C35600 Brass vs. N09777 Nickel
C35600 brass belongs to the copper alloys classification, while N09777 nickel belongs to the nickel alloys. There are 20 material properties with values for both materials. Properties with values for just one material (14, in this case) are not shown.
For each property being compared, the top bar is C35600 brass and the bottom bar is N09777 nickel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 100 | |
200 |
Poisson's Ratio | 0.31 | |
0.29 |
Shear Modulus, GPa | 39 | |
77 |
Tensile Strength: Ultimate (UTS), MPa | 340 to 650 | |
580 |
Thermal Properties
Latent Heat of Fusion, J/g | 170 | |
300 |
Maximum Temperature: Mechanical, °C | 120 | |
960 |
Melting Completion (Liquidus), °C | 900 | |
1440 |
Melting Onset (Solidus), °C | 890 | |
1390 |
Specific Heat Capacity, J/kg-K | 380 | |
460 |
Thermal Expansion, µm/m-K | 21 | |
13 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 23 | |
38 |
Density, g/cm3 | 8.1 | |
8.1 |
Embodied Carbon, kg CO2/kg material | 2.6 | |
7.4 |
Embodied Energy, MJ/kg | 45 | |
100 |
Embodied Water, L/kg | 320 | |
200 |
Common Calculations
Stiffness to Weight: Axial, points | 7.0 | |
14 |
Stiffness to Weight: Bending, points | 19 | |
24 |
Strength to Weight: Axial, points | 11 to 22 | |
20 |
Strength to Weight: Bending, points | 13 to 21 | |
19 |
Thermal Shock Resistance, points | 11 to 22 | |
16 |
Alloy Composition
Aluminum (Al), % | 0 | |
0 to 0.35 |
Carbon (C), % | 0 | |
0 to 0.030 |
Chromium (Cr), % | 0 | |
14 to 19 |
Copper (Cu), % | 60 to 63 | |
0 |
Iron (Fe), % | 0 to 0.1 | |
28.5 to 47.5 |
Lead (Pb), % | 2.0 to 3.0 | |
0 |
Manganese (Mn), % | 0 | |
0 to 1.0 |
Molybdenum (Mo), % | 0 | |
2.5 to 5.5 |
Nickel (Ni), % | 0 | |
34 to 42 |
Niobium (Nb), % | 0 | |
0 to 0.1 |
Phosphorus (P), % | 0 | |
0 to 0.030 |
Silicon (Si), % | 0 | |
0 to 0.5 |
Sulfur (S), % | 0 | |
0 to 0.010 |
Titanium (Ti), % | 0 | |
2.0 to 3.0 |
Zinc (Zn), % | 33.4 to 38 | |
0 |
Residuals, % | 0 to 0.5 | |
0 |