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Nickel 80A vs. C83300 Brass

Nickel 80A belongs to the nickel alloys classification, while C83300 brass belongs to the copper alloys. There are 28 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 nickel 80A and the bottom bar is C83300 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
110
Elongation at Break, % 22
35
Poisson's Ratio 0.29
0.34
Shear Modulus, GPa 74
42
Tensile Strength: Ultimate (UTS), MPa 1040
220
Tensile Strength: Yield (Proof), MPa 710
69

Thermal Properties

Latent Heat of Fusion, J/g 320
200
Maximum Temperature: Mechanical, °C 980
180
Melting Completion (Liquidus), °C 1360
1060
Melting Onset (Solidus), °C 1310
1030
Specific Heat Capacity, J/kg-K 470
380
Thermal Conductivity, W/m-K 11
160
Thermal Expansion, µm/m-K 13
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.5
32
Electrical Conductivity: Equal Weight (Specific), % IACS 1.6
33

Otherwise Unclassified Properties

Base Metal Price, % relative 55
30
Density, g/cm3 8.3
8.8
Embodied Carbon, kg CO2/kg material 9.8
2.7
Embodied Energy, MJ/kg 140
44
Embodied Water, L/kg 280
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 210
60
Resilience: Unit (Modulus of Resilience), kJ/m3 1300
21
Stiffness to Weight: Axial, points 13
7.0
Stiffness to Weight: Bending, points 23
18
Strength to Weight: Axial, points 35
6.9
Strength to Weight: Bending, points 27
9.2
Thermal Diffusivity, mm2/s 2.9
48
Thermal Shock Resistance, points 31
7.9

Alloy Composition

Aluminum (Al), % 0.5 to 1.8
0
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 18 to 21
0
Copper (Cu), % 0
92 to 94
Iron (Fe), % 0 to 3.0
0
Lead (Pb), % 0
1.0 to 2.0
Manganese (Mn), % 0 to 1.0
0
Nickel (Ni), % 69.4 to 79.7
0
Silicon (Si), % 0 to 1.0
0
Sulfur (S), % 0 to 0.015
0
Tin (Sn), % 0
1.0 to 2.0
Titanium (Ti), % 1.8 to 2.7
0
Zinc (Zn), % 0
2.0 to 6.0
Residuals, % 0
0 to 0.7