MakeItFrom.com
Menu (ESC)

C49300 Brass vs. 7005 Aluminum

C49300 brass belongs to the copper alloys classification, while 7005 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (2, 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 C49300 brass and the bottom bar is 7005 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
70
Elongation at Break, % 4.5 to 20
10 to 20
Poisson's Ratio 0.31
0.33
Shear Modulus, GPa 40
26
Shear Strength, MPa 270 to 290
120 to 230
Tensile Strength: Ultimate (UTS), MPa 430 to 520
200 to 400
Tensile Strength: Yield (Proof), MPa 210 to 410
95 to 350

Thermal Properties

Latent Heat of Fusion, J/g 170
380
Maximum Temperature: Mechanical, °C 120
200
Melting Completion (Liquidus), °C 880
640
Melting Onset (Solidus), °C 840
610
Specific Heat Capacity, J/kg-K 380
880
Thermal Conductivity, W/m-K 88
140 to 170
Thermal Expansion, µm/m-K 20
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 15
35 to 43
Electrical Conductivity: Equal Weight (Specific), % IACS 17
110 to 130

Otherwise Unclassified Properties

Base Metal Price, % relative 26
9.5
Density, g/cm3 8.0
2.9
Embodied Carbon, kg CO2/kg material 3.0
8.3
Embodied Energy, MJ/kg 50
150
Embodied Water, L/kg 370
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 21 to 71
32 to 57
Resilience: Unit (Modulus of Resilience), kJ/m3 220 to 800
65 to 850
Stiffness to Weight: Axial, points 7.2
13
Stiffness to Weight: Bending, points 19
47
Strength to Weight: Axial, points 15 to 18
19 to 38
Strength to Weight: Bending, points 16 to 18
26 to 41
Thermal Diffusivity, mm2/s 29
54 to 65
Thermal Shock Resistance, points 14 to 18
8.7 to 18

Alloy Composition

Aluminum (Al), % 0 to 0.5
91 to 94.7
Antimony (Sb), % 0 to 0.5
0
Bismuth (Bi), % 0.5 to 2.0
0
Chromium (Cr), % 0
0.060 to 0.2
Copper (Cu), % 58 to 62
0 to 0.1
Iron (Fe), % 0 to 0.1
0 to 0.4
Lead (Pb), % 0 to 0.010
0
Magnesium (Mg), % 0
1.0 to 1.8
Manganese (Mn), % 0 to 0.030
0.2 to 0.7
Nickel (Ni), % 0 to 1.5
0
Phosphorus (P), % 0 to 0.2
0
Selenium (Se), % 0 to 0.2
0
Silicon (Si), % 0 to 0.1
0 to 0.35
Tin (Sn), % 1.0 to 1.8
0
Titanium (Ti), % 0
0.010 to 0.060
Zinc (Zn), % 30.6 to 40.5
4.0 to 5.0
Zirconium (Zr), % 0
0.080 to 0.2
Residuals, % 0
0 to 0.15