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SAE-AISI 1055 Steel vs. C69400 Brass

SAE-AISI 1055 steel belongs to the iron alloys classification, while C69400 brass belongs to the copper 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.

For each property being compared, the top bar is SAE-AISI 1055 steel and the bottom bar is C69400 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
110
Elongation at Break, % 11 to 14
17
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 72
42
Shear Strength, MPa 440 to 450
350
Tensile Strength: Ultimate (UTS), MPa 730 to 750
570
Tensile Strength: Yield (Proof), MPa 400 to 630
270

Thermal Properties

Latent Heat of Fusion, J/g 250
260
Maximum Temperature: Mechanical, °C 400
170
Melting Completion (Liquidus), °C 1460
920
Melting Onset (Solidus), °C 1420
820
Specific Heat Capacity, J/kg-K 470
410
Thermal Conductivity, W/m-K 51
26
Thermal Expansion, µm/m-K 12
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
6.2
Electrical Conductivity: Equal Weight (Specific), % IACS 12
6.7

Otherwise Unclassified Properties

Base Metal Price, % relative 1.8
27
Density, g/cm3 7.8
8.3
Embodied Carbon, kg CO2/kg material 1.4
2.7
Embodied Energy, MJ/kg 18
44
Embodied Water, L/kg 46
300

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 80 to 85
80
Resilience: Unit (Modulus of Resilience), kJ/m3 440 to 1070
340
Stiffness to Weight: Axial, points 13
7.4
Stiffness to Weight: Bending, points 24
19
Strength to Weight: Axial, points 26
19
Strength to Weight: Bending, points 23
18
Thermal Diffusivity, mm2/s 14
7.7
Thermal Shock Resistance, points 23 to 24
20

Alloy Composition

Carbon (C), % 0.5 to 0.6
0
Copper (Cu), % 0
80 to 83
Iron (Fe), % 98.4 to 98.9
0 to 0.2
Lead (Pb), % 0
0 to 0.3
Manganese (Mn), % 0.6 to 0.9
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0
3.5 to 4.5
Sulfur (S), % 0 to 0.050
0
Zinc (Zn), % 0
11.5 to 16.5
Residuals, % 0
0 to 0.5