Monel 400

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Monel 400 / (2.4360) / UNS N04400 / AMS 4675 / AMS 4544

Monel 400
UNS N04400 · W.Nr. 2.4360 (some sources also give 2.4361 for the same alloy) · NiCu30Fe (DIN/EN) · BS NA13 · ISO NW4400 · Ni(+Co) 63% min – Cu 28-34% – Fe 2.5% max – Mn 2.0% max – C 0.3% max – Si 0.5% max – S 0.024% max.
Not to be confused with

Monel K500

For what
Nickel-copper SOLID SOLUTION alloy. It is NOT PRECIPITATION HARDENABLE; its strength comes from the Ni-Cu matrix and from cold work, and it cannot be strengthened by ageing.
Forms
Round bar · flat bar · plate · sheet · tube and pipe · forgings. All forms are supplied to order.
Standards
AMS 4544 — sheet, strip and plate; ANNEALED (67Ni-30Cu). · AMS 4675 — bars (2.35-100.00 mm) plus forgings and forging stock (67Ni-30Cu). · AMS 4574 — seamless tubing; ANNEALED (67Ni-31Cu). · AMS 4575 — BRAZED tubing; ANNEALED (67Ni-31Cu). · AMS 4730 — wire; ANNEALED (67Ni-31Cu, alloy 400). · AMS 4731 — wire and ribbon; ANNEALED (67Ni-31Cu, Monel 400). · ASTM B127 / ASME SB-127 — plate, sheet and strip. · ASTM B164 / ASME SB-164 — rod, bar and wire. · ASTM B165 / ASME SB-165 — seamless pipe and tube. · ASTM B163 / ASME SB-163 — condenser and heat-exchanger tube. · ASTM B725 / ASME SB-725 — welded pipe. · ASTM B730 / ASME SB-730 — welded tube. · ASTM B564 / ASME SB-564 — forgings. · ASTM B366 / ASME SB-366 — welded fittings. · ASTM B751, B775, B829 — general requirements for tubular products. · DIN 17743, 17750, 17752, 17753, 17754 · VdTUV Material Sheet 263. · QQ-N-281 (Class A and Class B) · MIL-T-1368. · NACE MR0175 / ISO 15156 and MR0103.
AMS 4674 (67Ni-30Cu-0.04S, free machining) is NOT N04400; it covers the sulphur-bearing free-machining Monel R-405 (UNS N04405), which some distributor lists wrongly file under 400.
Advantage
Having no chromium, it is weak in oxidising media, but it works in reducing media: it is one of the few commercial alloys usable in de-aerated hydrofluoric acid at ALL concentrations up to the boiling point.
Welding
Filler metal: AWS A5.14 ERNiCu-7 (UNS N04060; Monel Filler Metal 60 / VDM FM 60, W.Nr. 2.4377) for GTAW, GMAW and SAW. Covered electrode: AWS A5.11 ENiCu-7 (Monel Welding Electrode 190). INCOFLUX 5 is used as the flux for submerged-arc welding. Shielding gas is argon with at most 3% H2;
Limits
NOT FOR OXIDISING SERVICE — there is no chromium. Nitric acid above 0.5% concentration attacks the alloy rapidly. Oxidising salts in sulphuric acid (ferric sulphate, chromates, dichromates, nitrates, nitrites, peroxides, cupric salts) and ferric chloride make the solution highly corrosive; aeration raises the corrosion rate.
Compiled from manufacturer data sheets · confirm against the current specification before ordering

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On this page · click to jump
Standards by Product FormR-405 and K-500Mechanical PropertiesMagnetic BehaviourWelding and Heat TreatmentMachining and FormingCorrosionFrequently Asked Questions



Monel 400 (2.4360 – 2.4361), also widely known as Alloy 400, is an alloy of nickel and copper. Belonging to the Monel family, this nickel-copper material is the most widely used and most readily available Monel grade. It has a very high degree of corrosion resistance, and its mechanical values are high as well. Able to withstand a wide range of corrosive environments, this nickel/copper alloy is chosen across a very broad range of applications.

Alloy 400 (Monel 400) is used in many marine fittings, in parts exposed to chemical processes, in valves, pumps, special shafts, connecting parts and screws, and in electrical components. It is also very suitable for welding, and is used from time to time in boat and yacht shafts. The material is also resistant to acids such as hydrochloric acid and phosphoric acid. It is weakly attracted by a magnet and is not a non-magnetic material.​‌​​‌​

Able to work across a very wide temperature range, this nickel-copper alloy operates at sub-zero temperatures and also retains most of its mechanical properties up to 450-500 °C. A much more readily machinable version of this material, Monel Alloy R-405 (Monel R405), is also available.

Chemical Composition (Monel 400) · Monel 400 (2.4360 – 2.4361)

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Nimin 63.0%​‌​​‌​
Femax 2.50%​‌​​‌​
Cmax 0.30%​‌​​‌​
Mnmax 2.00%​‌​​‌​
Simax 0.50%​‌​​‌​
Smax 0.024%​‌​​‌​
Cu28.0-34.0%​‌​​‌​
Mechanical Properties at Room Temperature

Density (specific gravity)​‌​​‌​8800 kg/m³
Melting Temperature​‌​​‌​1300-1350°C
Standards and Equivalents · Monel 400
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Trade nameMonel 400​‌​​‌​
UNSN04400​‌​​‌​
W.Nr (DIN/EN)2.4360 · 2.4361​‌​​‌​
AMS4544 · 4574 · 4675​‌​​‌​
Available formsRound bar · Flat bar · Plate · Sheet · Tube · Forgings
All forms are supplied to order.​‌​​‌​

