Monel K-500 vs. C36200 Brass
Monel K-500 belongs to the nickel alloys classification, while C36200 brass belongs to the copper alloys. They have a modest 30% 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 (4, in this case) are not shown.
For each property being compared, the top bar is Monel K-500 and the bottom bar is C36200 brass.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 160 | |
100 |
Elongation at Break, % | 25 to 36 | |
20 to 53 |
Poisson's Ratio | 0.32 | |
0.31 |
Shear Modulus, GPa | 61 | |
39 |
Shear Strength, MPa | 430 to 700 | |
210 to 240 |
Tensile Strength: Ultimate (UTS), MPa | 640 to 1100 | |
340 to 420 |
Tensile Strength: Yield (Proof), MPa | 310 to 880 | |
130 to 360 |
Thermal Properties
Latent Heat of Fusion, J/g | 270 | |
170 |
Maximum Temperature: Mechanical, °C | 900 | |
120 |
Melting Completion (Liquidus), °C | 1350 | |
900 |
Melting Onset (Solidus), °C | 1320 | |
890 |
Specific Heat Capacity, J/kg-K | 440 | |
380 |
Thermal Conductivity, W/m-K | 18 | |
120 |
Thermal Expansion, µm/m-K | 14 | |
21 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 3.1 | |
26 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 3.2 | |
28 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 50 | |
23 |
Density, g/cm3 | 8.7 | |
8.2 |
Embodied Carbon, kg CO2/kg material | 8.1 | |
2.6 |
Embodied Energy, MJ/kg | 120 | |
45 |
Embodied Water, L/kg | 280 | |
320 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 180 to 260 | |
74 to 140 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 300 to 2420 | |
89 to 630 |
Stiffness to Weight: Axial, points | 10 | |
6.9 |
Stiffness to Weight: Bending, points | 21 | |
19 |
Strength to Weight: Axial, points | 21 to 35 | |
11 to 14 |
Strength to Weight: Bending, points | 19 to 27 | |
13 to 15 |
Thermal Diffusivity, mm2/s | 4.8 | |
37 |
Thermal Shock Resistance, points | 21 to 36 | |
11 to 14 |
Alloy Composition
Aluminum (Al), % | 2.3 to 3.2 | |
0 |
Carbon (C), % | 0 to 0.18 | |
0 |
Copper (Cu), % | 27 to 33 | |
60 to 63 |
Iron (Fe), % | 0 to 2.0 | |
0 to 0.15 |
Lead (Pb), % | 0 | |
3.5 to 4.5 |
Manganese (Mn), % | 0 to 1.5 | |
0 |
Nickel (Ni), % | 63 to 70.4 | |
0 |
Silicon (Si), % | 0 to 0.5 | |
0 |
Sulfur (S), % | 0 to 0.010 | |
0 |
Titanium (Ti), % | 0.35 to 0.85 | |
0 |
Zinc (Zn), % | 0 | |
32.4 to 36.5 |