Kovar / (1.3981) / ASTM F15

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Kovar / (1.3981) / UNS K94610 / ASTM F15

Kovar
UNS K94610 · W.Nr. 1.3981 · DIN 17745 · FeNi29Co17 · ~53% Fe – 29% Ni – 17% Co. Minor elements: C 0.02-0.04% max · Mn 0.30-0.50% max · Si 0.20% max · Cr 0.20% max · Cu 0.20% max · Mo 0.20% max · Al, Mg, Zr, Ti 0.10% max each · P and S 0.02% max. It is an iron-nickel-cobalt controlled-expansion alloy. ASTM F15 requires the iron, nickel and cobalt contents to be ADJUSTED by the manufacturer so that the alloy meets the expansion coefficient requirement; the figures given for those three elements are nominal. Other producer names: NILO alloy K, Alloy K, Rodar, Pernifer 2918.
Not to be confused with

Invar 36

For what
Its real job is the HERMETIC GLASS-TO-METAL SEAL. It is NOT PRECIPITATION HARDENABLE and cannot be hardened by heat treatment; its distinguishing property is not mechanical strength but THE SHAPE OF ITS THERMAL EXPANSION CURVE.
Forms
Round bar · flat bar · plate · sheet · strip · tube · wire · forging. All forms are supplied to order.
Standards
AMS 7726 — wire; SAE title ‘Iron-Nickel-Cobalt Alloy, Wire 53Fe – 29Ni – 17Co Low Expansion, Glass Sealing, Annealed’. · AMS 7727 — bars and forgings; SAE title ‘Iron-Nickel-Cobalt Alloy, Bars and Forgings 53Fe – 29Ni – 17Co Low Expansion, Glass Sealing’. · AMS 7728 — sheet, strip and plate; SAE title ‘Iron-Nickel-Cobalt Alloy, Sheet, Strip, and Plate, 53Fe – 29Ni – 17Co, Low Expansion Glass Sealing, Annealed’. · AMS-I-23011 / MIL-I-23011 Class 1 (‘Iron-Nickel Alloys for Sealing to Glasses and Ceramic’). · ASTM F15 — iron-nickel-cobalt sealing alloy; it covered wire, rod, bar, strip, sheet and tubing and was WITHDRAWN IN 2024 WITH NO REPLACEMENT. The last valid edition is F15-04(2022). · DIN 17745.
SPECIFICATION GAP: with the withdrawal of ASTM F15 in 2024, the only specification family left in force is AMS 7726/7727/7728. Those three numbers cover WIRE, BAR AND FORGINGS, and SHEET, STRIP AND PLATE; TUBING appears in none of them.
Advantage
The expansion CURVE is flat between 20 and 450 °C and follows the curve of borosilicate glass across that band. For NILO alloy K, Special Metals gives mean coefficients referenced to 20 °C of 20-100 °C: 6.0 · 20-200 °C: 5.5 · 20-250 °C: 5.3 · 20-300 °C: 5.1 · 20-400 °C: 4.9 · 20-500 °C: 6.2 x…
Welding
In glass-to-metal seal parts Kovar is joined by brazing and resistance welding rather than by fusion welding; where fusion welding is used, GTAW is chosen and the heat input is limited.
Limits
ABOVE 450 °C THE EXPANSION CURVE BREAKS DOWN. The inflection point is 450 °C; above it the coefficient rises sharply (the 20-500 °C mean is 6.2, the 600-700 °C value 7.8 and the 800-900 °C value 10.3 x 10-6/°C). The match with the glass ends and the seal is left under stress. The Curie temperature is 435 °C;
Compiled from manufacturer data sheets · confirm against the current specification before ordering

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On this page · click to jump
What Kovar IsStandards by Product FormTemperature LimitsProduct Forms With NO StandardChemical CompositionMechanical PropertiesPhysical PropertiesHeat TreatmentWelding, Soldering and PlatingMachiningCorrosionFrequently Asked QuestionsCommon Datasheet Errors



Kovar is a nickel-iron-cobalt based alloy with a specifically controlled coefficient of thermal expansion. Within the nickel alloy group it forms, together with Invar 36, the controlled expansion sub-class. Its UNS designation is K94610.