Standards by Product Form​‌​​‌​

STANDARDS BY PRODUCT FORM
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Product formStandards
Round bar, flat barAMS 4675 (bars 2.35-100.00 mm plus forgings and forging stock) · ASTM B164 / ASME SB-164 (rod, bar, wire) · QQ-N-281 · DIN 17752 · BS 3076 NA13 · VdTUV 263​‌​​‌​
ForgingAMS 4675 (forgings and forging stock) · ASTM B564 / ASME SB-564 · DIN 17754​‌​​‌​
PlateAMS 4544 (sheet, strip, plate; ANNEALED) · ASTM B127 / ASME SB-127 · QQ-N-281 Class A · DIN 17750​‌​​‌​
Sheet, stripAMS 4544 (sheet, strip, plate; ANNEALED) · ASTM B127 / ASME SB-127 · QQ-N-281 Class A · DIN 17750​‌​​‌​
Tube and pipe — seamlessAMS 4574 (seamless tubing; ANNEALED) · ASTM B165 / ASME SB-165 (seamless pipe and tube) · ASTM B163 / ASME SB-163 (condenser and heat-exchanger tube) · ASTM B829 and B775 (general requirements) · MIL-T-1368 · VdTUV 263​‌​​‌​
Tube and pipe — weldedASTM B725 / ASME SB-725 (welded pipe) · ASTM B730 / ASME SB-730 (welded tube) · ASTM B751 and B775 (general requirements). There is NO AMS specification covering welded pipe or tube; AMS 4575 is BRAZED tubing, not welded.​‌​​‌​
Tube — brazedAMS 4575 (brazed tubing; ANNEALED, 67Ni-31Cu). There is no ASTM equivalent for this form.​‌​​‌​
Wire, ribbonAMS 4730 (wire; ANNEALED) · AMS 4731 (wire and ribbon; ANNEALED) · ASTM B164 / ASME SB-164 (cold-worked wire) · DIN 17753 · BS 3075 NA13​‌​​‌​
Welded fittingASTM B366 / ASME SB-366. There is NO AMS specification for this form.​‌​​‌​
Welding consumableAWS A5.14 ERNiCu-7 (welding wire, UNS N04060, W.Nr. 2.4377) · AWS A5.11 ENiCu-7 (covered electrode). ASME Section IX F-No. 42; base metal P-No. 42.​‌​​‌​
AMS numbers are listed first, ASTM second. There is no AMS specification for welded pipe, welded tube or welded fittings; only ASTM covers them. Selling AMS 4575 as ‘seamless tubing’ is a common error; the specification title is BRAZED tubing. QQ-N-281 is a cancelled federal specification. Class A corresponds to the annealed condition and Class B to cold-drawn and stress-relieved; it is listed here only because it is still referenced. DIN 17743 (composition), 17750 (sheet and plate), 17752 (bar), 17753 (wire), 17754 (forgings) and VdTUV Material Sheet 263 are the European counterparts.

Monel 400 (UNS N04400 / W.Nr. 2.4360 / EN NiCu30Fe) is a solid-solution Ni-Cu alloy. Two things on this page deserve particular care: magnetic behaviour (the alloy is sold as “non-magnetic” and is not) and flow regime in seawater (flowing seawater and stagnant seawater are not the same duty).​‌​​‌​

Standards by Product Form · Monel 400 (N04400)

Plate · sheet · strip​‌​​‌​ASTM B127 / ASME SB-127 — N04400 only
Rod · bar · wire​‌​​‌​ASTM B164 / SB-164 — covers N04400 AND N04405
Forgings​‌​​‌​ASTM B564 / SB-564 — a multi-alloy umbrella specification
Seamless pipe and tube​‌​​‌​ASTM B165 / SB-165 — specific to N04400
Condenser · heat-exchanger tube​‌​​‌​ASTM B163 / SB-163 — a multi-alloy TUBE specification; N04400 is one of several grades in it. Do not confuse it with B165
Welded pipe​‌​​‌​ASTM B725 / SB-725 — “Welded Nickel (N02200/N02201) and Nickel-Copper Alloy (N04400) Pipe”
Welded tube​‌​​‌​ASTM B730 / SB-730
Fittings​‌​​‌​ASTM B366 / SB-366
General requirements​‌​​‌​B751 (welded tube), B775 (welded pipe), B829 (seamless pipe/tube) — these are companion documents. An order citing only “ASTM B829” has specified no product at all
Bolts · nuts​‌​​‌​ASTM F468 (Class A = N04400 / “F468U”; Class B = N04405 / “F468V”) · ASTM F467 (nuts)
AMS​‌​​‌​AMS 4544 (plate/sheet/strip) · AMS 4574 (tube) · AMS 4675 (bar/forgings) · AMS 4730/4731 (bar family, single-sourced). Revision letters could not be verified — order to a revision letter, not a bare “AMS 4544”. AMS 4674 and 7234 are R-405 only; AMS 4676 is K-500 only
European​‌​​‌​W.Nr. 2.4360 (and the higher-purity 2.4361) · DIN 17743 (composition), 17750 (sheet/plate), 17751 (tube), 17752 (bar), 17753 (wire), 17754 (forgings) · BS 3072–3076 NA13 · VdTÜV Material Sheet 263, pressure-vessel approval −10 to +425 °C
NACE​‌​​‌​N04400 and N04405 are acceptable under MR0175 / ISO 15156-3, maximum hardness 35 HRC. But know the history: N04400 was in the 1975 edition, was removed from general usage in the MR0175 rewrite, was restored by ISO 15156-3:2003 Technical Corrigendum 2 and confirmed in the 2009 second edition. Legacy datasheets and old certificates may mislead in either direction
ASME​‌​​‌​ASME-adopted across all the SB- numbers above and code-usable in Section VIII Div. 1. Maximum code temperature 480 °C (900 °F) (single-sourced; confirm against the current Code edition). Code Case 1192 applies to K-500 bolting, not to alloy 400 — it is frequently mis-attributed
Nuclear​‌​​‌​— (could not be verified). No ASME Section III listing or NRC acceptance for N04400 was found. Do not claim nuclear approval
Military · federal​‌​​‌​QQ-N-281 (bar, plate, sheet, strip, wire, forgings; Class A hot-worked/annealed, Class B cold-worked/stress-relieved) and MIL-T-1368C (tube and pipe, dated 1965) both list as active on specification aggregators — but those lag the official register, so verify before publishing. MIL-N-894 applies to R-405, not 400; QQ-N-286 applies to K-500, not 400 — both are routinely mis-listed
Welding consumables​‌​​‌​Bare wire (GTAW/GMAW/SAW): AWS A5.14 ERNiCu-7 (Filler Metal 60) · Covered electrode: AWS A5.11 ENiCu-7 (Electrode 190) · ISO 18274 S Ni 4060 (NiCu30Mn3Ti). Procedure qualification P-No. 42

