C33200 Brass vs. N10675 Nickel
C33200 brass belongs to the copper alloys classification, while N10675 nickel belongs to the nickel alloys. There are 29 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.
For each property being compared, the top bar is C33200 brass and the bottom bar is N10675 nickel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 100 | |
| 220 |
| Elongation at Break, % | 7.0 to 60 | |
| 47 |
| Poisson's Ratio | 0.31 | |
| 0.31 |
| Shear Modulus, GPa | 40 | |
| 85 |
| Shear Strength, MPa | 240 to 300 | |
| 610 |
| Tensile Strength: Ultimate (UTS), MPa | 320 to 520 | |
| 860 |
| Tensile Strength: Yield (Proof), MPa | 110 to 450 | |
| 400 |
Thermal Properties
| Latent Heat of Fusion, J/g | 170 | |
| 320 |
| Maximum Temperature: Mechanical, °C | 130 | |
| 910 |
| Melting Completion (Liquidus), °C | 930 | |
| 1420 |
| Melting Onset (Solidus), °C | 900 | |
| 1370 |
| Specific Heat Capacity, J/kg-K | 380 | |
| 380 |
| Thermal Conductivity, W/m-K | 120 | |
| 11 |
| Thermal Expansion, µm/m-K | 20 | |
| 11 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 26 | |
| 1.3 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 28 | |
| 1.2 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 24 | |
| 80 |
| Density, g/cm3 | 8.2 | |
| 9.3 |
| Embodied Carbon, kg CO2/kg material | 2.6 | |
| 16 |
| Embodied Energy, MJ/kg | 44 | |
| 210 |
| Embodied Water, L/kg | 320 | |
| 280 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 35 to 150 | |
| 330 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 60 to 960 | |
| 350 |
| Stiffness to Weight: Axial, points | 7.1 | |
| 13 |
| Stiffness to Weight: Bending, points | 19 | |
| 22 |
| Strength to Weight: Axial, points | 11 to 17 | |
| 26 |
| Strength to Weight: Bending, points | 13 to 17 | |
| 22 |
| Thermal Diffusivity, mm2/s | 37 | |
| 3.1 |
| Thermal Shock Resistance, points | 11 to 17 | |
| 26 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 0 to 0.5 |
| Carbon (C), % | 0 | |
| 0 to 0.010 |
| Chromium (Cr), % | 0 | |
| 1.0 to 3.0 |
| Cobalt (Co), % | 0 | |
| 0 to 3.0 |
| Copper (Cu), % | 65 to 68 | |
| 0 to 0.2 |
| Iron (Fe), % | 0 to 0.070 | |
| 1.0 to 3.0 |
| Lead (Pb), % | 1.5 to 2.5 | |
| 0 |
| Manganese (Mn), % | 0 | |
| 0 to 3.0 |
| Molybdenum (Mo), % | 0 | |
| 27 to 32 |
| Nickel (Ni), % | 0 | |
| 51.3 to 71 |
| Niobium (Nb), % | 0 | |
| 0 to 0.2 |
| Phosphorus (P), % | 0 | |
| 0 to 0.030 |
| Silicon (Si), % | 0 | |
| 0 to 0.1 |
| Sulfur (S), % | 0 | |
| 0 to 0.010 |
| Tantalum (Ta), % | 0 | |
| 0 to 0.2 |
| Titanium (Ti), % | 0 | |
| 0 to 0.2 |
| Tungsten (W), % | 0 | |
| 0 to 3.0 |
| Vanadium (V), % | 0 | |
| 0 to 0.2 |
| Zinc (Zn), % | 29 to 33.5 | |
| 0 to 0.1 |
| Residuals, % | 0 to 0.4 | |
| 0 |