MakeItFrom.com
Menu (ESC)

6005 Aluminum vs. C69300 Brass

6005 aluminum belongs to the aluminum alloys classification, while C69300 brass belongs to the copper 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 6005 aluminum and the bottom bar is C69300 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
110
Elongation at Break, % 9.5 to 17
8.5 to 15
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 26
41
Shear Strength, MPa 120 to 210
330 to 370
Tensile Strength: Ultimate (UTS), MPa 190 to 310
550 to 630
Tensile Strength: Yield (Proof), MPa 100 to 280
300 to 390

Thermal Properties

Latent Heat of Fusion, J/g 410
240
Maximum Temperature: Mechanical, °C 160
160
Melting Completion (Liquidus), °C 650
880
Melting Onset (Solidus), °C 610
860
Specific Heat Capacity, J/kg-K 900
400
Thermal Conductivity, W/m-K 180 to 200
38
Thermal Expansion, µm/m-K 23
19

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
8.0
Electrical Conductivity: Equal Weight (Specific), % IACS 180
8.8

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
26
Density, g/cm3 2.7
8.2
Embodied Carbon, kg CO2/kg material 8.3
2.7
Embodied Energy, MJ/kg 150
45
Embodied Water, L/kg 1180
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27 to 36
47 to 70
Resilience: Unit (Modulus of Resilience), kJ/m3 77 to 550
400 to 700
Stiffness to Weight: Axial, points 14
7.4
Stiffness to Weight: Bending, points 51
19
Strength to Weight: Axial, points 20 to 32
19 to 21
Strength to Weight: Bending, points 28 to 38
18 to 20
Thermal Diffusivity, mm2/s 74 to 83
12
Thermal Shock Resistance, points 8.6 to 14
19 to 22

Alloy Composition

Aluminum (Al), % 97.5 to 99
0
Chromium (Cr), % 0 to 0.1
0
Copper (Cu), % 0 to 0.1
73 to 77
Iron (Fe), % 0 to 0.35
0 to 0.1
Lead (Pb), % 0
0 to 0.090
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.1
0 to 0.1
Nickel (Ni), % 0
0 to 0.1
Phosphorus (P), % 0
0.040 to 0.15
Silicon (Si), % 0.6 to 0.9
2.7 to 3.4
Tin (Sn), % 0
0 to 0.2
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.1
18.4 to 24.3
Residuals, % 0
0 to 0.5