
EFINEA Metals is a proud distributor of Hiperco® 50, Hiperco® 50A, and Hiperco® 50 HS soft magnetic alloys. This iron-cobalt-vanadium family reaches among the highest magnetic saturation of any commercially produced soft magnetic material, with flux density approaching 2.3 Tesla at 16,000 A/m. That capability lets engineers reduce the mass of a magnetic circuit while maintaining output.
We stock Hiperco® 50A as plate and round bar, and supply Hiperco® 50, Hiperco® 50A, and Hiperco® 50 HS as strip and coil. Precision cutting to your specifications is available, with no minimum order size.
Choosing Between Hiperco® 50, 50A, and 50 HS
Your selection usually comes down to what the part has to survive. If the component is a static core or a stator operating at moderate stress, Hiperco® 50 alloy covers the requirement at the best value. If the design is loss-sensitive or needs the highest permeability the family offers, Hiperco® 50A alloy is the stronger candidate. If the part is a spinning rotor lamination or a magnetic bearing element carrying mechanical load, Hiperco® 50 HS is ideal because its strength can be fine-tuned during final annealing.
Section thickness also matters. Thinner strip reduces eddy-current losses at higher frequencies, as shown in the AC core loss tables below. Bulk bar behaves differently again, with markedly lower permeability than strip of the same chemistry.
Hiperco® 50 Properties
The tables in this section cover the magnetic, physical, and mechanical behavior of Hiperco® 50. For downloadable data sheets on this or any of the soft magnetic alloys we stock, visit the Data Sheets section of our Technical Library.
DC Magnetic Properties
DC magnetic data describes how the alloy responds to a steady applied field. Coercivity indicates how much reverse field is needed to bring the material back to zero magnetization, so lower values mean the core is easier to cycle. Maximum DC relative permeability shows how efficiently the material amplifies an applied field. The flux density columns list the induction reached at each field strength in A/m.
Hiperco® 50 Typical DC Magnetic Properties |
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|---|---|---|---|---|---|---|---|---|
| Heat Treatment | Coercivity (A/m) from 8 k/A/m | DC Relative Permeability µ max | B (Tesla) A/m | |||||
| 400 | 800 | 1600 | 4000 | 6000 | 16000 | |||
| 0.014" Strip | ||||||||
| Standard Ferromagnetic Anneal | 40 | 19200 | 2.12 | 2.19 | 2.23 | 2.27 | 2.28 | 2.30 |
| Standard Mechanical Anneal | 125 | 7900 | 2.01 | 2.12 | 2.19 | 2.25 | 2.28 | 2.29 |
| 0.006" Strip | ||||||||
| Standard Ferromagnetic Anneal | 50 | 15000 | 2.03 | 2.14 | 2.21 | 2.27 | 2.28 | 2.30 |
| Standard Mechanical Anneal | 125 | 7400 | 1.99 | 2.11 | 2.18 | 2.25 | 2.28 | 2.29 |
| Source: Carpenter Electrification® Hiperco® 50 data sheet 5/20 | ||||||||
AC Core Loss
Core loss is the energy dissipated as heat each time the magnetic field reverses, and it increases steeply with frequency. The table lists specific core loss in watts per pound at 60, 400, and 1000 Hz for two strip thicknesses and two heat treatments, measured at induction levels of 1.0, 1.5, and 2.0 Tesla.
Ferromagnetically annealed material loses considerably less energy than mechanically annealed material under every condition.
Hiperco® 50 Typical AC Core Loss By Heat Treatment |
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|---|---|---|---|---|---|---|---|
| Heat Treatment | 0.014" Strip Specific Core Loss | 0.006" Strip Specific Core Loss | B (Tesla) | ||||
| 60 Hz | 400 Hz | 1000 Hz | 60 Hz | 400 Hz | 1000 Hz | ||
| Standard Ferromagnetic Anneal | 1.11 | 13.3 | 54.1 | 1.17 | 10.2 | 33.9 | 1.0 |
| 2.03 | 29.8 | 142.0 | 2.08 | 19.2 | 65.8 | 1.5 | |
| 3.29 | 56.7 | 301.0 | 3.32 | 30.9 | 109.0 | 2.0 | |
| Standard Mechanical Anneal | 2.48 | 23.0 | 80.2 | 2.17 | 16.7 | 46.2 | 1.0 |
| 4.47 | 47.5 | 191.0 | 3.96 | 31.1 | 93.8 | 1.5 | |
| 7.16 | 84.5 | 388.0 | 6.54 | 51.4 | 157.0 | 2.0 | |
| Source: Carpenter Electrification® Hiperco® 50 data sheet 5/20 | |||||||
Physical and Thermal Properties
Physical properties describe the bulk behavior of the alloy independent of the applied field. The Curie temperature of 938°C (1720°F) marks the point at which the material loses its magnetic ordering and sets the ceiling for any magnetic application. Electrical resistivity of 40.1 × 10⁻⁸ ohm-m limits eddy currents within each lamination.
