Mu-metal Ni-Fe-Mo
Nickel-iron-molybdenum soft magnetic alloy, nominal 80 % Ni and 5 % Mo by weight, balance Fe, with Mn 0.50 % and Si 0.15 % nominal (CarTech HyMu 800 type analysis)
Also known as UNS N14080, DIN 17745, JIS C 2531, ASTM A753, MuMETAL, Mumetall · 1 more
Mu-metal is a soft nickel-iron-molybdenum alloy, nominally 80 % Ni and 5 % Mo (ASTM A753 Alloy 4), used to shield sensitive electronics from static and low-frequency magnetic fields.
Evidence level
2 of 5
Lab-measured
- 0Predicted only. No one has made it, or no measurement exists.
- 1Calculated. Only calculated or predicted values from sources.
- 2Lab-measured. Measured properties with their conditions stated.
- 3Space-relevant tests. Measured in conditions relevant to space, such as vacuum or atomic oxygen.
- 4Ground-qualified. Qualified for an application on the ground.
- 5Flown or field-proven. Flight or field results exist.
Shield a field
400000 DC permeability
Saturate at low field
0.75 T
Weight
8.7 g/cm3
Strength when annealed
530 MPa tensile
Recipe, share of the weight
- Ni nominal, 80.00 % in the type analysisNickel
- Mo nominal, 5.00 % in the type analysisMolybdenum
- Mn nominal, 0.50 %Manganese
- Si nominal, 0.15 %Silicon
- Fe balanceIron
Best for
Shielding sensitive electronics from static and low-frequency fields: DC permeability of at least 400,000 and AC permeability of at least 75,000 at 60 Hz in the MuMETAL sheet datasheet
Weakest at
Strength and weight: 160 MPa yield in the final annealed state and 8.7 g/cm3 density, and the permeability falls after shock or plastic strain, which needs a re-anneal to recover
Risk at a glance
- People Low. Nickel classes
- If it fails Moderate. Permeability loss from shock or plastic strain
- Corrosion Low. The high nickel content lets the alloy be used without a corrosion-resistant coating.
Quick facts: Ni-Fe-Mo
| Property | Value | Basis |
|---|---|---|
| Density | 8.7 to 8.75 g/cm³ | 2 sourced values across conditions |
| Yield strength | 160 to 450 MPa | 2 sourced values across conditions |
| Tensile strength | 500 to 700 MPa | 3 sourced values across conditions |
| Young's modulus | 190 to 221 GPa | 1 sourced value |
| Thermal conductivity | 19 W/(m·K) | 2 sourced values across conditions |
| Thermal expansion (CTE) | 12 ppm/K | 1 sourced value |
| Melting point | 1,450 °C | 1 sourced value |
| Specific heat | 460 J/(kg·K) | 1 sourced value |
| Electrical resistivity | 6.0e-7 Ω·m | 2 sourced values across conditions |
What is the density of Mu-metal (Ni-Fe-Mo)?
Mu-metal (Ni-Fe-Mo) has a density of 8.7 to 8.75 g/cm³. The range covers 2 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.
What is the thermal conductivity of Mu-metal (Ni-Fe-Mo)?
Mu-metal (Ni-Fe-Mo) has a thermal conductivity of 19 W/(m·K). The range covers 2 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.
What is the coefficient of thermal expansion of Mu-metal (Ni-Fe-Mo)?
Mu-metal (Ni-Fe-Mo) has a coefficient of thermal expansion of 12 ppm/K. The source and test conditions are listed in the properties table on this page.
What is the melting point of Mu-metal (Ni-Fe-Mo)?
Mu-metal (Ni-Fe-Mo) has a melting point of 1,450 °C. The source and test conditions are listed in the properties table on this page.
What is the yield strength of Mu-metal (Ni-Fe-Mo)?
Mu-metal (Ni-Fe-Mo) has a yield strength of 160 to 450 MPa. The range covers 2 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.
What are the other names and codes for Mu-metal (Ni-Fe-Mo)?
Mu-metal (Ni-Fe-Mo) is also written as UNS N14080, DIN 17745, JIS C 2531, ASTM A753, MuMETAL, Mumetall. Each code is printed in the source listed beside it in the designations table.
What is Mu-metal (Ni-Fe-Mo) used for?
Uses recorded in the sources include Magnetic shielding for sensitive electronics, current sensors and current transformer cores; Relays, stepper motors and magnetic sensors; Spacecraft magnetic cleanliness, soft magnetic parts near magnetometers.
Why it exists
Mu-metal is used to shield sensitive electronics from static and low-frequency magnetic fields. It is a soft nickel-iron-molybdenum alloy with nominal 80 % Ni and 5 % Mo, and its high permeability gives a low-reluctance path for the field. The MuMETAL sheet datasheet gives a DC permeability of at least 400,000 at 0.005 Oe and an AC permeability of at least 75,000 at 60 Hz. The saturation induction is 0.75 T, and the Curie temperature is 420 °C. The sources read give it a yield strength of 160 MPa in the final annealed state, so it is chosen for its magnetic performance, not for its strength.
Where it's used
Magnetic shields and sensors
MuMETAL is used in high quality magnetic shielding, current sensors and high precision current transformer cores. Permimphy is used for relays, stepper motors and magnetic sensors.
Spacecraft magnetic cleanliness
NASA SP-8018 lists Mu-metal as an example of a soft magnetic material to consider for spacecraft magnetic cleanliness, and warns that shielding by a highly permeable container can create problems.
Recipe
Nickel-iron-molybdenum soft magnetic alloy, nominal 80 % Ni and 5 % Mo by weight, balance Fe, with Mn 0.50 % and Si 0.15 % nominal (CarTech HyMu 800 type analysis)
Mu-metal is a nickel-iron-molybdenum alloy, nominally 80 % Ni and 5 % Mo, with balance Fe and small manganese and silicon (CarTech HyMu 800 type analysis; MuMETAL sheet typical composition 80 Ni, 5.0 Mo, Mn 0.3 to 0.5, Si 0.1 to 0.4). Its magnetic properties come from a final anneal in dry hydrogen; the HyMu 800 datasheet gives 2050/2150 °F (1120/1177 °C) for low-frequency response, and the Permimphy datasheet gives 800 to 1150 °C.
| Ingredient | Share of the weight | What it does |
|---|---|---|
| Nickel Ni | nominal, 80.00 % in the type analysis | Main element of the alloy, nominal 80 % |
| Molybdenum Mo | nominal, 5.00 % in the type analysis | Alloying element; the Permimphy datasheet says molybdenum increases magnetic permeability |
| Manganese Mn | nominal, 0.50 % | Minor element, nominal |
| Silicon Si | nominal, 0.15 % | Minor element, nominal |
| Iron Fe | balance | Balance of the alloy |
Weight shares are as printed in the sources.
What it can do
Shield a field
400000 DC permeability
measured
The MuMETAL sheet gives a DC permeability of at least 400,000 at 0.005 Oe, and at least 75,000 at 60 Hz and 0.4 A/m for AC.
Saturate at low field
0.75 T
measured
Saturation induction is 0.75 T in the MuMETAL sheet and 0.8 T at 20 °C in the Permimphy datasheet. The alloy saturates at low fields, which keeps its hysteresis loss low in AC circuits.
