MakeItFrom.com
Menu (ESC)

C66300 Brass vs. 295.0 Aluminum

C66300 brass belongs to the copper alloys classification, while 295.0 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is C66300 brass and the bottom bar is 295.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
71
Elongation at Break, % 2.3 to 22
2.0 to 7.2
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 42
27
Shear Strength, MPa 290 to 470
180 to 230
Tensile Strength: Ultimate (UTS), MPa 460 to 810
230 to 280
Tensile Strength: Yield (Proof), MPa 400 to 800
100 to 220

Thermal Properties

Latent Heat of Fusion, J/g 200
400
Maximum Temperature: Mechanical, °C 180
170
Melting Completion (Liquidus), °C 1050
640
Melting Onset (Solidus), °C 1000
530
Specific Heat Capacity, J/kg-K 380
880
Thermal Conductivity, W/m-K 110
140
Thermal Expansion, µm/m-K 18
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
35
Electrical Conductivity: Equal Weight (Specific), % IACS 26
100

Otherwise Unclassified Properties

Base Metal Price, % relative 29
10
Density, g/cm3 8.6
3.0
Embodied Carbon, kg CO2/kg material 2.8
7.9
Embodied Energy, MJ/kg 46
150
Embodied Water, L/kg 320
1140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 17 to 98
5.2 to 13
Resilience: Unit (Modulus of Resilience), kJ/m3 710 to 2850
77 to 340
Stiffness to Weight: Axial, points 7.2
13
Stiffness to Weight: Bending, points 19
46
Strength to Weight: Axial, points 15 to 26
21 to 26
Strength to Weight: Bending, points 15 to 22
27 to 32
Thermal Diffusivity, mm2/s 32
54
Thermal Shock Resistance, points 16 to 28
9.8 to 12

Alloy Composition

Aluminum (Al), % 0
91.4 to 95.3
Cobalt (Co), % 0 to 0.2
0
Copper (Cu), % 84.5 to 87.5
4.0 to 5.0
Iron (Fe), % 1.4 to 2.4
0 to 1.0
Lead (Pb), % 0 to 0.050
0
Magnesium (Mg), % 0
0 to 0.030
Manganese (Mn), % 0
0 to 0.35
Phosphorus (P), % 0 to 0.35
0
Silicon (Si), % 0
0.7 to 1.5
Tin (Sn), % 1.5 to 3.0
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 6.0 to 12.8
0 to 0.35
Residuals, % 0
0 to 0.15