R-405 and K-500 — Separate UNS Numbers, Separate Products​‌​​‌​

Monel R-405 is UNS N04405, NOT N04400. The chemical difference is sulphur alone: S 0.025–0.060 % — a band with a minimum as well as a maximum — against S ≤0.024 % for N04400. Every other limit is identical. Forms: the originator states R-405 is “normally furnished only in the form of rod and bar“, and ASTM corroborates indirectly: B164 is the only ASTM product specification that lists N04405; B127, B165, B163, B725, B730 and B564 do not cover it. The mill’s own words: R-405 “is used chiefly for automatic screw-machine stock and is not generally recommended for other applications“. So “Monel R-405 sheet to ASTM B127” is a product that does not exist. And a grade whose sulphur is deliberately raised to 0.060 % is a poor choice for welded fabrication, given that nickel alloys embrittle with sulphur at temperature — specify N04400 for anything that will be welded.

Monel K-500 is UNS N05500 / 2.4375 and is age-hardenable: Al 2.30–3.15 % and Ti 0.35–0.85 % precipitate Ni₃(Ti,Al). Its specifications are ASTM B865, QQ-N-286 and AMS 4676 — not B127/B164/B165 and not QQ-N-281. Aged, it reaches 965–1310 MPa tensile and 27–38 HRC. And critically it is effectively non-magnetic (permeability ≈1.001–1.002). Alloy 400 cannot be heat-treated to K-500 strengths — it hardens only by cold work.​‌​​‌​

Composition (B127/B164/B165, identical across all three): Ni (+Co) 63.0 % min — a MINIMUM, not a maximum · Cu 28.0–34.0 % — a band with both ends specified · Fe ≤2.5 % · Mn ≤2.0 % · C ≤0.30 % · Si ≤0.50 % · S ≤0.024 %. Why nickel is a floor and copper a band: nickel is the corrosion-controlling element and the matrix former, and specifying it as a minimum guarantees the reducing-acid and caustic performance. Copper is bounded at both ends: too little and you lose the seawater and HF behaviour; too much and the alloy drifts toward the copper-rich cupronickels, dropping the Curie point and the nickel content and degrading reducing-acid resistance.

What the small iron and manganese do. Iron (≤2.5 %) is a deliberate residual, not a tramp element — the EN/DIN name is NiCu30Fe. It improves impingement and erosion resistance in flowing seawater and contributes solid-solution strengthening. Manganese (≤2.0 %) is a deoxidiser and, critically, a sulphur scavenger: it ties up residual sulphur as MnS and suppresses the low-melting nickel-sulphide grain-boundary films that cause hot-shortness in hot working and welding. The filler metal takes this further — ERNiCu-7 carries up to 4 % Mn and 1.5–3.0 % Ti.​‌​​‌​

Two real chemistry divergences — a dual-certification trap. (1) Carbon: ASTM/ASME allow 0.30 % max; one European mill runs 0.15 % max on its own product. Both are “to specification”. (2) Iron minimum: ASTM sets NO iron minimum; EN/DIN NiCu30Fe requires Fe ≥1.0 %. Material fully compliant with ASTM B127 at Fe = 0.4 % would fail an EN 2.4360 order.

Mechanical Properties — Minimums and Typicals​‌​​‌​

STRENGTH VALUES
Yield (MPa)Tensile (MPa)ASTM B164 · bar, annealed480170ASTM B164 · bar, hot-worked552276ASTM B164 · bar, cold-drawn + stress-relieved600415ASTM B127 · hot-rolled plate, annealed485195ASTM B127 · hot-rolled plate, as-rolled515275ASTM B127 · cold-rolled sheet and strip, annealed485195ASTM B127 · cold-rolled sheet and strip, hard690620ASTM B165 · seamless tube, annealed (OD <= 127 mm)480195ASTM B165 · seamless tube, stress-relieved585380ASTM B564 · forging, annealed483172Typical · bar, annealed517172Typical · bar, cold-drawn + stress-relieved579380
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ConditionHardnessYield MPaTensile MPaElongation
ASTM B164 · bar, annealed—​‌​​‌​170480​‌​​‌​35%
ASTM B164 · bar, hot-worked​‌​​‌​—276​‌​​‌​55230%​‌​​‌​
ASTM B164 · bar, cold-drawn + stress-relieved—​‌​​‌​415600​‌​​‌​20%
ASTM B127 · hot-rolled plate, annealed​‌​​‌​—195​‌​​‌​48535%​‌​​‌​
ASTM B127 · hot-rolled plate, as-rolled—​‌​​‌​275515​‌​​‌​25%
ASTM B127 · cold-rolled sheet and strip, annealed​‌​​‌​—195​‌​​‌​485-58535%​‌​​‌​
ASTM B127 · cold-rolled sheet and strip, hard—​‌​​‌​620690​‌​​‌​2%
ASTM B165 · seamless tube, annealed (OD <= 127 mm)​‌​​‌​—195​‌​​‌​48035%​‌​​‌​
ASTM B165 · seamless tube, stress-relieved—​‌​​‌​380585​‌​​‌​15%
ASTM B564 · forging, annealed​‌​​‌​—172​‌​​‌​48335%​‌​​‌​
Typical · bar, annealed60-80 HRB​‌​​‌​172-345517-620​‌​​‌​35-60%
Typical · bar, cold-drawn + stress-relieved​‌​​‌​—380-690​‌​​‌​579-827—​‌​​‌​
The first ten rows are SPECIFICATION MINIMUMS for room temperature; the last two rows are producer TYPICAL ranges, not specification requirements, and the two must not be mixed. Because N04400 is not precipitation hardenable, the rows are split by PRODUCT FORM and TEMPER (annealed, hot-worked, cold-worked plus stress-relieved), not by ageing condition. The AMS rows are a separate specification family; their numerical minimums could not be confirmed by 4 independent sources and are therefore NOT in this table. When ordering to an AMS number, the values must be confirmed from the specification text. In the chart, a value given as a range is drawn at its lower bound; the full range is in the table. The rows are split by product form and temper, not by AGEING CONDITION; N04400 is not precipitation hardenable. In ASTM B127, the tensile strength of cold-rolled annealed sheet and strip is bounded both below and ABOVE (485-585 MPa). The other annealed rows have a lower bound only. In ASTM B127 the quarter-hard, half-hard and three-quarter-hard tempers are defined by Rockwell B hardness only, with no tensile or yield minimum; those tempers are not in this table. ASTM B164 has a separate table for wire, defined only by tensile strength bands (annealed 483-586 MPa, No. 0 temper 552-655 MPa, No. 1 temper 621-758 MPa, regular temper 758-965 MPa); because no yield or elongation minimum is given, no wire row is in this table. In ASTM B165 the yield minimum of annealed tube depends on outside diameter: 195 MPa up to 127 mm, 170 MPa above it. Tensile and elongation are the same. The numerical minimums of AMS 4544, 4574, 4675, 4730 and 4731 could not be confirmed by 4 independent sources and are therefore NOT in this table.