The alloy is formulated to give an expansion coefficient very close to that of borosilicate glass over the 20-400 °C range. That match makes it possible to form a hermetic, gas-tight joint between glass or ceramic and metal that does not crack under thermal cycling. Invar 36 aims at the lowest possible expansion, whereas Kovar aims to match a particular glass — that is the difference between them.​‌​​‌​

This property makes the material indispensable in electronic packaging and vacuum technology. Although the name Kovar is used commercially for most Fe-Ni-Co low expansion alloys, technically only material conforming to ASTM F15 is regarded as true Kovar.

It is used in electronics for transistor, diode and integrated circuit packages, TO-3 / TO-5 metal housings and microwave sealing components; in aerospace for hermetic sub-system enclosures and for the glass-to-metal seals of vacuum and laser tubes; in medical devices for pacemaker and implant bodies; and in optoelectronics for fibre optic connector housings.​‌​​‌​

Chemical Composition · Kovar (K94610)

Fe — Iron​‌​​‌​Bakiye
Ni — Nickel​‌​​‌​~29%
Co — Cobalt​‌​​‌​~17%
Mn — Manganese​‌​​‌​0.30% max
Si — Silicon​‌​​‌​0.20% max
C — Carbon​‌​​‌​0.04% max
Key Properties · Kovar

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Primary functionHermetic sealing to glass and ceramic​‌​​‌​
Expansion match20 – 400 °C controlled range, matched to borosilicate glass​‌​​‌​
Typical product formsPlate, strip, bar, machined parts​‌​​‌​
Standards and Equivalents · Kovar

Trade name​‌​​‌​Kovar
UNS​‌​​‌​K94610
W.Nr (DIN/EN)​‌​​‌​1.3981
ASTM​‌​​‌​F15
Available forms​‌​​‌​Round bar · Flat bar · Plate · Sheet · Tube · Forgings
All forms are supplied to order.

→ Contact us for Kovar stock availability, sizes and ASTM F15 certified supply.​‌​​‌​

Request a quote

Related grades​‌​​‌​

Invar 36  ·  Nickel 200  ·  Nickel 201  ·  Monel 400  ·  All nickel alloys →

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What Kovar Is — and Why It Is a MATCHED-Expansion Alloy, Not a Low-Expansion One

Kovar (UNS K94610 · W.Nr. 1.3981 · DIN designation FeNi29Co17 — some publishers write FeNi29Co18 · ASTM F15 · Chinese 4J29) is a ternary iron-nickel-cobalt alloy, nominally 29 % nickel – 17 % cobalt – balance iron. This cobalt-bearing Fe-Ni-Co family was historically developed under the name Fernico. Kovar contains no chromium and no molybdenum, is never bought for strength, and is not a corrosion alloy.​‌​​‌​

The one distinguishing sentence is this: Kovar exists not because its thermal expansion is low, but because the SHAPE of its expansion curve is tailored to that of borosilicate glass. Alloys that expand less than Kovar exist — Invar 36 heads the list and expands less than a quarter as much over 20–100 °C. But Invar does not match glass; Kovar does. What a hermetic glass-to-metal transition needs is not low expansion but a metal curve that FOLLOWS the glass curve throughout cooldown.

The second distinguishing fact is cobalt. Cobalt is there not only to shape the expansion curve but to make the oxide interface between glass and metal work: the bond forms through a deliberately grown nickel(II) oxide – cobalt(II) oxide film on the metal surface, and cobalt makes that oxide easier to melt and to dissolve in the molten glass. The proportion of iron oxide in such a seal is low, because cobalt reduces it. In a cobalt-free Fe-Ni alloy this mechanism does not work — the second reason you cannot substitute Invar for Kovar.​‌​​‌​

