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Nickel 890 vs. C85700 Brass

Nickel 890 belongs to the nickel alloys classification, while C85700 brass belongs to the copper alloys. There are 24 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.

For each property being compared, the top bar is nickel 890 and the bottom bar is C85700 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
100
Elongation at Break, % 39
17
Poisson's Ratio 0.28
0.31
Shear Modulus, GPa 78
40
Tensile Strength: Ultimate (UTS), MPa 590
310
Tensile Strength: Yield (Proof), MPa 230
110

Thermal Properties

Latent Heat of Fusion, J/g 330
170
Maximum Temperature: Mechanical, °C 1000
120
Melting Completion (Liquidus), °C 1390
940
Melting Onset (Solidus), °C 1340
910
Specific Heat Capacity, J/kg-K 480
380
Thermal Expansion, µm/m-K 14
21

Otherwise Unclassified Properties

Base Metal Price, % relative 47
24
Density, g/cm3 8.1
8.0
Embodied Carbon, kg CO2/kg material 8.2
2.8
Embodied Energy, MJ/kg 120
47
Embodied Water, L/kg 250
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 180
41
Resilience: Unit (Modulus of Resilience), kJ/m3 140
59
Stiffness to Weight: Axial, points 14
7.2
Stiffness to Weight: Bending, points 24
20
Strength to Weight: Axial, points 20
11
Strength to Weight: Bending, points 19
13
Thermal Shock Resistance, points 15
10

Alloy Composition

Aluminum (Al), % 0.050 to 0.6
0 to 0.8
Carbon (C), % 0.060 to 0.14
0
Chromium (Cr), % 23.5 to 28.5
0
Copper (Cu), % 0 to 0.75
58 to 64
Iron (Fe), % 17.3 to 33.9
0 to 0.7
Lead (Pb), % 0
0.8 to 1.5
Manganese (Mn), % 0 to 1.5
0
Molybdenum (Mo), % 1.0 to 2.0
0
Nickel (Ni), % 40 to 45
0 to 1.0
Niobium (Nb), % 0.2 to 1.0
0
Silicon (Si), % 1.0 to 2.0
0 to 0.050
Sulfur (S), % 0 to 0.015
0
Tantalum (Ta), % 0.1 to 0.6
0
Tin (Sn), % 0
0.5 to 1.5
Titanium (Ti), % 0.15 to 0.6
0
Zinc (Zn), % 0
32 to 40
Residuals, % 0
0 to 1.3