C27200 Brass vs. AWS ENiCrCoMo-1
C27200 brass belongs to the copper alloys classification, while AWS ENiCrCoMo-1 belongs to the nickel alloys. There are 20 material properties with values for both materials. Properties with values for just one material (10, in this case) are not shown.
For each property being compared, the top bar is C27200 brass and the bottom bar is AWS ENiCrCoMo-1.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 110 | |
210 |
Elongation at Break, % | 10 to 50 | |
28 |
Poisson's Ratio | 0.31 | |
0.29 |
Shear Modulus, GPa | 40 | |
82 |
Tensile Strength: Ultimate (UTS), MPa | 370 to 590 | |
710 |
Thermal Properties
Latent Heat of Fusion, J/g | 170 | |
330 |
Melting Completion (Liquidus), °C | 920 | |
1430 |
Melting Onset (Solidus), °C | 870 | |
1380 |
Specific Heat Capacity, J/kg-K | 390 | |
440 |
Thermal Expansion, µm/m-K | 20 | |
13 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 24 | |
75 |
Density, g/cm3 | 8.1 | |
8.5 |
Embodied Carbon, kg CO2/kg material | 2.7 | |
11 |
Embodied Energy, MJ/kg | 45 | |
140 |
Embodied Water, L/kg | 320 | |
340 |
Common Calculations
Stiffness to Weight: Axial, points | 7.2 | |
14 |
Stiffness to Weight: Bending, points | 19 | |
23 |
Strength to Weight: Axial, points | 13 to 20 | |
23 |
Strength to Weight: Bending, points | 14 to 19 | |
21 |
Thermal Shock Resistance, points | 12 to 20 | |
19 |
Alloy Composition
Carbon (C), % | 0 | |
0.050 to 0.15 |
Chromium (Cr), % | 0 | |
21 to 26 |
Cobalt (Co), % | 0 | |
9.0 to 15 |
Copper (Cu), % | 62 to 65 | |
0 to 0.5 |
Iron (Fe), % | 0 to 0.070 | |
0 to 5.0 |
Lead (Pb), % | 0 to 0.070 | |
0 |
Manganese (Mn), % | 0 | |
0.3 to 2.5 |
Molybdenum (Mo), % | 0 | |
8.0 to 10 |
Nickel (Ni), % | 0 | |
38.6 to 61.7 |
Niobium (Nb), % | 0 | |
0 to 1.0 |
Phosphorus (P), % | 0 | |
0 to 0.030 |
Silicon (Si), % | 0 | |
0 to 0.75 |
Sulfur (S), % | 0 | |
0 to 0.015 |
Zinc (Zn), % | 34.6 to 38 | |
0 |
Residuals, % | 0 | |
0 to 0.5 |