The thermal conductivity of 29.83 W/m°C governs how readily heat escapes a core, while the coefficient of thermal expansion is listed across four temperature ranges because it rises with temperature.
Hiperco® 50 Typical Physical Properties |
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|---|---|---|
| Density | lb/in3 | 0.293 |
| Specific Gravity | 68°F | 8.12 |
| *Curie Temperature | °F | 1720 |
| °C | 938 | |
| Electrical Resistivity | ||
| (70°F) | ohm-cir mil/ft | 241.0 |
| (21°C) | ohm-m | 40.1x10-8 |
| Elastic Modulus | ksi | 30x103 |
| GPa | 206.8 | |
| Thermal Conductivity | BTU-in/sq. ft-hr- °F | 206.8 |
| W/m °C | 29.83 | |
| Mean Coefficient of Thermal Expansion | ||
| 77 to 392°F | 5.3x10-6 | |
| 77 to 752°F | 5.6x10-6 length/length/°F | |
| 77 to 1112°F | 5.8x10-6 length/length/°F | |
| 77 to 1472°F | 6.3x10-6 length/length/°F | |
| *Curie temperature is phase transition from magnetic to non-magnetic phase. | ||
| Source: Carpenter Electrification® Hiperco® 50 data sheet 5/20 | ||
Mechanical Properties
Mechanical values shift dramatically with heat treatment. Cold-rolled, unannealed strip reaches 190 ksi ultimate tensile strength at 36 HRC but offers only 2% elongation, limiting forming. A standard magnetic anneal softens the material to 115 ksi ultimate with 5 to 15% elongation, releasing the internal stress that degrades magnetic performance. A mechanical anneal lands between the two at 135 ksi. Parts are normally stamped or machined in the harder condition and then annealed as a final operation.
Hiperco® 50 Typical Mechanical Properties - 0.014" Strip |
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|---|---|---|---|---|
| Heat Treatment | Cold Rolled Unannealed | Std. Magnetic Anneal | Std. Mechanical Anneal | |
| Ultimate Tensile Strength | ksi (MPa) | 190 (1310) | 115 (792) | 135 (930) |
| Yield Strength 0.2% | ksi (MPa) | 175 (1270) | 48 (331) | 60 (414) |
| Elongation | % in 2 in. | 2 | 5-15 | 5-15 |
| Hardness | Rockwell C | 36 | .. | .. |
| Source: Carpenter Electrification® Hiperco® 50 data sheet 5/20 | ||||
Hiperco® 50A Properties
Hiperco® 50A is a low-carbon, high-permeability member of the family. The tables below separate strip data from bar data, since form has a large effect on magnetic response.
DC Magnetic Properties, Strip and Bar
In annealed 0.014″ strip, Hiperco® 50A reaches a coercivity of 30 A/m with maximum DC relative permeability of 22,000, an improvement over standard Hiperco® 50 on both counts. Bulk bar tells a different story: coercivity rises to 209 A/m and maximum permeability falls to 3,350, though saturation flux density at 16,000 A/m still reaches 2.30 Tesla.
Engineers specifying Hiperco® 50A round bar for a solid pole piece should design around the bar figures rather than the strip figures.