ASTM Specification Minimums (what you can enforce on a certificate)

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B127 — hot-rolled plate, annealedTensile ≥ 485 MPa (70 ksi) · Yield ≥ 195 MPa (28 ksi) · Elongation ≥35 %​‌​​‌​
B127 — hot-rolled plate, as-rolledTensile ≥515 MPa · Yield ≥275 MPa · Elongation ≥25 %​‌​​‌​
B127 — cold-rolled sheet, annealedTensile 485–585 MPa (a band, not just a floor) · Yield ≥195 MPa · Elongation ≥35 %​‌​​‌​
B127 — cold-rolled sheet/strip, hardTensile ≥690 MPa · Yield ≥620 MPa · Elongation ≥2 %​‌​​‌​
B165 — seamless pipe/tube, annealed, ≤5 in ODTensile ≥480 MPa · Yield ≥ 195 MPa · Elongation ≥35 %​‌​​‌​
B165 — annealed, >5 in ODTensile ≥480 MPa · Yield ≥ 170 MPa · Elongation ≥35 %​‌​​‌​
B165 — stress-relieved, all sizesTensile ≥ 585 MPa · Yield ≥ 380 MPa · Elongation ≥ 15 %​‌​​‌​
B164 — rod/bar/wire, annealed (all sizes)Tensile ≥480 MPa · Yield ≥170 MPa · Elongation ≥35 %​‌​​‌​
B164 caveatB164’s diameter bands overlap inconsistently in places, and only the row above is confirmed in two independent publishers. The designing engineer must read the current B164 Table 1 itself​‌​​‌​
F468 Class A (N04400) bolts⌀6.4–19 mm: 550–895 MPa tensile, yield ≥275 MPa, elongation 20 %, 75 HRB–25 HRC · ⌀22–38 mm: 480–895 MPa, yield ≥205 MPa. The 25 HRC cap sits below the NACE 35 HRC limit, so F468 Class A is inherently MR0175-conformant on hardness​‌​​‌​
The EN / VdTÜV Route — DIFFERENT from ASTM

Annealed (EN/VdTÜV)​‌​​‌​Rm ≥ 450 MPa · Rp0.2 ≥ 175 MPa · A ≥ 30 %
Stress-relieved (EN/VdTÜV)​‌​​‌​Rm 550–600 MPa · Rp0.2 275–415 MPa · A ≥20 %
This is not a rounding difference​‌​​‌​The ASTM annealed floor is 480–485 / 195 MPa / 35 %; the EN-VdTÜV floor is 450 / 175 MPa / 30 %. ASTM is the more demanding on every axis. A “2.4360 certified” plate is not automatically B127-compliant
QQ-N-281 diverges too​‌​​‌​Cold-worked/stress-relieved: QQ-N-281 600/415 MPa, B164 585/380 MPa. Hot-worked/stress-relieved: QQ-N-281 550/275 MPa, B164 585/345 MPa. Dual certification requires meeting the higher of each pair, which is not automatic

Typical values (NOT minimums, not enforceable): annealed rod 517–620 MPa tensile / 172–345 MPa yield / 60–35 % elongation / 110–149 HB · cold-drawn and stress-relieved rod 579–827 MPa / 379–690 MPa / 40–22 % / 160–225 HB · annealed sheet 482–586 MPa / 207–310 MPa / 45–35 % / 65–80 HRB. Two publishing traps: (1) the originator’s typical table is very widely reproduced with the tensile and yield columns transposed (giving the absurd “annealed rod: 75–90 ksi yield, 25–50 ksi tensile”) — the correct reading is tensile 75–90 ksi, yield 25–50 ksi. (2) Some pages publish typical figures as minimums (“UTS min 82,000 psi, elongation 48 % minimum”) — the enforceable ASTM minimums are 70 ksi / 28 (or 25) ksi / 35 %, and quoting typicals as minimums produces rejectable certificates.​‌​​‌​

Magnetic Behaviour — the Commercially Dangerous Point

Monel 400 is not a non-magnetic alloy, and almost every distributor gets this wrong.​‌​​‌​

Its Curie temperature is approximately 21–49 °C — inside the ambient range. The originator’s own words: “The Curie temperature lies within the ambient range. It is affected by variations in chemical composition. The values shown represent the range which can be expected from normal production; therefore, some heats will be magnetic at room temperature and others not.” And its own recommendation: “If there is a strong requirement for nonmagnetic characteristics, other MONEL alloys should be considered.” Two distributors state plainly that alloy 400 is “slightly magnetic at room temperature”.