Weight
8.7 g/cm3
measured
Density is 8.7 g/cm3 in the MuMETAL sheet, and 0.316 lb/in3 in the HyMu 800 datasheet.
Strength when annealed
530 MPa tensile
measured
In the final annealed state a supplier page gives 530 MPa tensile, 160 MPa yield and 45 % elongation. Soft annealed strip in the Permimphy datasheet has a tensile strength of 500 to 700 N/mm2.
How it compares
The alloy is chosen to shield a field, not to carry a load, so its low yield strength matters less than its permeability. The density of 8.7 g/cm3 is the figure to weigh against any alternative shield.
The same measurements for each material, so you can compare them. Each row names the key condition under the value; the full conditions and methods are in the numbered notes under Technical details. Other materials are shown beside it; each was measured under its own conditions, so open its page before comparing closely. Compare every grade in the family.
| Measurement | Ni-Fe-Mo | NdFeB | SmCo | Alnico | FeCoV | CoFe / Co-W / Co-Ti / Co-Al | Ni-Fe-Mo | Fe-Si | MG | NbTi | MgB2, REBCO, BSCCO |
|---|---|---|---|---|---|---|---|---|---|---|---|
| Thermal behavior and safety | |||||||||||
| Melting temperatureValue printed in a manufacturer datasheet | 1450 °C | no data | no data | 1200 to 1450 °C | no data | no data | 1450 °C | no data | 969 to 1024 °C | 2300 °C | 830 °C |
| Thermal conductivity, stress annealed sheet | 19 W/(m·K)8 | 5.3 kcal/(m h °C) | 11.6 to 12.8 W/m °C | no data | 29.83 W/(m·°C) | no data | 0.32 W/cm K | 21 W/(m·K) | no data | no data | no data |
| Thermal conductivity, 80 Ni 5 Mo alloy (HyMu 800)Value printed in a manufacturer datasheet | 240 BTU-in/hr/ft2/°F | 5.3 kcal/(m h °C) | 11.6 to 12.8 W/m °C | no data | 29.83 W/(m·°C) | no data | 0.32 W/cm K | 21 W/(m·K) | no data | no data | no data |
| Specific heatValue printed in a manufacturer datasheet | 460 J/(kg·K) | no data | 370 J/(kg °C) | no data | no data | no data | no data | no data | no data | no data | no data |
| Physical and electrical | |||||||||||
| Density, stress annealed sheet | 8.7 g/cm³7 | 7.6 g/cm³ | 8.2 to 8.4 g/cm³ | 6.9 to 7.3 g/cm³ | 8.12 g/cm³ | 7.9 g/cm³ | 8.7 g/cm³ | 7.6 kg/dm3 | 7.18 g/cm³ | 6.4 to 6.5 g/cm³ | 2.57 g/cm³ |
| Density, 80 Ni 5 Mo alloy (HyMu 800)Value printed in a manufacturer datasheet | 0.316 lb/in3 | 7.6 g/cm³ | 8.2 to 8.4 g/cm³ | 6.9 to 7.3 g/cm³ | 8.12 g/cm³ | 7.9 g/cm³ | 8.7 g/cm³ | 7.6 kg/dm3 | 7.18 g/cm³ | 6.4 to 6.5 g/cm³ | 2.57 g/cm³ |
| Electrical resistivity, stress annealed sheetValue printed in a manufacturer datasheet | 60 µΩ·cm | 150 uohm cm | 80 to 90 uohm cm | 45 to 75 uohm cm | 0.401 Ω·mm²/m | 0.3 µΩm | 55 µΩcm | 59 µΩ·cm | 1.3 µΩm | no data | no data |
| Electrical resistivity at 70 °F, 80 Ni 5 Mo alloy (HyMu 800)Range printed in a manufacturer datasheet | 370 to 380 ohm-cir-mil/ft | 150 uohm cm | 80 to 90 uohm cm | 45 to 75 uohm cm | 0.401 Ω·mm²/m | 0.3 µΩm | 55 µΩcm | 59 µΩ·cm | 1.3 µΩm | no data | no data |
| Temperature behavior | |||||||||||
| Curie temperatureValue printed in a manufacturer datasheet | 420 °C | 310 °C | 700 to 750 °C | 860 °C | 950 °C | 940 °C | 410 °C | no data | 395 °C | no data | no data |
| Other measurements | |||||||||||
| Saturation induction, stress annealed sheet | 0.75 T1 | no data | no data | no data | 2.35 T | no data | 0.8 T | no data | 1.56 T | no data | no data |
| Saturation induction at 20 °C | 0.8 T2 | no data | no data | no data | 2.35 T | no data | 0.8 T | no data | 1.56 T | no data | no data |
| DC permeability at 0.005 Oe, minimum | > 4×10^5 -3 | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data |
| AC permeability at 60 Hz and 0.4 A/m, minimum | > 75000 -4 | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data |
| DC permeability at 5 mOe, typical, 1.00 mm strip | 4.7×10^5 -5 | no data | no data | no data | no data | no data | 4.7×10^5 - | no data | no data | no data | no data |
| DC permeability at 5 mOe, typical, 0.34 mm strip | 5.2×10^5 -6 | no data | no data | no data | no data | no data | 4.7×10^5 - | no data | no data | no data | no data |
| Maximum DC permeability after final heat treatmentRange printed on a manufacturer web page | 3.5×10^5 to 5×10^5 - | no data | no data | no data | no data | no data | 3.2×10^5 to 4.8×10^5 - | no data | no data | no data | no data |
| Coercive force after final heat treatmentTypical value printed on a manufacturer web page | 0.6 A/m | no data | no data | no data | no data | no data | < 1 A/m | no data | no data | no data | no data |
| Thermal expansion coefficient, stress annealed sheetValue printed in a manufacturer datasheet | 12 10-6/K | 7 1e-6 per °C (dL/L) | 8 to 10 1e-6 per °C | 11 to 13 1e-6 per °C | 9.4 ppm/K | no data | 12 10-6/K | 12 10-6/C | 7.6 x10-6/°C | no data | no data |
| Mean coefficient of thermal expansion, -90 to 400 °FValue printed in a manufacturer datasheet | 7.2 10-6 in/in/°F | 7 1e-6 per °C (dL/L) | 8 to 10 1e-6 per °C | 11 to 13 1e-6 per °C | 9.4 ppm/K | no data | 12 10-6/K | 12 10-6/C | 7.6 x10-6/°C | no data | no data |
| Modulus of elasticity, Permimphy stripRange printed in a manufacturer datasheet | 190 to 221 kN/mm2 | no data | 1.2 10^11 N/m2 | no data | 190 to 210 GPa | 440 GPa | 190 to 221 kN/mm2 | 185 GPa | 110 GPa | no data | 149 to 186 GPa |
| Tensile strength, soft annealed temper R500Range printed in a manufacturer datasheet | 500 to 700 N/mm29 | no data | no data | no data | 350 MPa | no data | 450 N/mm2 | 535 MPa | 2000 N/mm2 | no data | no data |
| Yield strength Rp0.2, soft annealed temper R500Range printed in a manufacturer datasheet | 200 to 450 N/mm210 | no data | no data | no data | 250 MPa | no data | 170 N/mm2 | 435 MPa | 1986 MPa | no data | 694 to 957 MPa |
| Elongation A50mm, soft annealed temper R500, minimum | > 25 %11 | no data | no data | no data | < 3 % | no data | 30 % | 17 % | no data | no data | no data |
| Tensile strength, final annealedTypical value printed on a manufacturer web page | 530 MPa12 | no data | no data | no data | 350 MPa | no data | 450 N/mm2 | 535 MPa | 2000 N/mm2 | no data | no data |
| Yield strength 0.2 %, final annealedTypical value printed on a manufacturer web page | 160 MPa13 | no data | no data | no data | 250 MPa | no data | 170 N/mm2 | 435 MPa | 1986 MPa | no data | 694 to 957 MPa |
| Elongation, final annealedTypical value printed on a manufacturer web page | 45 % | no data | no data | no data | < 3 % | no data | 30 % | 17 % | no data | no data | no data |
| Tensile strength after in-process anneal, maximum | < 690 MPa14 | no data | no data | no data | 350 MPa | no data | 450 N/mm2 | 535 MPa | 2000 N/mm2 | no data | no data |
Why choose it, and why not
Good for
- Shielding sensitive electronics from static and low-frequency fields: at least 400,000 DC permeability and 75,000 AC permeability at 60 Hz.