Honest Comparison · Invar 36 · “Invar 42” (Alloy 42) · Kovar

Invar 36
K93600/K93603 · 1.3912​‌​​‌​
Fe–36 Ni. 1.5 × 10⁻⁶/K over 20–100 °C · inflection 220 °C · Curie 279 °C. A dimensional-stability alloy. It does NOT match glass or ceramic — it expands far too little. No cobalt, therefore no oxide-interface mechanism. Uses: precision optics, metrology, composite tooling, LNG membranes
“Invar 42” = Alloy 42
K94100 · 1.3917 · NILO 42​‌​​‌​
Fe–42 Ni. 4.0–4.7 × 10⁻⁶/K over 30–300 °C · inflection 370 °C · Curie 330 °C. This is a glass/ceramic matching alloy and it matches silicon and alumina. IC lead frames, semiconductor packages. Sold as “Invar 42” but it is NOT the same alloy as Invar 36
Alloy 48
K94800​‌​​‌​
Fe–48 Ni. Inflection 460 °C. For soft (soda-lime) glasses, not for borosilicate
KOVAR
K94610 · 1.3981​‌​​‌​
Fe–29 Ni–17 Co. ~5.1 × 10⁻⁶/K over 20–300 °C · inflection 450 °C · Curie 435 °C. The shape of the curve is tailored to borosilicate glass (the 7052 family) and cobalt makes the oxide interface work. The only true hermetic glass-to-metal sealing alloy in this family. Uses: hermetic packages, vacuum tubes, microwave tubes, X-ray tubes, optoelectronic packages
The selection rule — one sentence​‌​​‌​If dimension is critical, Invar 36. If you need a hermetic seal to borosilicate glass, Kovar. If you need a match to silicon or alumina, alloy 42. These are NOT interchangeable.

Trade names — not all produced to the same specification​‌​​‌​

Kovar® is a registered trademark (CRS Holdings / Carpenter Technology). Other trade names for the same alloy: Nilo® K (Special Metals), Pernifer® 2918 (VDM Metals), Dilver® P, Rodar®, Nicoseal®, Telcoseal®, Fenicoloy®, Ulbravar®, Nicosel®. The Chinese equivalent is 4J29. All belong to the K94610 family, but carbon and impurity ceilings — and, more importantly, the as-delivered decarburisation condition — vary from mill to mill. If you are going to seal to glass, write “decarburised in wet hydrogen” separately into the order; the trade name does not guarantee it.

Standards by Product Form — and What Happened in 2024​‌​​‌​

STANDARDS BY PRODUCT FORM
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Product formStandards
Sheet, strip, plateAMS 7728 (‘Iron-Nickel-Cobalt Alloy, Sheet, Strip, and Plate, 53Fe – 29Ni – 17Co, Low Expansion Glass Sealing, Annealed’) · AMS-I-23011 / MIL-I-23011 Class 1 · ASTM F15 — WITHDRAWN in 2024, last edition F15-04(2022) · DIN 17745​‌​​‌​
Round bar, flat bar, forgingAMS 7727 (‘Iron-Nickel-Cobalt Alloy, Bars and Forgings 53Fe – 29Ni – 17Co Low Expansion, Glass Sealing’) · AMS-I-23011 / MIL-I-23011 Class 1 · ASTM F15 (withdrawn) · DIN 17745​‌​​‌​
WireAMS 7726 (‘Iron-Nickel-Cobalt Alloy, Wire 53Fe – 29Ni – 17Co Low Expansion, Glass Sealing, Annealed’) · AMS-I-23011 / MIL-I-23011 Class 1 · ASTM F15 (withdrawn) · DIN 17745​‌​​‌​
TubeNO AMS number — AMS 7726, 7727 and 7728 do not cover tubing · ASTM F15 did cover tubing but was withdrawn in 2024 · There is no product specification in force; the acceptance criteria must be written into the purchase order​‌​​‌​
Expansion coefficient acceptance criterionASTM F15 (withdrawn edition) acceptance band: 4.60-5.20 µm/m·°C over 30-400 °C and 5.10-5.50 µm/m·°C over 30-450 °C. Because the specification is not in force, this band must be written into the purchase order.​‌​​‌​
Chemical composition and numberingUNS K94610 · W.Nr. 1.3981 · DIN 17745 · FeNi29Co17​‌​​‌​
AMS numbers are given first, ASTM afterwards. The titles of all three AMS numbers were verified one by one from SAE records. The most important gap is TUBING: neither an AMS number nor an ASTM specification in force covers Kovar tube. Because ASTM F15 has been withdrawn, the expansion coefficient acceptance band must be written into the purchase order.

