C99400 Brass vs. C46200 Brass
Both C99400 brass and C46200 brass are copper alloys. They have 67% of their average alloy composition in common. There are 22 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown.
For each property being compared, the top bar is C99400 brass and the bottom bar is C46200 brass.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 120 | |
100 |
Poisson's Ratio | 0.34 | |
0.31 |
Shear Modulus, GPa | 44 | |
40 |
Tensile Strength: Ultimate (UTS), MPa | 460 to 550 | |
370 to 480 |
Tensile Strength: Yield (Proof), MPa | 230 to 370 | |
120 to 290 |
Thermal Properties
Latent Heat of Fusion, J/g | 230 | |
170 |
Maximum Temperature: Mechanical, °C | 200 | |
120 |
Melting Completion (Liquidus), °C | 1070 | |
840 |
Melting Onset (Solidus), °C | 1020 | |
800 |
Specific Heat Capacity, J/kg-K | 400 | |
380 |
Thermal Expansion, µm/m-K | 17 | |
20 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 30 | |
24 |
Density, g/cm3 | 8.7 | |
8.1 |
Embodied Carbon, kg CO2/kg material | 2.8 | |
2.7 |
Embodied Energy, MJ/kg | 45 | |
46 |
Embodied Water, L/kg | 310 | |
330 |
Common Calculations
Resilience: Unit (Modulus of Resilience), kJ/m3 | 230 to 590 | |
72 to 400 |
Stiffness to Weight: Axial, points | 7.5 | |
7.2 |
Stiffness to Weight: Bending, points | 19 | |
19 |
Strength to Weight: Axial, points | 15 to 17 | |
13 to 16 |
Strength to Weight: Bending, points | 15 to 17 | |
14 to 17 |
Thermal Shock Resistance, points | 16 to 19 | |
12 to 16 |
Alloy Composition
Aluminum (Al), % | 0.5 to 2.0 | |
0 |
Copper (Cu), % | 83.5 to 96.5 | |
62 to 65 |
Iron (Fe), % | 1.0 to 3.0 | |
0 to 0.1 |
Lead (Pb), % | 0 to 0.25 | |
0 to 0.2 |
Manganese (Mn), % | 0 to 0.5 | |
0 |
Nickel (Ni), % | 1.0 to 3.5 | |
0 |
Silicon (Si), % | 0.5 to 2.0 | |
0 |
Tin (Sn), % | 0 | |
0.5 to 1.0 |
Zinc (Zn), % | 0.5 to 5.0 | |
33.3 to 37.5 |
Residuals, % | 0 | |
0 to 0.4 |