- Current transformer cores and relay parts, as the datasheets list.
- Spacecraft magnetic cleanliness design, where soft magnetic parts must be chosen with care.
Watch out for
- Soft and weak: 160 MPa yield in the final annealed state.
- Heavy: 8.7 g/cm3, so a shield adds mass.
- Permeability is lost after shock or forming, and the alloy needs a re-anneal to recover.
- No corrosion rate or flight record was found for the alloy; the only statement is a manufacturer's claim that no coating is needed.
- The only hazard codes found are for nickel metal, not for the alloy.
Mu-metal is a soft nickel-iron-molybdenum alloy with very high permeability, nominally 80 % Ni and 5 % Mo, used to shield sensitive electronics. It is heavy and weak, and its permeability depends on a careful dry hydrogen anneal and on keeping the part free of shock and deformation. Spacecraft use is documented as design guidance; no flight record was found in this run.
Technical details
For scientists and researchers. Everything above comes from the record below: every number with its method, its conditions and its source.
Other names and standards
The same grade under other systems, as datasheets and standards print them. Each code was checked against the page it comes from.
| System | Codes |
|---|---|
| UNS | N14080 |
| DIN | 17745 |
| JIS | C 2531 |
| ASTM | A753 (Alloy 4) |
| Trade name | MuMETAL, Mumetall, Permimphy |
Notes
The method, full conditions and any caveat for the numbered rows above.
| # | Measurement | Method | Conditions | Caveat |
|---|---|---|---|---|
| 1 | Saturation induction, stress annealed sheet | Typical value printed in a manufacturer datasheet | grade MuMETAL, 80 Ni 5 Mo, stress annealed sheettemperature not statedunit in source 7,500 G (0.75 T) | — |
| 2 | Saturation induction at 20 °C | Typical value printed in a manufacturer datasheet | grade Permimphy N14080 type 4 (80 % Ni, 5 % Mo)temperature 20 °C | — |
| 3 | DC permeability at 0.005 Oe, minimum | Minimum value printed in a manufacturer datasheet | grade MuMETAL, 80 Ni 5 Mofield 0.005 Oe (0.4 A/m)sample stamped rings of 0.35 mm sheet after perfection annealing | — |
| 4 | AC permeability at 60 Hz and 0.4 A/m, minimum | Minimum value printed in a manufacturer datasheet | grade MuMETAL, 80 Ni 5 Mofrequency 60 Hzfield 0.4 A/msample stamped rings of 0.35 mm sheet after perfection annealing | — |
| 5 | DC permeability at 5 mOe, typical, 1.00 mm strip | Typical value printed in a manufacturer datasheet | grade Permimphy N14080 type 4thickness 1.00 mmfield 5 mOe (0.4 A/m)treatment ring samples annealed at 1170 °C in dry pure hydrogen | — |
| 6 | DC permeability at 5 mOe, typical, 0.34 mm strip | Typical value printed in a manufacturer datasheet | grade Permimphy N14080 type 4thickness 0.34 mmfield 5 mOe (0.4 A/m)treatment ring samples annealed at 1170 °C in dry pure hydrogen | — |
| 7 | Density, stress annealed sheet | Typical value printed in a manufacturer datasheet | grade MuMETAL, 80 Ni 5 Mounit in source 0.316 lb/in3 | — |
| 8 | Thermal conductivity, stress annealed sheet | Typical value printed in a manufacturer datasheet | grade MuMETAL, 80 Ni 5 Motemperature not stated | — |
| 9 | Tensile strength, soft annealed temper R500 | — | grade Permimphy N14080 type 4temper R500 soft annealedproduct form strip | — |
| 10 | Yield strength Rp0.2, soft annealed temper R500 | — | grade Permimphy N14080 type 4temper R500 soft annealedmeasure Rp0.2product form strip | — |
| 11 | Elongation A50mm, soft annealed temper R500, minimum | Minimum value printed in a manufacturer datasheet | grade Permimphy N14080 type 4temper R500 soft annealedgauge length 50 mm | — |
| 12 | Tensile strength, final annealed | — | grade Mu-metaltemper final annealed (after dry hydrogen heat treatment)form typical final annealed properties | — |
| 13 | Yield strength 0.2 %, final annealed | — | grade Mu-metaltemper final annealed (after dry hydrogen heat treatment)measure 0.2 % offset | — |
| 14 | Tensile strength after in-process anneal, maximum | Maximum value printed in a manufacturer datasheet | grade HyMu 800, 80 Ni 5 Motemper after in-process strand anneal at 1000/1050 °C, before further cold rolling | — |
Corrosion and compatibility
What happens when it meets other materials and environments.
| Environment | Concern | What happens |
|---|---|---|
| Uncoated, in ordinary air | low | The high nickel content lets the alloy be used without a corrosion-resistant coating.1 |
| # | Environment | Details | Test conditions |
|---|---|---|---|
| 1 | Uncoated, in ordinary air | The Permimphy datasheet says the high nickel content allows use of this material without a corrosion resistant coating. No corrosion rate, humidity test or salt-spray result is printed in the sources read. | grade Permimphy N14080 type 4exposure not statedbasis manufacturer statement, no test data |
Risks and side effects
Hazards to people, what happens when a cell overheats, and how the material is handled and stored.
For people
The hazard classes in the sources are for nickel metal, which makes up about 80 % of the alloy. No separate classification of the alloy was found.
- Nickel as a substance
- PubChem's GHS record for nickel lists H317 allergic skin reaction, H351 suspected cancer and H372 organ damage from repeated exposure, with signal word Danger.
- Alloy as handled
- No health classification of the 80Ni-5Mo alloy itself was found in the sources read.
If it fails
The failure routes in the sources are mechanical and thermal. None of them is a flight result for mu-metal.
- Shock and forming
- Severe shock or further mechanical working after the anneal lowers the permeability in the affected areas. A re-anneal can restore it.
- Poor anneal
- Oxidation or contamination during the hydrogen anneal, or plastic deformation of the treated part, degrades the magnetic properties.
- Mass
- At 8.7 g/cm3 the alloy is heavy, so a shield adds mass to the spacecraft or instrument.