Kovar’s ASTM basis disappeared in 2024 and most distributor pages still do not publish this. Read this section before you quote.​‌​​‌​

Standards by Product Form · Kovar (K94610 / 1.3981)

Principal specification​‌​​‌​ASTM F15 — “Standard Specification for Iron-Nickel-Cobalt Sealing Alloy”. WITHDRAWN 2024, NO REPLACEMENT. The last valid edition is F15-04(2022). Scope: UNS K94610, nominally 29 % Ni – 17 % Co – 53 % Fe, for glass sealing in electronic applications. Forms covered: wire, rod, bar, strip, sheet and tubing
Wire​‌​​‌​SAE AMS 7726 — wire
Rod · bar · forgings​‌​​‌​SAE AMS 7727 — bars and forgings
Sheet · strip · plate​‌​​‌​SAE AMS 7728 — sheet, strip and plate
Tube​‌​​‌​Was covered by the withdrawn F15. Today: mill specification. Capillary tube is commercially available but has no product specification
Seamless or welded PIPE​‌​​‌​No specification, and there never was one. F15 covered tubing, not pressure pipe
Wrought fittings · flanges​‌​​‌​No specification
Bolts · nuts​‌​​‌​No specification
Castings​‌​​‌​Kovar has no cast equivalent and no casting specification. Hermetic package bodies are made from wrought material by deep drawing, stamping or machining
Welding wire​‌​​‌​No AWS classification. Matched Kovar filler wire is commercially available but sold to proprietary specification
Covered electrode​‌​​‌​No specification. Kovar is not welded with covered electrodes
Military​‌​​‌​MIL-I-23011 is cited by one distributor — single source, could not be independently verified
Europe​‌​​‌​Material number 1.3981. Two publishers cite DIN 17745 and AFNOR NF A54-301. No current, in-force EN product specification could be verified
ASTM F29​‌​​‌​One manufacturer’s bulletin also lists ASTM F29 on the NILO K line. Single source, and the scope of F29 could not be independently verified — confirm before writing it on a certificate
ASME IX P / F number​‌​​‌​— could not be verified. Do NOT publish a P or F number
ASME code acceptance​‌​​‌​No published ASME pressure-vessel allowable stress table for Kovar could be verified. Kovar is not marketed as a pressure-boundary material; do not look for a maximum code temperature
Inspection document​‌​​‌​EN 10204 3.1; 3.2 for critical hermetic work

What the withdrawal of F15 means in practice​‌​​‌​

The alloy is not banned; the document the certificate rested on is gone. In the same 2024 round ASTM F1684 (low-expansion alloys including Invar) and ASTM F30 (Fe-Ni sealing alloys) were also withdrawn — the entire controlled-expansion family lost its ASTM basis at once. For Kovar this carries particular weight, because F15 was not only a chemistry table: it also carried the expansion acceptance requirements and the hardness/temper requirements.
Three practical consequences. (1) Cite the standard with its edition year in the purchase text: “ASTM F15-04(2022), withdrawn edition”. (2) AMS 7726 / 7727 / 7728 remain in force and are the strongest published specification route left for Kovar — cite the one that matches the form (wire / bar-forging / sheet-strip-plate). (3) Move the work the standard used to do into the order text: chemical ranges, expansion measurement range and acceptance criterion, temper and hardness, and the as-delivered heat treatment condition (decarburised in wet hydrogen or not?).

Temperature Limits — Kovar’s Real Ceiling Is 450 °C, for Two Reasons​‌​​‌​

HEAT TREATMENT — SCHEMATIC
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1 · ANNEALING — the usual delivery condition
Step1 · ANNEALING — the usual delivery condition​‌​​‌​
SummaryStandard anneal for parts that will not enter a glass-to-metal seal and for general use. It recrystallises the material and relieves internal stress. It gives no strength increase.​‌​​‌​
Temperature850-1000 °C (1560-1830 °F), preferably in hydrogen or cracked ammonia — Special Metals NILO K. Alternative for sheet and strip: 999 °C for 30 minutes — EFINEA / Ed Fagan.​‌​​‌​
TimeAccording to section; 30 minutes for sheet and strip (EFINEA).​‌​​‌​
CoolingFurnace cool (EFINEA).​‌​​‌​
Resulting hardnessTypical annealed hardness 68 HRB (EFINEA, High Temp Metals, Ed Fagan, Aircraft Materials).​‌​​‌​