Hiperco® 50A Typical DC Magnetic Properties - 0.014" Strip |
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|---|---|---|---|---|---|---|---|---|
| Heat Treatment | Coercivity (A/m) from 8 kA/m | DC Relative Permeability µ max | B (Tesla) A/m | |||||
| 400 | 800 | 1600 | 4000 | 8000 | 1600 | |||
| Standard Ferromagnetic Annealing | 30 | 22000 | 2.12 | 2.19 | 2.23 | 2.27 | 2.28 | 2.30 |
| Source: Carpenter Electrification® Hiperco® 50A data sheet 5/20 | ||||||||
Hiperco® 50A Typical DC Magnetic Properties - Bar (Bulk Material) |
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|---|---|---|---|---|---|---|---|---|
| Heat Treatment | Coercivity (A/m) from 8 kA/m | DC Relative Permeability µ max | B (Tesla) A/m | |||||
| 400 | 800 | 1600 | 4000 | 8000 | 1600 | |||
| Standard Ferromagnetic Annealing | 209 | 3350 | 1.49 | 1.80 | 2.00 | 2.18 | 2.25 | 2.30 |
| Source: Carpenter Electrification® Hiperco® 50A data sheet 5/20 | ||||||||
AC Core Loss
Core loss for annealed Hiperco® 50A strip runs below that of comparably treated Hiperco® 50 at 60 Hz and 400 Hz, reflecting the cleaner chemistry. The three rows correspond to induction levels of 1.0, 1.5, and 2.0 Tesla.
Hiperco® 50A Typical AC Core Loss By Heat Treatment - 0.014" Strip |
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|---|---|---|---|
| Heat Treatment | Specific Core Loss | ||
| 60 Hz | 400 Hz | 1000 Hz | |
| Standard Ferromagnetic Annealing | 0.94 | 12.7 | 55.6 |
| 1.75 | 30.0 | 151.0 | |
| 2.73 | 56.8 | 313.0 | |
| Source: Carpenter Electrification® Hiperco® 50A data sheet 5/20 | |||
Physical and Thermal Properties
Physical properties for Hiperco® 50A track closely with Hiperco® 50. Density, specific gravity, Curie temperature, elastic modulus, and thermal conductivity are effectively identical, and electrical resistivity differs only marginally at 240.7 ohm-cir mil/ft.
Thermal expansion behaves the same way across the four listed ranges. Substituting Hiperco® 50A for Hiperco® 50 therefore rarely disturbs the thermal or dimensional side of a design.
Hiperco® 50A Typical Physical Properties |
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|---|---|---|
| Density | lb/in3 | 0.293 |
| Specific Gravity | 68°F | 8.12 |
| *Curie Temperature | °F | 1720 |
| °C | 938 | |
| Electrical Resistivity | ||
| (70°F) | ohm-cir mil/ft | 240.7 |
| (21°C) | ohm-m | 40.1x10-8 |
| Elastic Modulus | ksi | 30x103 |
| GPa | 206.8 | |
| Thermal Conductivity | BTU-in/sq. ft-hr- °F | 206.8 |
| W/cm °C | 29.83 | |
| Mean Coefficient of Thermal Expansion | ||
| 77 to 392°F | 5.3x10-6 length/length/°F | |
| 77 to 752°F | 5.6x10-6 length/length/°F | |
| 77 to 1112°F | 5.8x10-6 length/length/°F | |
| 77 to 1472°F | 6.3x10-6 length/length/°F | |
| *Curie temperature is phase transition from magnetic to non-magnetic phase. | ||
| Source: Carpenter Electrification® Hiperco® 50A data sheet 5/20 | ||
Mechanical Properties
The mechanical spread between conditions is wider for Hiperco® 50A than for Hiperco® 50. Cold rolled unannealed strip reaches 195 ksi ultimate tensile strength with 1% elongation, while the standard magnetic anneal reduces that to 72.2 ksi with 6.7% elongation. The low annealed strength reflects the priority placed on magnetic performance in this grade, so parts under mechanical load generally need either a design allowance or a move to Hiperco® 50 HS.
Hiperco® 50A Typical Mechanical Properties - 0.014" Strip |
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|---|---|---|---|
| Heat Treatment | Cold Rolled Unannealed | Standard Magnetic Anneal | |
| Ultimate Tensile Strength | ksi (MPa) | 195 (1344) | 72.2 (498) |
| Yield Strength 0.2% | ksi (MPa) | 185 (1276) | 30.8 (202) |
| Elongation | % in 2 in. | 1 | 6.7 |
| Source: Carpenter Electrification® Hiperco® 50A data sheet 5/20 | |||
Hiperco® 50 HS Properties
Hiperco® 50 HS is the high-strength variant, developed for rotating parts that must hold together under centrifugal load while still carrying high flux.