Handling and storage
- Clean before anneal
- Remove oil, grease, lacquer and contaminants before annealing. Separate parts with inert powder such as magnesium or aluminium oxide.
- Anneal in dry hydrogen
- The HyMu 800 datasheet recommends an oxygen-free, dry hydrogen anneal with a dew point below -40 °C, held 2 to 4 hours at 1120 to 1177 °C (2050/2150 °F).
Test details
The original wording and numbers from the sources, for readers who want them.
Failure risks
| Failure | Trigger and consequence |
|---|---|
| Permeability loss from shock or plastic strainmoderate severity | Severe shock, forming or further mechanical working after the final annealThe Magnetic Shield page says the enlarged grains are susceptible to severe shocks or further mechanical working, and the permeability will decrease in those areas. A re-anneal can restore it. |
| Contamination or oxidation during the annealmoderate severity | Heat treatment without a protective atmosphere, or with parts not cleaned or handled with carePermimphy says a protective atmosphere is essential to avoid oxidation, that treated parts must avoid plastic deformation which degrades the magnetic properties, and that parts must be degreased and cleaned first. |
Side effects on surrounding parts
| Affects | Effect |
|---|---|
| Mass of a shield or cored component | The MuMETAL sheet gives a density of 8.7 g/cm3, so shields and cored components add mass. |
Handling and storage
- The Carpenter sheet says oil, grease, lacquer and all other contaminants must be removed before annealing, and parts should be separated by an inert powder such as magnesium or aluminium oxide during the hydrogen anneal. It recommends an oxygen-free, dry hydrogen anneal with a dew point below -40 °C, at 2050/2150 °F (1120/1177 °C), held 2 to 4 hours.
- The Permimphy sheet recommends pure dry hydrogen for the anneal, between 800 and 1150 °C, with anhydrous inert powder to keep parts apart.
Supply and geography
How common the raw materials are and where they come from.
Nickel (about 80 % of the alloy)
- Top producers (2025)
- Indonesia 66.7%, Philippines 6.9%, Russia 5.1%
- Recycling
- USGS: in 2025 nickel recovered from scrap accounted for approximately 60 % of apparent consumption, and most secondary nickel was in the form of stainless steel scrap.
Molybdenum (about 5 % of the alloy)
- Top producers (2025)
- China 37.3%, Chile 16.2%, Peru 15%
- Recycling
- USGS: molybdenum is recycled as a component of catalysts, ferrous scrap and superalloy scrap, and the molybdenum content of recycled alloys is significant and reused.
- Substitutes
- USGS: there is little substitution for molybdenum in its major application in steels and cast irons.
Documents
Datasheets, safety data sheets, papers and standards you can open.
Full record
The complete spore, as stored. Free to reuse under CC-BY-4.0. Images keep the licence shown with each one.
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spore: profile
id: mu-metal
spore_version: 0.2
family: magnet-and-superconducting-alloys
name: Mu-metal
abbreviation: Ni-Fe-Mo
role: magnetic shield
category: metals
type: magnet-alloys
summary: |
Mu-metal is a soft nickel-iron-molybdenum alloy, nominally 80 % Ni and 5 % Mo (ASTM A753 Alloy 4), used to shield sensitive electronics from static and low-frequency magnetic fields. The Magnetic Shield Corporation sheet gives a DC permeability of at least 400,000 at 0.005 Oe, an AC permeability of at least 75,000 at 60 Hz and 0.4 A/m, a saturation induction of 0.75 T and a density of 8.7 g/cm3. Its strength is modest: a supplier page gives 530 MPa tensile and 160 MPa yield in the final annealed state.
best_for: 'Shielding sensitive electronics from static and low-frequency fields: DC permeability of at least 400,000 and AC permeability of at least 75,000 at 60 Hz in the MuMETAL sheet datasheet'
weakest_at: 'Strength and weight: 160 MPa yield in the final annealed state and 8.7 g/cm3 density, and the permeability falls after shock or plastic strain, which needs a re-anneal to recover'
identity:
formula: Nickel-iron-molybdenum soft magnetic alloy, nominal 80 % Ni and 5 % Mo by weight, balance Fe, with Mn 0.50 % and Si 0.15 % nominal (CarTech HyMu 800 type analysis)
source: carpenter-hymu800
where: 'Type Analysis table: Carbon 0.01 %, Manganese 0.50 %, Silicon 0.15 %, Nickel 80.00 %, Molybdenum 5.00 %, Iron balance'
designations:
- system: UNS
code: N14080
source: msc-mumetal
where: 'Specifications paragraph: meets ASTM-A-753 Alloy 4, UNS N14080'
- system: ASTM
code: A753
note: Alloy 4
source: carpenter-hymu800
where: 'Other Information, Applicable Specifications: ASTM A753 Alloy 4'
- system: DIN
code: '17745'
source: msc-mumetal
where: 'Specifications paragraph: DIN 17745'
- system: JIS
code: C 2531
source: matthey-permimphy
where: 'International Standards table: JIS C 2531, row N14080 Type 4'
- system: Trade name
code: MuMETAL
source: msc-mumetal
where: 'Footer and product title: MuMETAL registered trademark of Magnetic Shield Corporation'
- system: Trade name
code: Mumetall
source: wikipedia-mumetal
where: 'Lead section: trade names such as MuMETAL, Mumetall and Mumetal2'
- system: Trade name
code: Permimphy
source: matthey-permimphy
where: 'Title and main technical properties: Permimphy N14080 type 4 alloy'
tags:
environments: []
applications:
- electronics-and-chips
properties:
- benchmark: saturation_induction
label: Saturation induction, stress annealed sheet
value: 0.75
unit: T
scope: material
conditions:
grade: MuMETAL, 80 Ni 5 Mo, stress annealed sheet
temperature: not stated
unit_in_source: 7,500 G (0.75 T)
method: Typical value printed in a manufacturer datasheet
status: ground
source: msc-mumetal
where: Physical Properties table, row Saturation Induction (Bs)
- benchmark: saturation_induction
label: Saturation induction at 20 °C
value: 0.8
unit: T
scope: material
conditions:
grade: Permimphy N14080 type 4 (80 % Ni, 5 % Mo)
temperature: 20 °C
method: Typical value printed in a manufacturer datasheet
status: ground
source: matthey-permimphy
where: Physical properties table, row Saturation induction at 20ºC
- benchmark: permeability_dc_min
label: DC permeability at 0.005 Oe, minimum
value: 400000
bound: lower
unit: '-'
scope: material
conditions:
grade: MuMETAL, 80 Ni 5 Mo
field: 0.005 Oe (0.4 A/m)
sample: stamped rings of 0.35 mm sheet after perfection annealing
method: Minimum value printed in a manufacturer datasheet
status: ground
source: msc-mumetal
where: DC Magnetic Properties, row Permeability at 0.005 Oe
- benchmark: permeability_ac_60hz
label: AC permeability at 60 Hz and 0.4 A/m, minimum
value: 75000
bound: lower
unit: '-'
scope: material
conditions:
grade: MuMETAL, 80 Ni 5 Mo
frequency: 60 Hz
field: 0.4 A/m
sample: stamped rings of 0.35 mm sheet after perfection annealing
method: Minimum value printed in a manufacturer datasheet
status: ground
source: msc-mumetal
where: AC (60 Hz) Magnetic Properties, row Permeability at 0.4 A/m
- benchmark: permeability_dc
label: DC permeability at 5 mOe, typical, 1.00 mm strip
value: 470000
unit: '-'
scope: material
conditions:
grade: Permimphy N14080 type 4
thickness: 1.00 mm
field: 5 mOe (0.4 A/m)
treatment: ring samples annealed at 1170 °C in dry pure hydrogen
method: Typical value printed in a manufacturer datasheet
status: ground
source: matthey-permimphy
where: Magnetic properties table, DC row, thickness 1.00 - 0.04 mm
- benchmark: permeability_dc
label: DC permeability at 5 mOe, typical, 0.34 mm strip
value: 520000
unit: '-'
scope: material
conditions:
grade: Permimphy N14080 type 4
thickness: 0.34 mm
field: 5 mOe (0.4 A/m)
treatment: ring samples annealed at 1170 °C in dry pure hydrogen
method: Typical value printed in a manufacturer datasheet
status: ground
source: matthey-permimphy