What that means in practice: (1) Two conforming heats from the same mill can behave differently on a magnet — the Ni:Cu balance and the iron level move the Curie point across room temperature. (2) It is temperature-dependent within the service range: a part that is magnetic in a cold warehouse in January may be non-magnetic in a 55 °C process line — and no heat treatment fixes this. (3) There is no permeability limit in B127/B164/B165; a magnetic-permeability requirement is not a standard property and must be negotiated as a supplementary requirement with heat selection and measurement — and even then cannot be reliably met. (4) If the customer genuinely needs non-magnetic, sell them K-500 (permeability ≈1.001–1.002), not alloy 400. No numeric permeability for N04400 could be verified — no mill publishes one, precisely because it is not a stable property. Do not put a permeability figure on the page.​‌​​‌​

Welding and Heat Treatment

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HEAT TREATMENT — SCHEMATIC

ANNEALING — standard delivery condition
Step​‌​​‌​ANNEALING — standard delivery condition
Summary​‌​​‌​Fully softens and recrystallises cold-worked material. It gives no increase in strength; this is the alloy’s normal delivery and corrosion-service condition.
Temperature​‌​​‌​Open/strand annealing: 871-982 °C (1600-1800 °F) — Special Metals, Corrosion Materials. Box annealing: 760-816 °C (1400-1500 °F) — Special Metals. Producer bands: 704-982 °C, typically 871-982 °C (Carpenter Technology and High Temp Metals) · 700-900 °C, preferably about 825 °C (VDM Metals) · 760-980 °C (Jacquet) · 900 °C (Combined Metals, wire). Combined band: 700-982 °C.
Time​‌​​‌​2-10 minutes in open annealing; 1-3 hours in box annealing (Special Metals, Corrosion Materials). VDM Metals ties it to section: for d <= 10 mm, t = d x 3 min/mm. No single figure could be confirmed by 4 independent sources, so a band is given.
Cooling​‌​​‌​Water quench or accelerated air cooling. Special Metals and Corrosion Materials call for a rapid quench; VDM Metals calls for cooling accelerated with air.
Purpose​‌​​‌​The standard delivery condition for corrosion service and general use. The annealed minimums of ASTM B164 (480/170 MPa), ASTM B127 and B165 (485/195 MPa) and ASTM B564 (483/172 MPa) apply in this condition.
Specifications​‌​​‌​AMS 4544 (sheet, strip, plate) · AMS 4574 (seamless tubing) · AMS 4575 (brazed tubing) · AMS 4730 and AMS 4731 (wire, ribbon) · ASTM B127 · ASTM B164 · ASTM B165 · ASTM B564
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STRESS RELIEVING
StepSTRESS RELIEVING​‌​​‌​
SummaryRemoves internal stresses in hot- or cold-worked product without recrystallisation. It lowers tensile and yield strength slightly and raises elongation slightly.​‌​​‌​
Temperature538-566 °C (1000-1050 °F) — the band on which 4 independent sources agree: Special Metals, Corrosion Materials, Carpenter Technology, High Temp Metals. European producer practice goes above this: Special Metals gives a second band of 538-649 °C (1000-1200 °F) and VDM Metals gives 550-650 °C (1022-1202 °F) for stress relief annealing; that upper branch was found in only 3 independent sources, so it is stated separately and is NOT merged into 538-566 °C.​‌​​‌​
Time1-2 hours (Special Metals, Corrosion Materials, Carpenter Technology, High Temp Metals).​‌​​‌​
CoolingSlow cooling. Corrosion Materials requires slow cooling to limit distortion.​‌​​‌​
PurposeServices with a stress corrosion cracking risk: mercury and mercury salts, moist aerated hydrofluoric or fluosilicic acid vapour, ammonia at elevated temperature. Also for dimensional stability after machining.​‌​​‌​
SpecificationsASTM B165 defines ‘stress-relieved’ as a separate delivery condition with minimums of 585/380 MPa and 15% elongation. In ASTM B164, cold-worked bar is ordered as ‘stress-relieved’.​‌​​‌​

STRESS EQUALIZING
Step​‌​​‌​STRESS EQUALIZING
Summary​‌​​‌​A short low-temperature cycle. It raises the low-offset yield strength of cold-drawn product without markedly changing other properties. It does not soften or recrystallise.
Temperature​‌​​‌​300 °C (575 °F) — Special Metals, Corrosion Materials, Heanjia Super Metals. Jacquet gives the same treatment as a ‘low-temperature stress relief’ at about 300 °C (575 °F).
Time​‌​​‌​3 hours (Special Metals, Corrosion Materials, Heanjia Super Metals). Jacquet gives 1-3 hours.
Cooling​‌​​‌​Rapid quench (Corrosion Materials).
Purpose​‌​​‌​To raise the yield strength of cold-drawn bar and wire without the softening that annealing would bring. It is NOT sufficient to remove a stress corrosion cracking risk; that requires the 538-566 °C stress relief.
Specifications​‌​​‌​Not a specification requirement; it is producer practice.
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CONDITION TO AVOID — sulphur-bearing atmosphere
StepCONDITION TO AVOID — sulphur-bearing atmosphere​‌​​‌​
SummaryThe heat-treating atmosphere must be sulphur-free and reducing. Sulphur embrittles the nickel-copper alloy and the effect is irreversible; furnace fuel, oil and marking-pen residues are all sources.​‌​​‌​
TemperatureAttack is reported above roughly 370 °C (700 °F) in sulphur-bearing gases and above roughly 260 °C (500 °F) in molten sulphur (Jacquet).​‌​​‌​
Time—​‌​​‌​
Cooling—​‌​​‌​
PurposeThe surface is cleaned completely before heat treatment and the furnace atmosphere is kept sulphur-free (Carpenter Technology, High Temp Metals, Jacquet, VDM Metals).​‌​​‌​
SpecificationsNot a specification requirement; it is the common warning of every producer bulletin.​‌​​‌​

NONE — SOLUTION TREAT + AGE
Step​‌​​‌​NONE — SOLUTION TREAT + AGE
Summary​‌​​‌​N04400 is not precipitation hardenable. There is NO solution treat plus age step (H900, H1025 and so on) and none is applied. Strength is raised only by cold work; if a heat-treatable nickel-copper alloy is wanted, Monel K-500 (UNS N05500) is a separate material.
Temperature​‌​​‌​—
Time​‌​​‌​—
Cooling​‌​​‌​—
Purpose​‌​​‌​—
Specifications​‌​​‌​—
The diagram is schematic; the time axis is not to scale. N04400 is a solid solution alloy and is NOT PRECIPITATION HARDENABLE — there is no ageing step, and since no published TTT/CCT curve was used, no curve is drawn. The diagram is schematic; the time axis is not to scale. No curve is drawn because no published TTT/CCT curve was used. Monel 400 is a SOLID SOLUTION alloy. There is NO ageing step (nothing like H900, H1025 or H1150); an order text showing such a recipe is wrong. Sources spread the annealing temperature between 700 °C and 982 °C. The difference comes from the method: open annealing (short time, high temperature) and box annealing (long time, lower temperature) give the same result. No single figure is written; a band is left. Stress relieving and stress equalizing are NOT the same thing: stress equalizing is 300 °C for 3 hours and does not remove a stress corrosion cracking risk. Columbia Metals gives 760-815 °C for ‘stress relief’, far above the 538-566 °C band of the other four sources and coinciding with the annealing band. The conflict is recorded and the figure is not on the card. No significant effect of cooling rate on the hardness of annealed material is reported (Special Metals).