2 · DECARBURIZING ANNEAL — WET HYDROGEN (mandatory for glass sealing)
Step​‌​​‌​2 · DECARBURIZING ANNEAL — WET HYDROGEN (mandatory for glass sealing)
Summary​‌​​‌​This is the stage that determines the quality of the hermetic glass-to-metal seal. The wet hydrogen atmosphere removes carbon and dissolved gases. If glass sealing is attempted without this anneal, gas bubbles and leaks form in the seal.
Temperature​‌​​‌​900-1050 °C (1650-1920 °F) — Special Metals NILO K. · Two stages of 900 ± 20 °C and 1100 ± 20 °C — NiWire and High Temp Metals. · A band of 840-1100 °C (1540-2010 °F) — Carpenter Technology.
Time​‌​​‌​1 hour (Special Metals). · 1 hour at 900 °C plus 15 minutes at 1099-1100 °C (High Temp Metals, NiWire). · 20 minutes to 2 hours depending on temperature (Carpenter).
Cooling​‌​​‌​To room temperature within one hour (High Temp Metals). · At most 5 °C/min down to 200 °C (NiWire).
Resulting hardness​‌​​‌​—
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3 · CONTROLLED OXIDATION (before glass sealing)
Step3 · CONTROLLED OXIDATION (before glass sealing)​‌​​‌​
SummaryA thin, controlled oxide layer is formed on the surface so that the glass can wet the metal. This stage could not be verified numerically in four independent sources; no temperature or time is given and the existence of the stage is stated together with its source count.​‌​​‌​
TemperatureNo figure given — it appears qualitatively in two independent sources; no numerical band could be verified in four.​‌​​‌​
Time—​‌​​‌​
Cooling—​‌​​‌​
Resulting hardness—​‌​​‌​

4 · COLD WORKING — the only strengthening route
Step​‌​​‌​4 · COLD WORKING — the only strengthening route
Summary​‌​​‌​THERE IS NO PRECIPITATION HARDENING. Strength rises only with cold deformation. When intermediate annealing is needed, stage 1 is repeated; on parts that will enter a glass-to-metal seal the final operation is stage 2.
Temperature​‌​​‌​Room temperature
Time​‌​​‌​—
Cooling​‌​​‌​—
Resulting hardness​‌​​‌​In cold-drawn wire and strip the tensile strength rises above 850 N/mm2 (NiWire).
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5 · REGION TO AVOID — service above 450 °C
Step5 · REGION TO AVOID — service above 450 °C​‌​​‌​
SummaryNot a heat treatment stage but a usage limit. The inflection point is 450 °C; above it the expansion coefficient rises sharply and the match with the glass ends. The Curie temperature is 435 °C and the magnetic transition is the cause of this behaviour.​‌​​‌​
TemperatureInflection point 450 °C — Special Metals, EFINEA. Curie temperature 435 °C — Carpenter, High Temp Metals, EFINEA, Hempel.​‌​​‌​
Time—​‌​​‌​
Cooling—​‌​​‌​
Resulting hardnessThe mean expansion coefficient is 6.15 over 450-500 °C, 7.80 over 600-700 °C and 10.31 over 800-900 °C, in 10-6/°C (High Temp Metals).​‌​​‌​
The diagram is schematic; the time axis is NOT to scale. No published TTT/CCT curve was used, so no curve is drawn. Kovar is NOT PRECIPITATION HARDENABLE and cannot be hardened by heat treatment. The purpose of these cycles is not hardness but PREPARING A SOFT AND CLEAN STRUCTURE FOR THE GLASS-TO-METAL SEAL: removing carbon and oxygen, ordering the grain structure and relieving internal stress. The word ‘ageing’ is not used for this alloy. Schematic; the time axis is not to scale. NOT PRECIPITATION HARDENABLE — there is no solution treatment plus ageing cycle. Stage 3 (controlled oxidation) could not be verified numerically in four independent sources; no temperature or time is given. The decarburizing anneal is mandatory for a glass-to-metal seal; for general use stage 1 is sufficient.