where: Magnetic properties table, DC row, thickness 0.34 - 0.0134 mm
- benchmark: permeability_max
label: Maximum DC permeability after final heat treatment
value: 350000
value_high: 500000
bound: range
unit: '-'
scope: material
conditions:
grade: Mu-metal, final heat treatment in dry hydrogen
condition: typical DC magnetic properties after final heat treatment
method: Range printed on a manufacturer web page
status: ground
source: msc-mumetal-web
where: Typical Final Annealed Properties block, Typical Magnetic Properties (DC), row Permeability Mumax
- benchmark: coercive_force
label: Coercive force after final heat treatment
value: 0.6
unit: A/m
scope: material
conditions:
condition: typical DC magnetic properties after final heat treatment
method: Typical value printed on a manufacturer web page
status: ground
source: msc-mumetal-web
where: Typical Magnetic Properties (DC) block, row Coercive Force
- benchmark: curie_temperature
label: Curie temperature
value: 420
unit: °C
scope: material
conditions:
unit_in_source: 788 °F
method: Value printed in a manufacturer datasheet
status: ground
source: msc-mumetal
where: Physical Properties table, row Curie Temperature
- benchmark: density
label: Density, stress annealed sheet
value: 8.7
unit: g/cm3
scope: material
conditions:
grade: MuMETAL, 80 Ni 5 Mo
unit_in_source: 0.316 lb/in3
method: Typical value printed in a manufacturer datasheet
status: ground
source: msc-mumetal
where: Physical Properties table, row Density
- benchmark: density
label: Density, 80 Ni 5 Mo alloy (HyMu 800)
value: 0.316
unit: lb/in3
scope: material
conditions:
grade: HyMu 800, 80 Ni 5 Mo
temperature: not stated
method: Value printed in a manufacturer datasheet
status: ground
source: carpenter-hymu800
where: Physical Properties, row Density
- benchmark: melting_point
label: Melting temperature
value: 1450
unit: °C
scope: material
conditions:
grade: Permimphy N14080 type 4
method: Value printed in a manufacturer datasheet
status: ground
source: matthey-permimphy
where: Physical properties table, row Melting point
- benchmark: thermal_conductivity
label: Thermal conductivity, stress annealed sheet
value: 19
unit: W/(m·K)
scope: material
conditions:
grade: MuMETAL, 80 Ni 5 Mo
temperature: not stated
method: Typical value printed in a manufacturer datasheet
status: ground
source: msc-mumetal
where: Physical Properties table, row Thermal Conductivity
- benchmark: thermal_conductivity
label: Thermal conductivity, 80 Ni 5 Mo alloy (HyMu 800)
value: 240
unit: BTU-in/hr/ft2/°F
scope: material
conditions:
grade: HyMu 800, 80 Ni 5 Mo
temperature: not stated
method: Value printed in a manufacturer datasheet
status: ground
source: carpenter-hymu800
where: Physical Properties, row Thermal Conductivity
- benchmark: cte
label: Thermal expansion coefficient, stress annealed sheet
value: 12
unit: 10-6/K
scope: material
conditions:
grade: MuMETAL, 80 Ni 5 Mo
temperature: not stated
method: Value printed in a manufacturer datasheet
status: ground
source: msc-mumetal
where: Physical Properties table, row Thermal Expansion
- benchmark: cte
label: Mean coefficient of thermal expansion, -90 to 400 °F
value: 7.2
unit: 10-6 in/in/°F
scope: material
conditions:
grade: HyMu 800, 80 Ni 5 Mo
temperature: '-90 to 400 °F'
method: Value printed in a manufacturer datasheet
status: ground
source: carpenter-hymu800
where: Physical Properties, row Mean CTE (-90 to 400°F)
- benchmark: specific_heat
label: Specific heat
value: 460
unit: J/(kg·K)
scope: material
conditions:
grade: MuMETAL, 80 Ni 5 Mo
temperature: not stated
method: Value printed in a manufacturer datasheet
status: ground
source: msc-mumetal
where: Physical Properties table, row Specific Heat
- benchmark: electrical_resistivity
label: Electrical resistivity, stress annealed sheet
value: 60
unit: µΩ·cm
scope: material
conditions:
grade: MuMETAL, 80 Ni 5 Mo
temperature: not stated
method: Value printed in a manufacturer datasheet
status: ground
source: msc-mumetal
where: Physical Properties table, row Electrical Resistivity
- benchmark: electrical_resistivity
label: Electrical resistivity at 70 °F, 80 Ni 5 Mo alloy (HyMu 800)
value: 370
value_high: 380
bound: range
unit: ohm-cir-mil/ft
scope: material
conditions:
grade: HyMu 800, 80 Ni 5 Mo
temperature: 70 °F
method: Range printed in a manufacturer datasheet
status: ground
source: carpenter-hymu800
where: Physical Properties, row Electrical Resistivity (70°F)
- benchmark: elastic_modulus
label: Modulus of elasticity, Permimphy strip
value: 190
value_high: 221
bound: range
unit: kN/mm2
scope: material
conditions:
grade: Permimphy N14080 type 4
temperature: not stated
method: Range printed in a manufacturer datasheet
status: ground
source: matthey-permimphy
where: Physical properties table, row Modulus of elasticity
- benchmark: ultimate_tensile_strength
label: Tensile strength, soft annealed temper R500
value: 500
value_high: 700
bound: range
unit: N/mm2
scope: material
conditions:
grade: Permimphy N14080 type 4
temper: R500 soft annealed
product_form: strip
method: Range printed in a manufacturer datasheet
status: ground
source: matthey-permimphy
where: Mechanical properties of strips table, row R500 soft annealed, column Rm
- benchmark: yield_strength
label: Yield strength Rp0.2, soft annealed temper R500
value: 200
value_high: 450
bound: range
unit: N/mm2
scope: material
conditions:
grade: Permimphy N14080 type 4
temper: R500 soft annealed
measure: Rp0.2
product_form: strip
method: Range printed in a manufacturer datasheet
status: ground
source: matthey-permimphy
where: Mechanical properties of strips table, row R500 soft annealed, column Rp0.2
- benchmark: elongation
label: Elongation A50mm, soft annealed temper R500, minimum
value: 25
bound: lower
unit: '%'
scope: material
conditions:
grade: Permimphy N14080 type 4
temper: R500 soft annealed
gauge_length: 50 mm
method: Minimum value printed in a manufacturer datasheet
status: ground
source: matthey-permimphy
where: Mechanical properties of strips table, row R500 soft annealed, column A50mm
- benchmark: ultimate_tensile_strength
label: Tensile strength, final annealed
value: 530
unit: MPa
scope: material
conditions:
grade: Mu-metal
temper: final annealed (after dry hydrogen heat treatment)
form: typical final annealed properties
method: Typical value printed on a manufacturer web page
status: ground
source: msc-mumetal-web
where: Typical Final Annealed Properties block, row Tensile Strength
- benchmark: yield_strength
label: Yield strength 0.2 %, final annealed
value: 160
unit: MPa
scope: material
conditions:
grade: Mu-metal
temper: final annealed (after dry hydrogen heat treatment)
measure: 0.2 % offset
method: Typical value printed on a manufacturer web page
status: ground
source: msc-mumetal-web
where: Typical Final Annealed Properties block, row 0.2 % Yield Strength
- benchmark: elongation
label: Elongation, final annealed
value: 45
unit: '%'
scope: material
conditions:
grade: Mu-metal
temper: final annealed (after dry hydrogen heat treatment)
method: Typical value printed on a manufacturer web page
status: ground
source: msc-mumetal-web
where: Typical Final Annealed Properties block, row Elongation
- benchmark: ultimate_tensile_strength
label: Tensile strength after in-process anneal, maximum
value: 690
bound: upper
unit: MPa
scope: material
conditions:
grade: HyMu 800, 80 Ni 5 Mo
temper: after in-process strand anneal at 1000/1050 °C, before further cold rolling
method: Maximum value printed in a manufacturer datasheet
status: ground
source: carpenter-hymu800
where: Heat Treatment, In-Process Anneal paragraph (100 ksi (690 MPa) maximum)
corrosion:
- environment: Uncoated, in ordinary air
headline: The high nickel content lets the alloy be used without a corrosion-resistant coating.