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Welding

Processes: GTAW (including hot-wire), GMAW (spray, short-circuit, pulsed), SMAW, FCAW, SAW, plasma. GTAW is the reference process for thin sections and root passes. Preheat is not required — the only exception: if the base metal is ≤2 °C, warm the metal within about 300 mm of the joint to a few degrees above ambient, solely to stop condensation causing porosity, not for metallurgical reasons. Interpass temperature max 150 °C (single-sourced). Heat-input maxima (single-sourced): manual GTAW ≤8 kJ/cm, plasma ≤10 kJ/cm, GMAW ≤11 kJ/cm, SAW ≤7 kJ/cm. No post-weld heat treatment is required: “Neither pre- nor post weld heat treatments are normally required.” A stress relief or anneal may be desirable for heavily stressed structures going into SCC-inducing environments.​‌​​‌​

The number-one failure mode: sulphur, lead and phosphorus embrittlement. The originator’s joining handbook states it plainly: “Cleanliness is the single most important requirement for successfully welding nickel and nickel-based alloys. At high temperatures, nickel and its alloys are susceptible to embrittlement by sulfur, phosphorus, lead, and some other low-melting point substances.” The same handbook carries a photograph of cracking captioned “Typical effect of lead in MONEL alloy 400 welds“, and a failure case from a fatty-acid tank previously lined with lead and lined with Monel 400 without proper cleaning. Contamination sources named: grease, oil, paint, cutting fluids, marking crayons and inks, processing chemicals, machine lubricants, temperature indicating sticks, pellets and lacquers. Cleaning regime: vapour degrease or solvent swab for oils and crayon; alkaline cleaner for paint — but alkaline residues must themselves be removed, and wire brushing will not do it; a hot-water spray and scrub is required; embedded process chemicals need grinding, abrasive blasting or a 10 vol-% HCl swab followed by a thorough water wash. Clean a band of at least 50 mm either side of the joint, including plate edges and the bore of tubulars. The mill’s own illustration is the standard to hold a fabricator to: a root bend specimen cracked on the side wiped with a dirty cloth and sound on the side wiped with a clean one.

Porosity and flow. Ni-Cu weld metal is porosity-prone; the countermeasure is chemical — ERNiCu-7 carries 1.5–3.0 % Ti and up to 4 % Mn as deoxidiser and desulphuriser. Consequently: do not weld autogenously and do not use sheared strips of the base metal as filler — base-metal N04400 has no titanium, so the deposit has no deoxidiser and will be porous. The mill’s warning: “The molten pool must be kept as quiet as possible to prevent burning out of the deoxidizing elements“; keep the hot filler end inside the gas shield. Also: “Nickel alloy weld metal does not flow or spread as readily as steel weld metal.” The consequences: all beads must be slightly convex — “flat or concave beads such as those commonly encountered when joining stainless and carbon steels should be avoided”; bevel to an 80° included V (against about 60–70° for steel); use smaller root lands; and do not try to buy penetration with amperage — “increases in weld current will not significantly increase the penetration of the arc“, and excess current spalls the SMAW flux coating. Dilution: target at least 50 %, preferably 75 % filler metal in the completed weld.​‌​​‌​

Heat treatment

Monel 400 is a solid-solution alloy and is NOT hardenable by heat treatment. The originator: “MONEL alloy 400 is a solid-solution alloy that can be hardened only by cold working.” Verified in three independent sources; this is settled. Strength is set by the amount of cold or hot work plus the thermal cycle, and by nothing else.​‌​​‌​

Heat-Treatment Temperatures

Anneal — open/continuous furnace​‌​​‌​871–982 °C (1600–1800 °F), 2–10 minutes, rapid cool or quench
Anneal — box/batch furnace​‌​​‌​760–816 °C (1400–1500 °F), 1–3 hours at temperature
Anneal — EN practice​‌​​‌​700–900 °C, preferably about 825 °C; thickness rule ≤10 mm → 3 min/mm; 10–20 mm → 30 + (d−10)×2 min; >20 mm → 50 + (d−20)×1 min; accelerated air cool
Stress relief​‌​​‌​538–566 °C (1000–1050 °F) for 1–2 hours (US practice) or 550–650 °C (EN practice) — the two windows agree well. Against SCC: 538–649 °C for 1 hour, slow cool
Stress equalising​‌​​‌​About 302 °C (575 °F) for about 3 hours — raises yield strength without much else changing
Hot working​‌​​‌​649–1177 °C (1200–2150 °F); heavy reductions 927–1177 °C; optimum about 1093 °C. One European mill gives 800–1200 °C
A mislabelled “stress relief”​‌​​‌​One distributor publishes stress relief as 760–815 °C. That is the box-annealing range; it will recrystallise the metal and destroy the cold-worked strength the buyer is paying for. Three sources put stress relief at 538–650 °C
Embrittlement window​‌​​‌​— There is none. No source identifies a sigma-phase, 475 °C or similar intermetallic embrittlement window for N04400, which is expected for a single-phase Ni-Cu solid solution with no chromium. The embrittlement risks for this alloy are environmental, not thermal (sulphur, lead, mercury). Do not invent a temper-embrittlement range. Anneal in a sulphur-free atmosphere