Kovar’s service limit is not a code limit but the coincidence of two separate physical events. Both occur at roughly the same temperature, and that coincidence defines the whole application window of the alloy.​‌​​‌​

The Real Limits

Glass matching window​‌​​‌​Approximately −80 °C to +450 °C. Within this range Kovar’s expansion curve closely follows that of borosilicate glass and alumina ceramic. This is a design window, not a strength limit
Inflection point​‌​​‌​450 °C (840 °F) — where the expansion curve bends. Above it expansion climbs rapidly: the 20–450 °C mean is 5.3 while the 20–500 °C mean is 6.2 × 10⁻⁶/K
Curie temperature​‌​​‌​435 °C (815 °F) — three independent publishers. [Conflict] One publisher writes 425 °C. 435 °C and 450 °C are not the same thing: one is where magnetic order is lost, the other is where the expansion curve bends
The glass strain point​‌​​‌​The strain point of 7052 borosilicate glass is 435–440 °C. That is the temperature above which the glass can no longer sustain stress and begins to flow. Kovar’s Curie temperature and the glass strain point are practically the SAME temperature — which is why 450 °C is a real ceiling for a glass-to-metal transition for two separate reasons
What happens above 450 °C​‌​​‌​The metal starts to expand faster than the glass and the match breaks down. On cooldown the joint is left with a residual stress distribution different from the designed one. The result: cracked glass, interface separation, loss of hermeticity. If you are designing a package with high-temperature cycling, treat 450 °C as a red line
The sealing temperature is ABOVE that ceiling​‌​​‌​The softening point of 7052 glass is 710–712 °C and sealing is performed near there. This is not a contradiction: sealing is done while the glass is fluid and carries no stress; the service window must stay below the glass strain point
Oxidation · high temperature​‌​​‌​Kovar is not a high-temperature alloy. No chromium, no protective oxide. An oxide that thickens above 600 °C in air ruins the seal — this property is used deliberately only in the controlled oxidising step
The cryogenic side​‌​​‌​The lower end of the matching window is published as −80 °C. The alloy itself remains ductile far colder, but no glass-matching guarantee is published below −80 °C

Product Forms With NO Standard — the Commercially Valuable Section​‌​​‌​

After the withdrawal of F15 this list grew. These are the sentences a sales engineer should have memorised.

Specification Gaps for Kovar

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General position (post-2024)No in-force ASTM product specification remains for any form. The published route that remains is the trio AMS 7726 (wire) / 7727 (bar and forgings) / 7728 (sheet, strip, plate). When a customer asks for an AMS number, give the one that matches the form; listing all three is an error​‌​​‌​
PipeNever existed. Kovar pipe is not a process pipe; do not confuse it with the tube used in vacuum feedthroughs​‌​​‌​
Flanges · fittingsNo standard. A Kovar vacuum flange (for example in a CF/ConFlat-type feedthrough) is machined to drawing; Kovar is not in the ASME B16.5 material list​‌​​‌​
CastingsThere is no standardised cast Kovar grade, and that is just as well. Segregation and coarse grain in a casting shift the expansion curve locally; in a glass-to-metal seal that means a leak. Hermetic parts are made from wrought material​‌​​‌​
Welding consumablesNo AWS class. Matched Kovar wire is sold to proprietary specification. A weld bead expands differently in its own zone; if a weld will run near a glass feedthrough, account for that distance in the design​‌​​‌​
Plating specificationKovar has no plating specification of its own. Established field practice is 1.3–3.8 µm (50–150 microinches) nickel underplate + 1.3–2.5 µm (50–100 microinches) gold, but that is a manufacturer’s recommendation, not a standard. You must write the thickness and the acceptance criterion yourself​‌​​‌​
Decarburisation conditionThis is the most critical gap. No in-force product standard mandates whether the as-delivered condition is decarburised. If it is not written into the order, material unsuitable for glass sealing will arrive and the certificate will not show it​‌​​‌​
Expansion acceptance criterionF15 carried the expansion requirements; it is withdrawn. Write into the order text which expansion band you accept over which temperature range — otherwise the only property that matters in this alloy is never measured on the certificate​‌​​‌​