DC Magnetic Properties by Strength Level
This table is organized differently from the others because it shows the trade curve directly. Each row pairs a 0.2% yield strength with the flux density that material achieves at five field strengths, measured on ring laminations per ASTM A596/A596M. Raising yield strength from 73 ksi to 99 ksi costs about 1.1 kG of flux density at 800 A/m, though the penalty nearly vanishes at higher field strengths where all three conditions converge near 2.29 Tesla.
Designers use this relationship to pick the lowest strength level that satisfies the mechanical case, preserving magnetic headroom.
Hiperco® 50 HS Typical DC Magnetic Properties - 1.50 O.D. x 1.25" I.D. Ring Laminations ASTM Method A596/A596M |
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|---|---|---|---|---|---|---|---|---|---|---|---|
| 0.2 % Yield Strength | Flux Density at Indicated Magnetic Field Strength | ||||||||||
| 10 Oe 800 A/m | 20 Oe 1600 A/m | 50 Oe 4000 A/m | 100 Oe 8000 A/m | 200 Oe 16000 A/m | |||||||
| ksi, | MPa | kG | T | kG | T | kG | T | kG | T | kG | T |
| 73 | 503 | 19.3 | 1.93 | 20.7 | 2.07 | 21.9 | 2.19 | 22.3 | 2.23 | 23.0 | 2.30 |
| 86 | 593 | 19.0 | 1.90 | 20.3 | 2.03 | 21.8 | 2.18 | 22.3 | 2.23 | 22.9 | 2.29 |
| 99 | 683 | 18.2 | 1.82 | 19.9 | 1.99 | 21.5 | 2.15 | 22.3 | 2.23 | 22.9 | 2.29 |
| Source: Carpenter Electrification® Hiperco 50® HS data sheet 5/20 |
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Physical and Thermal Properties
Hiperco® 50 HS shares the density, Curie temperature, and thermal behavior of the other grades. The one meaningful difference is electrical resistivity, which rises to 253.0 ohm-cir mil/ft (42.1 ohm-m) because of the added columbium/niobium. Higher resistivity modestly suppresses eddy currents, a small bonus in a grade selected primarily for strength.
Hiperco® 50 HS Typical Physical Properties |
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|---|---|---|
| Density | lb/in3 | 0.293 |
| Specific Gravity | 68°F | 8.12 |
| *Curie Temperature | °F | 1720 |
| °C | 938 | |
| Electrical Resistivity | ||
| (70°F) | ohm-cir mil/ft | 253.0 |
| (21°C) | ohm-m | 42.1 |
| Elastic Modulus | ksi | 30x103 |
| GPa | 206.8 | |
| Thermal Conductivity | BTU-in/sq. ft-hr- °F | 206.8 |
| W/m/°C | 29.83 | |
| Mean Coefficient of Thermal Expansion | ||
| 77 to 392°F | 5.3x10-6 length/length/°F | |
| 77 to 752°F | 5.6x10-6 length/length/°F | |
| 77 to 1112°F | 5.8x10-6 length/length/°F | |
| 77 to 1472°F | 6.3x10-6 length/length/°F | |
| *Curie temperature is phase transition from magnetic to non-magnetic phase. | ||
| Source: Carpenter Electrification® Hiperco 50® HS data sheet 5/20 | ||
Mechanical Properties by Heat Treatment
This table maps ten combinations of annealing temperature and hold time to the resulting yield strength, tensile strength, and elongation in 0.006″ strip. Yield strength falls steadily as either temperature or time increases, ranging from 99 ksi after one hour at 720°C down to 64 ksi after four hours at 800°C.
All listed treatments were run in batch furnaces under dry hydrogen with a one-hour heat-up and a controlled 180°F/hr cool. Reproducing these values depends on matching that atmosphere and cooling rate, so heat treaters should treat the footnote as part of the specification.
