zn), % 0
7.0 to 8.0
Residuals, % 0
0 to 0.15