Machining and Forming​‌​​‌​

Monel 400 work-hardens rapidly, at a rate that sits between mild steel and 304 stainless. The practical rules follow directly: positive rake angles, sharp tools, a rigid setup and a continuous cut — never dwell or rub, which glazes the surface and work-hardens it ahead of the tool. Carbide over HSS; TiC and TiAlN coatings handle the heat. Flood coolant. Intermediate annealing is required during multi-stage cold work, and a stress-relief anneal is recommended after forming. Cold-drawn and stress-relieved bar machines better than annealed bar. Cutting speeds diverge by about 10× across publishers: one gives turning at 46–61 m/min (150–200 sfm), another at 155–205 m/min with a 45 % machinability rating. These cannot be reconciled or averaged; 46–61 m/min is consistent with conventional carbide turning of a work-hardening nickel alloy, while 155–205 m/min is only plausible with advanced coated carbide or ceramic tooling and high-pressure coolant. Publish both with attribution, or neither. One outright error in circulation: a comparison article states that “Monel 400 cannot be hot worked” — that is false; three sources publish a hot-working range for N04400. Free-machining alternative: if the part is a screw-machine component, not welded and not a pressure boundary, R-405 (N04405) exists for exactly that — but in bar and rod only.

Corrosion — the Alloy’s Reason to Exist​‌​​‌​

Monel 400 · Corrosion Behaviour

Seawater — the flow-regime distinction​‌​​‌​Excellent in flowing seawater: the originator’s words, “while alloy 400 products exhibit very low corrosion rates in flowing seawater…”, with superior resistance where cavitation and erosion matter. …BUT THE SAME SENTENCE CONTINUES: “…stagnant conditions have been shown to induce crevice and pitting corrosion.” That is the mill warning about its own product, and most supplier pages erase it
Seawater — numbers​‌​​‌​Typically <0.025 mm/yr in aerated flowing seawater (single-sourced). There is no published critical velocity in clean seawater — this is its structural advantage over the copper-nickels
Hydrofluoric acid​‌​​‌​The signature duty — with a qualifier. The originator: “MONEL alloy 400 offers exceptional resistance to hydrofluoric acid in all concentrations up to the boiling point.” The omitted qualifier is aeration: that rating is for un-aerated acid; “aeration increases the corrosion rate”, and oxidising salts increase it further. More pointedly, one European mill lists “moist, aerated HF vapours” under NOT RESISTANT, treats it as a stress-cracking risk, and requires stress-relief annealing before exposure to HF vapour (and to mercury). Field experience from an instrument maker: HF is “prone to triggering stress corrosion cracking, especially when oxygen is present in the vapor phase“; “even a small amount of oxygen in the tube can increase SCC risk, as it becomes trapped in the most highly stressed area”. What can safely be asserted: 400 is the standard material for HF in the liquid phase, air-free, at all concentrations to boiling; in aerated HF, especially moist aerated vapour, it is subject to stress-corrosion cracking and components must be stress-relieved before service
Hydrochloric acid​‌​​‌​Resistant under reducing (de-aerated) conditions. Quantified (single-sourced): <0.25 mm/yr in 10 % HCl at room temperature; usable below 20 % un-aerated and below 10 % aerated at room temperature, and up to about 204 °C within those ranges. But air-saturated HCl limits you to 3–4 % above room temperature
Sulphuric acid​‌​​‌​Resistant to many forms of sulphuric acid under reducing conditions. One source’s “resistant up to 80 % concentration” is single-sourced, states no temperature and no aeration state, and should be treated as unreliable. The defensible statement is the mill’s “reducing conditions” qualifier
Caustic / alkalis​‌​​‌​Resistant to sodium hydroxide across the entire concentration range, and resistant to caustic stress-corrosion cracking in strong alkalis at high temperature. But do not oversell it: corrosion rates rise in concentrated caustic soda and caustic potash at elevated temperature, and Nickel 200/201 outperforms alloy 400 in alkalis. For concentrated hot caustic evaporator duty, nickel is the right answer, not 400
Chloride stress-corrosion cracking​‌​​‌​Essentially immune — four sources. This is a genuine and defensible advantage over the austenitic stainless steels, and it is why 400 survives hot chloride duty where 304/316 crack
Cryogenic​‌​​‌​“The alloy does not undergo a ductile-to-brittle transition even when cooled to the temperature of liquid hydrogen” (single-sourced, mill) — commercially significant for LNG and cryogenic enquiries
Where Monel 400 Is NOT Good — the Honest List

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Oxidising acids“Rapidly attacked by nitric acid“; “not useful in oxidizing acids”. Disqualifying​‌​​‌​
Oxidising conditions generallyCorrosion rates “increase significantly”. Not a substitute for Ni-Cr-Mo alloys in strongly oxidising or mixed-acid service​‌​​‌​
Oxidising salts and impuritiesFerric chloride, ferric sulphate, chromates, nitrates, peroxides and cupric salts all cause attack — even as impurities in an otherwise acceptable reducing acid. This is the commonest way a good HF or HCl selection goes wrong​‌​​‌​
HypochloritesCause corrosion. The relevant consequence: chlorinated seawater is not the same duty as natural seawater​‌​​‌​
Stagnant / low-flow seawaterCrevice and pitting corrosion — the mill’s own warning. Flanges, gaskets, tubesheet joints, dead legs and lay-up periods​‌​​‌​
Ammonia“Rapidly attacked by ammonia systems.” It resists anhydrous ammonia and dilute (~3 %) ammonium hydroxide, but aerated aqueous ammonia above roughly 3 % causes SCC — the classic copper-bearing-alloy ammonia crack​‌​​‌​
MercuryStress-cracking risk. One mill explicitly requires stress-relief annealing before mercury exposure. One source claims it “resists amalgamation at moderate temperatures” — that directly contradicts the mill; follow the mill and treat mercury as a hazard​‌​​‌​
Sulphur-bearing gasesAttacked above about 371 °C (700 °F)​‌​​‌​
Molten sulphurAttacked above about 260 °C (500 °F)​‌​​‌​
BiofoulingThe copper content gives some antifouling benefit, but less than the copper-nickels, and quantitative data is unavailable. Fouling plus stagnation is the crevice-corrosion trigger​‌​​‌​
Service Temperature Limits — Different Bases, Not to Be Averaged

