EN 1.4062 Stainless Steel vs. C68400 Brass
EN 1.4062 stainless steel belongs to the iron alloys classification, while C68400 brass belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.
For each property being compared, the top bar is EN 1.4062 stainless steel and the bottom bar is C68400 brass.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 110 |
| Elongation at Break, % | 23 to 34 | |
| 18 |
| Poisson's Ratio | 0.27 | |
| 0.31 |
| Shear Modulus, GPa | 79 | |
| 41 |
| Shear Strength, MPa | 510 | |
| 330 |
| Tensile Strength: Ultimate (UTS), MPa | 770 to 800 | |
| 540 |
| Tensile Strength: Yield (Proof), MPa | 530 to 600 | |
| 310 |
Thermal Properties
| Latent Heat of Fusion, J/g | 290 | |
| 210 |
| Maximum Temperature: Mechanical, °C | 1030 | |
| 130 |
| Melting Completion (Liquidus), °C | 1430 | |
| 840 |
| Melting Onset (Solidus), °C | 1380 | |
| 820 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 400 |
| Thermal Conductivity, W/m-K | 15 | |
| 66 |
| Thermal Expansion, µm/m-K | 13 | |
| 20 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.1 | |
| 87 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.4 | |
| 99 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 12 | |
| 23 |
| Density, g/cm3 | 7.7 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 2.6 | |
| 2.7 |
| Embodied Energy, MJ/kg | 37 | |
| 47 |
| Embodied Water, L/kg | 150 | |
| 320 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 170 to 230 | |
| 81 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 690 to 910 | |
| 460 |
| Stiffness to Weight: Axial, points | 14 | |
| 7.5 |
| Stiffness to Weight: Bending, points | 25 | |
| 20 |
| Strength to Weight: Axial, points | 28 to 29 | |
| 19 |
| Strength to Weight: Bending, points | 24 to 25 | |
| 19 |
| Thermal Diffusivity, mm2/s | 4.0 | |
| 21 |
| Thermal Shock Resistance, points | 21 to 22 | |
| 18 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 0 to 0.5 |
| Boron (B), % | 0 | |
| 0.0010 to 0.030 |
| Carbon (C), % | 0 to 0.030 | |
| 0 |
| Chromium (Cr), % | 21.5 to 24 | |
| 0 |
| Copper (Cu), % | 0 | |
| 59 to 64 |
| Iron (Fe), % | 69.3 to 77.3 | |
| 0 to 1.0 |
| Lead (Pb), % | 0 | |
| 0 to 0.090 |
| Manganese (Mn), % | 0 to 2.0 | |
| 0.2 to 1.5 |
| Molybdenum (Mo), % | 0 to 0.45 | |
| 0 |
| Nickel (Ni), % | 1.0 to 2.9 | |
| 0 to 0.5 |
| Nitrogen (N), % | 0.16 to 0.28 | |
| 0 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0.030 to 0.3 |
| Silicon (Si), % | 0 to 1.0 | |
| 1.5 to 2.5 |
| Sulfur (S), % | 0 to 0.010 | |
| 0 |
| Tin (Sn), % | 0 | |
| 0 to 0.5 |
| Zinc (Zn), % | 0 | |
| 28.6 to 39.3 |
| Residuals, % | 0 | |
| 0 to 0.5 |