effect: The Permimphy datasheet says the high nickel content allows use of this material without a corrosion resistant coating. No corrosion rate, humidity test or salt-spray result is printed in the sources read.
rating: low
conditions:
grade: Permimphy N14080 type 4
exposure: not stated
basis: manufacturer statement, no test data
source: matthey-permimphy
where: Main technical properties and features, first paragraph
risks:
hazards:
- text: PubChem's GHS record for nickel (CID 935) lists H317 (may cause an allergic skin reaction), H351 (suspected of causing cancer) and H372 (causes damage to organs through prolonged or repeated exposure), signal word Danger. These are the classes for nickel metal, not for the alloy, which is not separately classified in the sources read; the alloy is about 80 % nickel.
ghs:
- H317
- H351
- H372
source: pubchem-ni
where: GHS Classification section, Hazard Statements
failure_risks:
- mode: Permeability loss from shock or plastic strain
trigger: Severe shock, forming or further mechanical working after the final anneal
consequence: The Magnetic Shield page says the enlarged grains are susceptible to severe shocks or further mechanical working, and the permeability will decrease in those areas. A re-anneal can restore it.
severity: moderate
source: msc-mumetal-web
where: Heat treatment paragraph after the dry hydrogen anneal description
- mode: Contamination or oxidation during the anneal
trigger: Heat treatment without a protective atmosphere, or with parts not cleaned or handled with care
consequence: Permimphy says a protective atmosphere is essential to avoid oxidation, that treated parts must avoid plastic deformation which degrades the magnetic properties, and that parts must be degreased and cleaned first.
severity: moderate
source: matthey-permimphy
where: Heat treatment of finished parts paragraph
side_effects:
- text: The MuMETAL sheet gives a density of 8.7 g/cm3, so shields and cored components add mass.
affects: Mass of a shield or cored component
source: msc-mumetal
where: Physical Properties table, row Density
handling:
- text: The Carpenter sheet says oil, grease, lacquer and all other contaminants must be removed before annealing, and parts should be separated by an inert powder such as magnesium or aluminium oxide during the hydrogen anneal. It recommends an oxygen-free, dry hydrogen anneal with a dew point below -40 °C, at 2050/2150 °F (1120/1177 °C), held 2 to 4 hours.
source: carpenter-hymu800
where: Heat Treatment, Thermal Treatment for Magnetic Properties paragraph
- text: The Permimphy sheet recommends pure dry hydrogen for the anneal, between 800 and 1150 °C, with anhydrous inert powder to keep parts apart.
source: matthey-permimphy
where: Heat treatment of finished parts paragraph
uses:
- application: electronics-and-chips
device: Magnetic shielding for sensitive electronics, current sensors and current transformer cores
example: The MuMETAL sheet datasheet says MuMETAL bar is used in high quality magnetic shielding, current sensors, high precision current transformer cores and ground fault circuit breaker relay parts.
source: msc-mumetal
where: Description paragraph
- application: electronics-and-chips
device: Relays, stepper motors and magnetic sensors
example: Permimphy's main applications include relays for ground fault circuit breakers and railway signalling, stepper motors for watches, shielding and magnetic sensors for current, angular position and displacement.
source: matthey-permimphy
where: Typical uses paragraph
- application: electronics-and-chips
device: Spacecraft magnetic cleanliness, soft magnetic parts near magnetometers
example: NASA SP-8018, a 1969 spacecraft design criteria document, names Mu-metal, with mild steel, as an example of a soft magnetic material in its guidance on magnetic cleanliness. It warns that enclosing a component in a highly permeable container can create problems for the shielded component.
source: nasa-sp8018
where: Section on magnetic materials, paragraph on hard and soft materials; Shielding paragraph (reference 37)
supply:
- subject: Nickel (about 80 % of the alloy)
producers:
- country: Indonesia
share_percent: 66.7
year: 2025
- country: Philippines
share_percent: 6.9
year: 2025
- country: Russia
share_percent: 5.1
year: 2025
critical_lists: []
recycling: 'USGS: in 2025 nickel recovered from scrap accounted for approximately 60 % of apparent consumption, and most secondary nickel was in the form of stainless steel scrap.'
substitutes: []
source: usgs-mcs2026-nickel
where: 'World Mine Production and Reserves table, 2025e column, metric tons of nickel content: Indonesia 2,600,000; Philippines 270,000; Russia 200,000; world total 3,900,000 (shares calculated by Space Mushroom from these figures). Recycling paragraph.'
