C66200 Brass vs. K93600 Alloy
C66200 brass belongs to the copper alloys classification, while K93600 alloy belongs to the iron alloys. There are 21 material properties with values for both materials. Properties with values for just one material (9, in this case) are not shown.
For each property being compared, the top bar is C66200 brass and the bottom bar is K93600 alloy.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 110 | |
140 |
Elongation at Break, % | 8.0 to 15 | |
5.0 to 35 |
Shear Strength, MPa | 270 to 300 | |
320 to 380 |
Tensile Strength: Ultimate (UTS), MPa | 450 to 520 | |
480 to 810 |
Tensile Strength: Yield (Proof), MPa | 410 to 480 | |
280 to 750 |
Thermal Properties
Maximum Temperature: Mechanical, °C | 180 | |
440 |
Melting Onset (Solidus), °C | 1030 | |
1430 |
Specific Heat Capacity, J/kg-K | 390 | |
520 |
Thermal Conductivity, W/m-K | 150 | |
13 |
Thermal Expansion, µm/m-K | 18 | |
7.3 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 35 | |
2.2 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 36 | |
2.4 |
Otherwise Unclassified Properties
Density, g/cm3 | 8.7 | |
8.1 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 40 to 66 | |
21 to 280 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 760 to 1030 | |
280 to 2050 |
Stiffness to Weight: Axial, points | 7.2 | |
9.4 |
Stiffness to Weight: Bending, points | 19 | |
21 |
Strength to Weight: Axial, points | 14 to 17 | |
16 to 28 |
Strength to Weight: Bending, points | 15 to 16 | |
17 to 24 |
Thermal Diffusivity, mm2/s | 45 | |
3.1 |
Thermal Shock Resistance, points | 16 to 18 | |
34 to 57 |