C68800 Brass vs. Monel 400
C68800 brass belongs to the copper alloys classification, while Monel 400 belongs to the nickel alloys. They have a modest 31% of their average alloy composition in common, which, by itself, doesn't mean much. There are 29 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.
For each property being compared, the top bar is C68800 brass and the bottom bar is Monel 400.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 110 | |
160 |
Elongation at Break, % | 2.0 to 36 | |
20 to 40 |
Poisson's Ratio | 0.32 | |
0.32 |
Shear Modulus, GPa | 41 | |
62 |
Shear Strength, MPa | 380 to 510 | |
370 to 490 |
Tensile Strength: Ultimate (UTS), MPa | 570 to 890 | |
540 to 780 |
Tensile Strength: Yield (Proof), MPa | 390 to 790 | |
210 to 590 |
Thermal Properties
Latent Heat of Fusion, J/g | 190 | |
270 |
Maximum Temperature: Mechanical, °C | 160 | |
1000 |
Melting Completion (Liquidus), °C | 960 | |
1350 |
Melting Onset (Solidus), °C | 950 | |
1300 |
Specific Heat Capacity, J/kg-K | 400 | |
430 |
Thermal Conductivity, W/m-K | 40 | |
23 |
Thermal Expansion, µm/m-K | 19 | |
14 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 18 | |
3.3 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 20 | |
3.4 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 26 | |
50 |
Density, g/cm3 | 8.2 | |
8.9 |
Embodied Carbon, kg CO2/kg material | 2.8 | |
7.9 |
Embodied Energy, MJ/kg | 48 | |
110 |
Embodied Water, L/kg | 350 | |
250 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 16 to 180 | |
140 to 180 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 710 to 2860 | |
140 to 1080 |
Stiffness to Weight: Axial, points | 7.3 | |
10 |
Stiffness to Weight: Bending, points | 19 | |
21 |
Strength to Weight: Axial, points | 19 to 30 | |
17 to 25 |
Strength to Weight: Bending, points | 19 to 25 | |
17 to 21 |
Thermal Diffusivity, mm2/s | 12 | |
6.1 |
Thermal Shock Resistance, points | 19 to 30 | |
17 to 25 |
Alloy Composition
Aluminum (Al), % | 3.0 to 3.8 | |
0 |
Carbon (C), % | 0 | |
0 to 0.3 |
Cobalt (Co), % | 0.25 to 0.55 | |
0 |
Copper (Cu), % | 70.8 to 75.5 | |
28 to 34 |
Iron (Fe), % | 0 to 0.2 | |
0 to 2.5 |
Lead (Pb), % | 0 to 0.050 | |
0 |
Manganese (Mn), % | 0 | |
0 to 2.0 |
Nickel (Ni), % | 0 | |
63 to 72 |
Silicon (Si), % | 0 | |
0 to 0.5 |
Sulfur (S), % | 0 | |
0 to 0.024 |
Zinc (Zn), % | 21.3 to 24.1 | |
0 |
Residuals, % | 0 to 0.5 | |
0 |