- subject: Molybdenum (about 5 % of the alloy)
producers:
- country: China
share_percent: 37.3
year: 2025
- country: Chile
share_percent: 16.2
year: 2025
- country: Peru
share_percent: 15
year: 2025
critical_lists: []
recycling: 'USGS: molybdenum is recycled as a component of catalysts, ferrous scrap and superalloy scrap, and the molybdenum content of recycled alloys is significant and reused.'
substitutes:
- 'USGS: there is little substitution for molybdenum in its major application in steels and cast irons.'
source: usgs-mcs2026-molybdenum
where: 'World Mine Production and Reserves table, 2025e column, thousand metric tons: China 97,000; Chile 42,000; Peru 39,000; world total 260,000 (shares calculated by Space Mushroom). Events, Trends and Issues: China, Chile, the United States, Peru and Mexico produced 90 % of world output in 2025.'
documents:
- title: Magnetic Shield Corporation, MuMETAL stress annealed sheet data
type: datasheet
url: https://www.magnetic-shield.com/content/MuMetal%20Stress%20Annealed%20Sheet%20Data.pdf
- title: CarTech HyMu 800 alloy datasheet (Carpenter Technology, 2020 copyright)
type: datasheet
url: https://www.carpentertechnology.com/hubfs/7407324/Material%20Saftey%20Data%20Sheets/HyMu%20800.pdf
year: 2020
- title: Lamineries Matthey, Mumetal Permimphy datasheet
type: datasheet
url: https://www.matthey.ch/fileadmin/user_upload/downloads/fichetechnique/EN/Permimphy_v22E.pdf
- title: 'Wikipedia: Mu-metal'
type: report
url: https://en.wikipedia.org/wiki/Mu-metal
- title: NASA SP-8018, Space Vehicle Design Criteria (Guidance and Control), NTRS 19690020961
type: report
url: https://ntrs.nasa.gov/citations/19690020961
year: 1969
- title: 'USGS Mineral Commodity Summaries 2026: Nickel'
type: report
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-nickel.pdf
year: 2026
- title: 'USGS Mineral Commodity Summaries 2026: Molybdenum'
type: report
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-molybdenum.pdf
year: 2026
- title: PubChem compound record for nickel (CID 935), GHS classification
type: database
url: https://pubchem.ncbi.nlm.nih.gov/compound/Nickel
gaps:
- No flight-proven mu-metal magnetic shield on a named spacecraft was found in this run. MAVEN and MMS magnetometer papers mention mu-metal test chambers, but the full texts were not read (the Springer PDF was blocked), so the only space use entered is the NASA SP-8018 design guidance.
- The DAMPE satellite calorimeter (arXiv 1309.7638) shielded a photomultiplier with a permalloy cylinder, not mu-metal, so it is not entered as a mu-metal use.
- The MuMETAL sheet mechanical table (tensile 650 MPa, yield 280 MPa, elongation 35 %, hardness 130 to 170 HV) gives no temper, so it is not entered. The Permimphy and final-annealed values are used instead.
- The HyMu 800 magnetic curves (DC, 60 Hz and 400 Hz permeability and core loss) are graphs with no printed table in the PDF, so no values were taken from them.
- The Permimphy electrical resistivity is printed as 55 with no unit, so it is not entered. The MuMETAL sheet gives 60 µΩ·cm.
- The mumetal.co.uk page gives 4.5 % molybdenum, which conflicts with 5 % in the other sources, so its composition is not used. The Wikipedia range of 12 to 15 % iron is a different formulation and is not used.
- Corrosion rate and salt-spray or humidity data for mu-metal were not found. The only corrosion statement is a manufacturer claim that the high nickel content needs no coating.
- No ASTM A753 standard text was opened, so the grade limits for Alloy 4 are taken from the Carpenter and Matthey datasheets only. The Fabdigit page was blocked by a security checkpoint.
- The GHS hazard codes are for nickel metal (PubChem CID 935). No hazard classification of the 80Ni-5Mo alloy itself was found.
- Whether nickel or molybdenum is on the U.S. 2025 final critical minerals list was not confirmed in the USGS text read, so critical_lists is empty for both.
- Radiation effects, cold-welding and outgassing data for mu-metal were not looked up.
- 'Dates for the HyMu 800 datasheet: the PDF gives an edition date of 11/01/1991 and a 2020 copyright, so the version is uncertain.'
sources:
msc-mumetal:
title: Magnetic Shield Corporation, MuMETAL stress annealed sheet data sheet
url: https://www.magnetic-shield.com/content/MuMetal%20Stress%20Annealed%20Sheet%20Data.pdf
kind: datasheet
license: Manufacturer datasheet (cited, not reproduced)
msc-mumetal-web:
title: Magnetic Shields Limited, Mu Metal specifications page (mumetal.co.uk)
url: https://mumetal.co.uk/?p=100
kind: web
license: Manufacturer web page (cited, not reproduced)
carpenter-hymu800:
title: CarTech HyMu 800 alloy data sheet, Carpenter Technology
url: https://www.carpentertechnology.com/hubfs/7407324/Material%20Saftey%20Data%20Sheets/HyMu%20800.pdf
kind: datasheet
license: Manufacturer data sheet, typical values (cited, not reproduced)
matthey-permimphy:
title: Lamineries Matthey, Mumetal Permimphy N14080 type 4 datasheet
url: https://www.matthey.ch/fileadmin/user_upload/downloads/fichetechnique/EN/Permimphy_v22E.pdf
kind: datasheet
license: Manufacturer data sheet (cited, not reproduced)
wikipedia-mumetal:
title: 'Wikipedia: Mu-metal'
url: https://en.wikipedia.org/wiki/Mu-metal
kind: web
license: CC BY-SA (cited, not reproduced)
nasa-sp8018:
title: NASA SP-8018, Space Vehicle Design Criteria (Guidance and Control), magnetic materials and shielding sections
id: NTRS 19690020961
url: https://ntrs.nasa.gov/citations/19690020961
year: 1969
kind: report
license: NASA public document (cited, not reproduced)
usgs-mcs2026-nickel:
title: 'USGS Mineral Commodity Summaries 2026: Nickel'
id: USGS MCS 2026
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-nickel.pdf
year: 2026
kind: report
license: Public domain (USGS)
usgs-mcs2026-molybdenum:
title: 'USGS Mineral Commodity Summaries 2026: Molybdenum'
id: USGS MCS 2026
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-molybdenum.pdf
year: 2026
kind: report
license: Public domain (USGS)
pubchem-ni:
title: 'PubChem compound record: Nickel (CID 935), GHS classification'
id: CID 935
url: https://pubchem.ncbi.nlm.nih.gov/compound/Nickel
kind: database
license: PubChem (NCBI), public domain; sections attributed to ECHA and notifiers
license: CC-BY-4.0
updated: '2026-10-26'
review:
status: draft
method: assistant
checked_values: 27
unreachable: 2
caveats: 6
note: 'Values were read by an AI assistant on 2026-10-26 from the datasheets, web pages and reports named in each entry. Unreachable: the MAVEN and MMS Springer full texts (blocked) and the Fabdigit page (security checkpoint). Caveats: the 80Ni-5Mo values come from three manufacturers and a supplier web page with typical or nominal figures; the permeability and strength values are typical, not guaranteed; the spacecraft use is design guidance, not a flight record; the hazard codes are for nickel metal; the supply shares are calculated from USGS tonnages.'
story:
risk_groups:
- title: For people
lead: The hazard classes in the sources are for nickel metal, which makes up about 80 % of the alloy. No separate classification of the alloy was found.
level: 1
verdict: Nickel classes
points:
- label: Nickel as a substance
line: PubChem's GHS record for nickel lists H317 allergic skin reaction, H351 suspected cancer and H372 organ damage from repeated exposure, with signal word Danger.
- label: Alloy as handled
line: No health classification of the 80Ni-5Mo alloy itself was found in the sources read.
- title: If it fails
lead: The failure routes in the sources are mechanical and thermal. None of them is a flight result for mu-metal.
points:
- label: Shock and forming
line: Severe shock or further mechanical working after the anneal lowers the permeability in the affected areas. A re-anneal can restore it.
