Type 4 Magnetic Alloy vs. C17500 Copper
Type 4 magnetic alloy belongs to the nickel alloys classification, while C17500 copper belongs to the copper alloys. There are 28 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 Type 4 magnetic alloy and the bottom bar is C17500 copper.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 120 |
| Elongation at Break, % | 2.0 to 40 | |
| 6.0 to 30 |
| Fatigue Strength, MPa | 220 to 400 | |
| 170 to 310 |
| Poisson's Ratio | 0.31 | |
| 0.34 |
| Shear Modulus, GPa | 73 | |
| 45 |
| Shear Strength, MPa | 420 to 630 | |
| 200 to 520 |
| Tensile Strength: Ultimate (UTS), MPa | 620 to 1100 | |
| 310 to 860 |
| Tensile Strength: Yield (Proof), MPa | 270 to 1040 | |
| 170 to 760 |
Thermal Properties
| Latent Heat of Fusion, J/g | 290 | |
| 220 |
| Maximum Temperature: Mechanical, °C | 900 | |
| 220 |
| Melting Completion (Liquidus), °C | 1420 | |
| 1060 |
| Melting Onset (Solidus), °C | 1370 | |
| 1020 |
| Specific Heat Capacity, J/kg-K | 440 | |
| 390 |
| Thermal Expansion, µm/m-K | 11 | |
| 18 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.9 | |
| 24 to 53 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 3.0 | |
| 24 to 54 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 60 | |
| 60 |
| Density, g/cm3 | 8.8 | |
| 8.9 |
| Embodied Carbon, kg CO2/kg material | 10 | |
| 4.7 |
| Embodied Energy, MJ/kg | 140 | |
| 73 |
| Embodied Water, L/kg | 210 | |
| 320 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 22 to 200 | |
| 30 to 120 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 190 to 2840 | |
| 120 to 2390 |
| Stiffness to Weight: Axial, points | 12 | |
| 7.5 |
| Stiffness to Weight: Bending, points | 22 | |
| 18 |
| Strength to Weight: Axial, points | 19 to 35 | |
| 9.7 to 27 |
| Strength to Weight: Bending, points | 18 to 27 | |
| 11 to 23 |
| Thermal Shock Resistance, points | 21 to 37 | |
| 11 to 29 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 0 to 0.2 |
| Beryllium (Be), % | 0 | |
| 0.4 to 0.7 |
| Carbon (C), % | 0 to 0.050 | |
| 0 |
| Chromium (Cr), % | 0 to 0.3 | |
| 0 |
| Cobalt (Co), % | 0 to 0.5 | |
| 2.4 to 2.7 |
| Copper (Cu), % | 0 to 0.3 | |
| 95.6 to 97.2 |
| Iron (Fe), % | 9.5 to 17.5 | |
| 0 to 0.1 |
| Manganese (Mn), % | 0 to 0.8 | |
| 0 |
| Molybdenum (Mo), % | 3.5 to 6.0 | |
| 0 |
| Nickel (Ni), % | 79 to 82 | |
| 0 |
| Phosphorus (P), % | 0 to 0.010 | |
| 0 |
| Silicon (Si), % | 0 to 0.5 | |
| 0 to 0.2 |
| Sulfur (S), % | 0 to 0.020 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.5 |