Hiperco® 50 HS Typical Mechanical Properties - 0.006" Strip |
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|---|---|---|---|---|---|---|---|
| Heat Treatment Temperatures | 0.2 % Yield Strength | Ultimate Tensile Strength | Elongation in 2" (50.8MM) | ||||
| °F | °C | Time, HR | ksi | MPa | ksi | MPa | % |
| 1328 | 720 | 1 | 99 | 683 | 185 | 1280 | 15 |
| 1328 | 720 | 2 | 94 | 648 | 177 | 1220 | 14 |
| 1328 | 720 | 4 | 87 | 600 | 156 | 1080 | 11 |
| 1364 | 740 | 1 | 86 | 593 | 168 | 1160 | 13 |
| 1364 | 740 | 2 | 83 | 572 | 167 | 1150 | 13 |
| 1364 | 740 | 4 | 78 | 538 | 158 | 1090 | 12 |
| 1400 | 760 | 1 | 76 | 524 | 149 | 1030 | 11 |
| 1400 | 760 | 2 | 76 | 524 | 166 | 1140 | 14 |
| 1400 | 760 | 4 | 73 | 503 | 145 | 1000 | 11 |
| 1472 | 800 | 4 | 64 | 441 | 142 | 979 | 11 |
| The tensile properties are for strips heat treated at room temperature. All heat treatments conducted in batch type furnaces (1 hour heat up time) in dry hydrogen followed by cooling rate of 180°F/hr. | |||||||
| Source: Carpenter Electrification® Hiperco 50® HS data sheet 5/20 |
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Hiperco® 50, 50A, 50 HS Chemistry
The chemistry table shows the nominal composition for all three grades side by side. Cobalt sits near 48.5% across the family and supplies the high saturation. Vanadium, around 1.9 to 2.0%, raises resistivity and improves hot workability.
The real differences are in the trace elements: Hiperco® 50A cuts carbon by an order of magnitude to 0.001% and drops columbium/niobium to 0.01%, both of which reduce magnetic losses. Hiperco® 50 HS moves the other way, raising columbium/niobium to 0.30% to pin grain boundaries and build strength.
Chemistry | Hiperco® 50 | Hiperco® 50A | Hiperco® 50 HS |
|---|---|---|---|
| Carbon | 0.01 | 0.001 | 0.01 |
| Manganese | 0.05 | 0.05 | 0.05 |
| Silicon | 0.05 | 0.05 | 0.05 |
| Columbium/Niobium | 0.05 | 0.01 | 0.30 |
| Cobalt | 48.5 | 48.5 | 48.75 |
| Vanadium | 1.90 | 2.00 | 1.90 |
| Iron | Remainder | Remainder | Remainder |
| Source: Carpenter Electrification® Hiperco® 50, 50A, 50 HS data sheets | |||
Hiperco® 50, 50A, 50 HS Specifications
All three grades meet ASTM A801 Type 1, the standard covering wrought iron-cobalt high-magnetic-saturation alloys.
Hiperco® 50 carries the additional UNS designation R30005 Type 1 and, along with Hiperco® 50A, conforms to MIL-A-47182 for defense procurement. Specifying by standard rather than by trade name alone provides purchasing with a fallback path and supports audit requirements for regulated programs.
Hiperco® 50, 50A, 50 HS Specifications | ||||
|---|---|---|---|---|
| Hiperco 50 | ASTM A801 Type 1 | UNS R30005 Type 1 | MIL A 47182 | |
| Hiperco 50A | ASTM A801 Type 1 | MIL A 47182 | ||
| Hiperco 50 HS | ASTM A801 Type 1 | |||
For additional information on specifications of the materials distributed by EFINEA, please visit the websites of the international organizations that develop and publish technical standards: ASTM International and ASM International.
Hiperco® Applications
High magnetic saturation enables any designer to achieve a given magnetic output with a smaller, lighter core, and that single advantage drives most Hiperco® applications.
ED FAGAN INC. supplies the highest quality special purpose metals and alloys for Aerospace/Aviation, Defense, Electronics, Magnetic, Medical, Lighting, Optical, Telecommunications, Ceramics, Heat Treating, and other high-technology industries.
CarTech® Hiperco® 50, 50A, 50 HS are registered trademarks of CRS Holdings, Inc., Delaware.
Hiperco® 50 is used in the rotors and stators of aircraft electrical generators, including the ram air turbine (RAT) and the auxiliary power unit (APU) that serve as backup power on commercial aircraft.
The value of that hardware was demonstrated on January 15, 2009, when US Airways Flight 1549 lost power in both main engines after being struck by birds shortly after takeoff from LaGuardia. The aircraft’s RAT and APU generators, built with Hiperco® 50 rotors and stators, supplied the emergency power that allowed Captain Sullenberger to control the aircraft through its landing on the Hudson River.
