Nickel 200 vs. R30556 Alloy
Nickel 200 belongs to the nickel alloys classification, while R30556 alloy belongs to the iron alloys. They have a modest 21% of their average alloy composition in common, which, by itself, doesn't mean much. There are 30 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.
For each property being compared, the top bar is nickel 200 and the bottom bar is R30556 alloy.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 180 | |
210 |
Elongation at Break, % | 23 to 44 | |
45 |
Fatigue Strength, MPa | 120 to 350 | |
320 |
Poisson's Ratio | 0.31 | |
0.28 |
Shear Modulus, GPa | 70 | |
81 |
Shear Strength, MPa | 300 to 340 | |
550 |
Tensile Strength: Ultimate (UTS), MPa | 420 to 540 | |
780 |
Tensile Strength: Yield (Proof), MPa | 120 to 370 | |
350 |
Thermal Properties
Latent Heat of Fusion, J/g | 290 | |
300 |
Maximum Temperature: Mechanical, °C | 900 | |
1100 |
Melting Completion (Liquidus), °C | 1460 | |
1420 |
Melting Onset (Solidus), °C | 1440 | |
1330 |
Specific Heat Capacity, J/kg-K | 450 | |
450 |
Thermal Conductivity, W/m-K | 69 | |
11 |
Thermal Expansion, µm/m-K | 13 | |
15 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 18 | |
1.8 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 18 | |
1.9 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 65 | |
70 |
Density, g/cm3 | 8.9 | |
8.4 |
Embodied Carbon, kg CO2/kg material | 11 | |
8.7 |
Embodied Energy, MJ/kg | 150 | |
130 |
Embodied Water, L/kg | 230 | |
300 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 110 to 150 | |
290 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 42 to 370 | |
290 |
Stiffness to Weight: Axial, points | 11 | |
14 |
Stiffness to Weight: Bending, points | 21 | |
23 |
Strength to Weight: Axial, points | 13 to 17 | |
26 |
Strength to Weight: Bending, points | 14 to 17 | |
22 |
Thermal Diffusivity, mm2/s | 17 | |
2.9 |
Thermal Shock Resistance, points | 13 to 16 | |
18 |
Alloy Composition
Aluminum (Al), % | 0 | |
0.1 to 0.5 |
Boron (B), % | 0 | |
0 to 0.020 |
Carbon (C), % | 0 to 0.15 | |
0.050 to 0.15 |
Chromium (Cr), % | 0 | |
21 to 23 |
Cobalt (Co), % | 0 | |
16 to 21 |
Copper (Cu), % | 0 to 0.25 | |
0 |
Iron (Fe), % | 0 to 0.4 | |
20.4 to 38.2 |
Lanthanum (La), % | 0 | |
0.0050 to 0.1 |
Manganese (Mn), % | 0 to 0.35 | |
0.5 to 2.0 |
Molybdenum (Mo), % | 0 | |
2.5 to 4.0 |
Nickel (Ni), % | 99 to 100 | |
19 to 22.5 |
Niobium (Nb), % | 0 | |
0 to 0.3 |
Nitrogen (N), % | 0 | |
0.1 to 0.3 |
Phosphorus (P), % | 0 | |
0 to 0.040 |
Silicon (Si), % | 0 to 0.35 | |
0.2 to 0.8 |
Sulfur (S), % | 0 to 0.010 | |
0 to 0.015 |
Tantalum (Ta), % | 0 | |
0.3 to 1.3 |
Tungsten (W), % | 0 | |
2.0 to 3.5 |
Zinc (Zn), % | 0 | |
0.0010 to 0.1 |