- label: Poor anneal
line: Oxidation or contamination during the hydrogen anneal, or plastic deformation of the treated part, degrades the magnetic properties.
- label: Mass
line: At 8.7 g/cm3 the alloy is heavy, so a shield adds mass to the spacecraft or instrument.
- title: Handling and storage
points:
- label: Clean before anneal
line: Remove oil, grease, lacquer and contaminants before annealing. Separate parts with inert powder such as magnesium or aluminium oxide.
- label: Anneal in dry hydrogen
line: The HyMu 800 datasheet recommends an oxygen-free, dry hydrogen anneal with a dew point below -40 °C, held 2 to 4 hours at 1120 to 1177 °C (2050/2150 °F).
why: Mu-metal is used to shield sensitive electronics from static and low-frequency magnetic fields. It is a soft nickel-iron-molybdenum alloy with nominal 80 % Ni and 5 % Mo, and its high permeability gives a low-reluctance path for the field. The MuMETAL sheet datasheet gives a DC permeability of at least 400,000 at 0.005 Oe and an AC permeability of at least 75,000 at 60 Hz. The saturation induction is 0.75 T, and the Curie temperature is 420 °C. The sources read give it a yield strength of 160 MPa in the final annealed state, so it is chosen for its magnetic performance, not for its strength.
uses:
- where: Magnetic shields and sensors
line: MuMETAL is used in high quality magnetic shielding, current sensors and high precision current transformer cores. Permimphy is used for relays, stepper motors and magnetic sensors.
- where: Spacecraft magnetic cleanliness
line: NASA SP-8018 lists Mu-metal as an example of a soft magnetic material to consider for spacecraft magnetic cleanliness, and warns that shielding by a highly permeable container can create problems.
can_do:
- label: Shield a field
value: 400000 DC permeability
benchmark: permeability_dc_min
line: The MuMETAL sheet gives a DC permeability of at least 400,000 at 0.005 Oe, and at least 75,000 at 60 Hz and 0.4 A/m for AC.
- label: Saturate at low field
value: 0.75 T
benchmark: saturation_induction
line: Saturation induction is 0.75 T in the MuMETAL sheet and 0.8 T at 20 °C in the Permimphy datasheet. The alloy saturates at low fields, which keeps its hysteresis loss low in AC circuits.
- label: Weight
value: 8.7 g/cm3
benchmark: density
line: Density is 8.7 g/cm3 in the MuMETAL sheet, and 0.316 lb/in3 in the HyMu 800 datasheet.
- label: Strength when annealed
value: 530 MPa tensile
benchmark: ultimate_tensile_strength
line: In the final annealed state a supplier page gives 530 MPa tensile, 160 MPa yield and 45 % elongation. Soft annealed strip in the Permimphy datasheet has a tensile strength of 500 to 700 N/mm2.
compare: The alloy is chosen to shield a field, not to carry a load, so its low yield strength matters less than its permeability. The density of 8.7 g/cm3 is the figure to weigh against any alternative shield.
compare_rows:
- label: Density
benchmark: density
- label: DC permeability
benchmark: permeability_dc_min
- label: Thermal expansion
benchmark: cte
handling:
- Anneal in dry hydrogen with a dew point below -40 °C, after removing all oil and contaminants.
- Avoid shock and plastic deformation after the anneal, because the permeability falls and needs a re-anneal to recover.
- The only hazard codes found are for nickel metal (PubChem); treat the alloy with the same care until a supplier classification is found.
good_for:
- 'Shielding sensitive electronics from static and low-frequency fields: at least 400,000 DC permeability and 75,000 AC permeability at 60 Hz.'
- Current transformer cores and relay parts, as the datasheets list.
- Spacecraft magnetic cleanliness design, where soft magnetic parts must be chosen with care.
watch_out:
- 'Soft and weak: 160 MPa yield in the final annealed state.'
- 'Heavy: 8.7 g/cm3, so a shield adds mass.'
- Permeability is lost after shock or forming, and the alloy needs a re-anneal to recover.
- No corrosion rate or flight record was found for the alloy; the only statement is a manufacturer's claim that no coating is needed.
- The only hazard codes found are for nickel metal, not for the alloy.
verdict: Mu-metal is a soft nickel-iron-molybdenum alloy with very high permeability, nominally 80 % Ni and 5 % Mo, used to shield sensitive electronics. It is heavy and weak, and its permeability depends on a careful dry hydrogen anneal and on keeping the part free of shock and deformation. Spacecraft use is documented as design guidance; no flight record was found in this run.
recipe:
line: Mu-metal is a nickel-iron-molybdenum alloy, nominally 80 % Ni and 5 % Mo, with balance Fe and small manganese and silicon (CarTech HyMu 800 type analysis; MuMETAL sheet typical composition 80 Ni, 5.0 Mo, Mn 0.3 to 0.5, Si 0.1 to 0.4). Its magnetic properties come from a final anneal in dry hydrogen; the HyMu 800 datasheet gives 2050/2150 °F (1120/1177 °C) for low-frequency response, and the Permimphy datasheet gives 800 to 1150 °C.
parts:
- name: Nickel
symbol: Ni
share_percent: 80
share_note: nominal, 80.00 % in the type analysis
role: Main element of the alloy, nominal 80 %
source: carpenter-hymu800
where: Type Analysis table, Nickel 80.00 %
- name: Molybdenum
symbol: Mo
share_percent: 5
share_note: nominal, 5.00 % in the type analysis
role: Alloying element; the Permimphy datasheet says molybdenum increases magnetic permeability
source: carpenter-hymu800
where: Type Analysis table, Molybdenum 5.00 %
- name: Manganese
symbol: Mn
share_percent: 0.5
share_note: nominal, 0.50 %
role: Minor element, nominal
source: carpenter-hymu800
where: Type Analysis table, Manganese 0.50 %
- name: Silicon
symbol: Si
share_percent: 0.15
share_note: nominal, 0.15 %
role: Minor element, nominal
source: carpenter-hymu800
where: Type Analysis table, Silicon 0.15 %
- name: Iron
symbol: Fe
share_note: balance
role: Balance of the alloy
source: carpenter-hymu800
where: Type Analysis table, Iron Balance
References
Every number above carries a reference number. Click one to see the source and where in it the value comes from.
| # | Source | Type | Year | Used for |
|---|---|---|---|---|
| Magnetic Shield Corporation, MuMETAL stress annealed sheet data sheet | datasheet | 11 values | ||
| Magnetic Shields Limited, Mu Metal specifications page (mumetal.co.uk) | web | 6 values | ||
| CarTech HyMu 800 alloy data sheet, Carpenter Technology | datasheet | 7 values | ||
| Lamineries Matthey, Mumetal Permimphy N14080 type 4 datasheet | datasheet | 12 values | ||
| Wikipedia: Mu-metal | web | 0 values | ||
| NASA SP-8018, Space Vehicle Design Criteria (Guidance and Control), magnetic materials and shielding sections | report | 1969 | 1 value | |
| USGS Mineral Commodity Summaries 2026: Nickel | report | 2026 | 1 value | |
| USGS Mineral Commodity Summaries 2026: Molybdenum | report | 2026 | 1 value | |
| PubChem compound record: Nickel (CID 935), GHS classification | database | 1 value |