MakeItFrom.com
Menu (ESC)

C48500 Brass vs. 242.0 Aluminum

C48500 brass belongs to the copper alloys classification, while 242.0 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, 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 C48500 brass and the bottom bar is 242.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
73
Elongation at Break, % 13 to 40
0.5 to 1.5
Poisson's Ratio 0.31
0.33
Shear Modulus, GPa 39
27
Shear Strength, MPa 250 to 300
150 to 240
Tensile Strength: Ultimate (UTS), MPa 400 to 500
180 to 290
Tensile Strength: Yield (Proof), MPa 160 to 320
120 to 220

Thermal Properties

Latent Heat of Fusion, J/g 170
390
Maximum Temperature: Mechanical, °C 120
210
Melting Completion (Liquidus), °C 900
640
Melting Onset (Solidus), °C 890
530
Specific Heat Capacity, J/kg-K 380
870
Thermal Conductivity, W/m-K 120
130 to 170
Thermal Expansion, µm/m-K 21
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26
33 to 44
Electrical Conductivity: Equal Weight (Specific), % IACS 29
96 to 130

Otherwise Unclassified Properties

Base Metal Price, % relative 23
12
Density, g/cm3 8.1
3.1
Embodied Carbon, kg CO2/kg material 2.7
8.3
Embodied Energy, MJ/kg 46
150
Embodied Water, L/kg 330
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 56 to 140
1.3 to 3.4
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 500
110 to 340
Stiffness to Weight: Axial, points 7.1
13
Stiffness to Weight: Bending, points 19
45
Strength to Weight: Axial, points 14 to 17
16 to 26
Strength to Weight: Bending, points 15 to 17
23 to 32
Thermal Diffusivity, mm2/s 38
50 to 62
Thermal Shock Resistance, points 13 to 17
8.0 to 13

Alloy Composition

Aluminum (Al), % 0
88.4 to 93.6
Chromium (Cr), % 0
0 to 0.25
Copper (Cu), % 59 to 62
3.5 to 4.5
Iron (Fe), % 0 to 0.1
0 to 1.0
Lead (Pb), % 1.3 to 2.2
0
Magnesium (Mg), % 0
1.2 to 1.8
Manganese (Mn), % 0
0 to 0.35
Nickel (Ni), % 0
1.7 to 2.3
Silicon (Si), % 0
0 to 0.7
Tin (Sn), % 0.5 to 1.0
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 34.3 to 39.2
0 to 0.35
Residuals, % 0
0 to 0.15