The engine-driven generators on that airframe also contain Hiperco® 50, though they stopped producing power once the main engines failed.
Beyond emergency systems, the same properties support main engine generators, starter-generators, and the power electronics of more-electric aircraft architectures, where increasing electrical load per airframe puts a premium on power density.
Hiperco® 50A alloy is specified for magnetic cores in electrical equipment that requires high permeability at high magnetic flux densities. It also appears in tape-wound cores, where the combination of low AC loss and high permeability at high induction is the deciding factor. Transformers, inductors, and current sensors in aerospace and industrial power conversion all draw on this construction.
Hiperco® 50 HS strip is ideal for rotor laminations in aircraft power generation and for magnetic bearing components. Laminations are stamped from cold-rolled strip, then final annealed in a protective atmosphere or vacuum at a temperature chosen to balance magnetic and mechanical performance so the part can withstand service stress.
In magnetic bearings, the rotor floats on a controlled magnetic field with no physical contact, eliminating lubrication and mechanical wear for high-speed compressors, flywheel energy storage, and turbomachinery.
The reduced core mass available with Hiperco® alloy benefits high-performance motors and electromagnetic actuators across defense and industrial equipment.
Applications include servo and torque motors, solenoid pole pieces, relay armatures, magnetic clutches, and electromagnet cores. Directed-energy hardware and pulsed-power systems also use the family, where a compact magnetic circuit must handle heavy flux.
Cobalt-iron alloys are used in the magnetic circuits of imaging and radiation therapy equipment, including the pole pieces and focusing structures that shape and steer beams. Particle accelerators and beam-line magnets in research settings rely on the same characteristic: a higher-saturation material allows a stronger field from a smaller magnet, reducing both the footprint and the structural support needed.
For more on engineering and advanced materials applications, visit the IEEE website.
Annealing and Machining
Final ferromagnetic annealing is what unlocks the magnetic performance in every table above, and it is normally performed after all forming and machining is complete. Our Ferromagnetic Annealing Guide for Hiperco® 50, 50A & 50 HS covers recommended cycles, and our Machining Hiperco® 50A guide covers tooling and technique for the pre-anneal condition.
Available Hiperco® Forms
Related soft magnetic alloys: EFINEA Alloy 50, EFINEA Alloy 79, and Core Iron (VIM VAR).
Why Work With EFINEA?
Among Hiperco® 50 and 50A suppliers, EFINEA combines stocked inventory with material traceable to the original mill, including heat and lot numbers, chemical analysis, mechanical properties, and the applicable specification. Our facilities meet ISO 9001:2015 and AS9100D requirements, which matter in aerospace and defense programs where documentation is audited.
Our team is trained in the properties and attributes of the materials we sell and can walk you through grade selection before you commit to a purchase.
Frequently Asked Questions About Hiperco® Alloy
Silicon steel saturates near 2.0 Tesla and costs far less, making it the default for utility transformers and industrial motors where mass is not a constraint. Nickel-iron alloys such as EFINEA Alloy 79 offer very high permeability at low field strengths but saturate at around 0.8 Tesla, making them ideal for shielding and low-signal work. Hiperco® alloy lies at the high-saturation end of the range, and its cobalt content makes it the most expensive of the group. The justification is almost always weight or volume savings in a system where those carry a high price.
Thickness is driven mainly by operating frequency. At 60 Hz, 0.014″ strip is usually adequate. As frequency climbs toward 400 Hz and beyond, eddy current losses scale sharply and thinner material, such as 0.006″ strip pays for itself in reduced heating. Thinner laminations do raise stamping and stacking costs, so the practical answer balances loss against manufacturing effort.
Cobalt-iron alloys contain no chromium and will rust in humid or corrosive environments, so exposed parts usually need a protective finish. Laminations are often coated with an insulating oxide or organic layer that serves double duty by reducing interlaminar eddy currents. Discuss any surface treatment plan alongside the annealing cycle, since some coatings will not survive a high-temperature hydrogen anneal.
Annealing is typically performed by the part manufacturer or a specialist heat treater after forming, since the cycle depends on the finished geometry and the balance of magnetic and mechanical properties the part requires. We supply material in the condition you specify and provide annealing guidance through our Technical Library. Contact us to discuss what makes sense for your process.