Oxidation in air​‌​​‌​Useful to 538 °C (1000 °F) in oxidising atmospheres. “Higher temperatures may be employed if the alloy is in a reducing environment.“
Mechanical-property basis​‌​​‌​Good properties to about 549 °C (single-sourced); one source rates continuous service at 427 °C
ASME B&PV Code​‌​​‌​480 °C (900 °F) (single-sourced)
VdTÜV 263​‌​​‌​−10 to +425 °C (European pressure equipment)
In sulphur-bearing gas​‌​​‌​371 °C — in sour or sulphur-bearing service this overrides everything else
In molten sulphur​‌​​‌​260 °C
Low temperature​‌​​‌​No ductile-to-brittle transition down to liquid-hydrogen temperature
Rule for this page​‌​​‌​Quote 538 °C for general, non-pressure service in air; 425 °C (VdTÜV) or 480 °C (ASME) for code pressure equipment; and state plainly that sulphur-bearing service drops the limit to about 371 °C. What sets the ceiling is not melting (1300–1350 °C) — it is oxidation, creep and allowable stress, and decisively in sour service, sulphidation

Physical properties: density ≈8.8 g/cm³ · melting range 1300–1350 °C · modulus of elasticity at 20 °C 179–182 GPa · Poisson’s ratio 0.32 · electrical resistivity ≈51 µΩ·cm · thermal conductivity at 20 °C 21.8 or 23.0 W/m·K (sources about 5 % apart) · specific heat 427 or 452 J/kg·K (about 6 % apart) · mean thermal expansion 13.8 × 10⁻⁶/K.​‌​​‌​

Frequently Asked Questions

Monel 400, K-500, 70/30 copper-nickel or super duplex for seawater — when is each actually required?​‌​​‌​

These four are not interchangeable, and the deciding factor is rarely corrosion rate — it is flow regime, strength and price. 70/30 copper-nickel (C71500) is the default for seawater piping and condenser tubing, and the cheapest. Its constraint is velocity: design maxima of roughly 2.9 m/s once-through, 2.4 m/s two-pass and 2.3 m/s in 4–8 inch piping with short-radius bends, plus a minimum of about 0.9 m/s to prevent under-deposit attack. Above those velocities it erodes. Monel 400 is what you buy when velocity or cavitation exceeds what copper-nickel tolerates — pump impellers, valve trim, propeller shafts, seawater-lift components. It has no published critical velocity in clean seawater and superior cavitation resistance. Its weakness is the mirror image: stagnant, creviced or fouled seawater causes pitting and crevice corrosion, and annealed it is only a ~170–195 MPa yield material. K-500 enters when you want the same Ni-Cu corrosion behaviour but need strength: aged, 965–1310 MPa tensile and 27–38 HRC — shafts, bolting, stems. It is also the genuinely non-magnetic one. You pay in price and in hydrogen-embrittlement risk; and it is not freely approved under NACE — it is restricted to wellhead and Christmas-tree components and non-pressure-containing valve internals, and is barred from valve shafts and stems. Super duplex beats both on strength (≥550 MPa yield) and pitting (PREN ≥40) and is usually cheaper — but it lacks Monel’s high-nickel margin against chloride SCC and is limited in sour service to 232 °C and 0.20 bar H₂S. In short: low velocity → copper-nickel; high velocity or cavitation → 400; strength as well → K-500; strength and pitting first with low stagnant-chloride SCC risk → super duplex.

“Exceptional resistance to HF at all concentrations to boiling” — is that really true?​‌​​‌​

You have to read the whole sentence. The mill’s statement is real and correct: Monel 400 offers “exceptional resistance to hydrofluoric acid in all concentrations up to the boiling point“; this is the alloy’s signature duty and HF alkylation units are built on it. But the qualifier is aeration, and it is dropped almost everywhere. That rating is for un-aerated acid: “aeration increases the corrosion rate”, and oxidising salts increase it further. More pointedly, one European mill lists “moist, aerated HF vapours” under NOT RESISTANT, identifies it as a stress-corrosion cracking risk, and requires stress-relief annealing before exposure to HF vapour. Field experience from an instrument manufacturer points the same way: HF is “both highly corrosive and prone to triggering stress corrosion cracking, especially when oxygen is present in the vapor phase“; “even a small amount of oxygen in the tube can increase SCC risk, as it becomes trapped in the most highly stressed area”. The consequences for the order and the design: (1) for liquid-phase, air-free HF, 400 is the standard material with no concentration limit; (2) vapour phase and aerated HF are a different duty — components must be stress-relieved at 538–650 °C and stress levels kept to a minimum; (3) oxidising impurities in the acid (ferric salts, chromates, peroxides) will spoil a good selection, so ask about them as part of the plant chemistry. A footnote: alloy 400’s HF-vapour SCC resistance is slightly better than K-500’s, “however, this advantage is minimal”.

We ordered “non-magnetic Monel” and a magnet sticks to it — is it the wrong material?​‌​​‌​

Most likely the material is right and the order was wrong. Monel 400’s Curie temperature is approximately 21–49 °C — inside the ambient range. The originator’s own bulletin says so plainly: “The Curie temperature lies within the ambient range… therefore, some heats will be magnetic at room temperature and others not“, and adds: “If there is a strong requirement for nonmagnetic characteristics, other MONEL alloys should be considered.” So two heats from the same mill, both fully compliant with ASTM B127/B164/B165, can behave differently on a magnet; what decides it is the Ni:Cu balance and the iron level. It is also temperature-dependent: a part that is magnetic in a cold warehouse in January may be non-magnetic in a 55 °C line — and no heat treatment fixes it. Third, B127, B164 and B165 contain no magnetic-permeability requirement; it is not a standard property. A permeability requirement can only be negotiated as a supplementary requirement with heat selection and actual measurement, and even then cannot be reliably guaranteed. What to do: if the requirement is real, specify Monel K-500 — permeability ≈1.001–1.002, and it stays that way at low temperature. Finally: no mill publishes a numeric permeability for N04400, precisely because it is not a stable property, so a datasheet that gives you a figure is inventing it.

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Related grades

Monel K-500  ·  Waspaloy  ·  Nimonic 80A  ·  Haynes 25  ·  All nickel alloys →​‌​​‌​

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