Chemical Composition — and How C, Mn, Si and S Limits Affect Glass Sealing

Chemistry in Kovar does two separate jobs: it fixes the expansion curve, and it keeps the glass interface clean. The major elements do the first, the impurity ceilings the second.​‌​​‌​

Chemical Composition · weight %

Nickel​‌​​‌​28.0–30.0 (two independent sources). Some publishers give a nominal 29.0
Cobalt​‌​​‌​17.0–18.0 (two independent sources). Nominal 17.0. This is the source of the DIN naming confusion: some publishers write FeNi29Co17, others FeNi29Co18 — the two ends of the same band
Iron​‌​​‌​Balance (nominal ~53 %). One publisher gives a band of 50.5–56
CRITICAL NOTE on Ni, Co and Fe​‌​​‌​The specification’s own wording: “The iron, nickel and cobalt percentages listed are nominal. They shall be adjusted by the MANUFACTURER so that the alloy meets the requirements for coefficient of thermal expansion.” In other words, the governing acceptance criterion in Kovar is not chemistry but EXPANSION. A heat that meets the chemistry table but fails the expansion band is not Kovar. That single sentence changes where you look when reading a certificate
Carbon​‌​​‌​[Conflict — the most important conflict on this page] Published ceilings: ≤0.04 (two sources reproducing the ASTM F15 route) · ≤0.05 (one European mill) · ≤0.03 (one supplier) · ≤0.02 (one US mill’s own typical ceiling) · one encyclopaedic source says <0.01. If you are sealing to glass, demand the lowest ceiling and write it into the order (see below)
Manganese​‌​​‌​≤0.50 · one mill nominal 0.30
Silicon​‌​​‌​≤0.20 (two sources) · one European mill ≤0.30
Phosphorus · Sulphur​‌​​‌​P ≤0.03 · S ≤0.03 (one European mill) · P ≤0.02 · S ≤0.02 (one supplier)
Chromium · Copper · Molybdenum​‌​​‌​Cr ≤0.20 · Cu ≤0.20 · Mo ≤0.20
Aluminium · Magnesium · Zirconium · Titanium​‌​​‌​Each ≤0.10 (one source) · another source states the four combined ≤0.20. These are deoxidiser residues and are unwanted at the glass interface

C, Mn, Si and S — why glass sealing hangs on these​‌​​‌​

Carbon: enemy number one. Carbon dissolved in Kovar reacts in the glass-sealing furnace with the surface oxide and with the glass to produce carbon monoxide and carbon dioxide. That gas becomes trapped in the molten glass and at the glass-metal interface as bubbles and blisters. The consequences are: the bonded area shrinks and the joint weakens mechanically; and when blisters coalesce they open a leak path. Leaks seen in hermeticity testing usually originate here. This is why Kovar is DECARBURISED in wet hydrogen before glass sealing — it is not merely cleaned, carbon is physically removed from the alloy. The decarburising anneal is not a cleaning step but a metallurgical operation, and it is MANDATORY for glass-to-metal sealing.

Silicon and aluminium: they corrupt the quality of the oxide film. What the seal bonds to is a deliberately grown NiO–CoO film on the metal surface; the glass wets that film and dissolves it. Silicon and aluminium form stable, stubborn oxides that do not dissolve in glass; those oxides leave locally non-wetting islands within the film and weaken the bond. That is why the Si and Al ceilings are held so low — not for strength.
Manganese: the ceiling is 0.50 %; more than that changes the composition and colour of the oxide film and makes the process harder to control.
Sulphur and phosphorus: they segregate to grain boundaries. Sulphur governs both hot cracking in welds and tearing in deep drawing and stamping; since hermetic package bodies are usually deep drawn, this is directly a yield issue.​‌​​‌​

The one sentence that reaches purchasing: on a Kovar order, write the carbon ceiling and the decarburisation condition separately. “Kovar to ASTM F15” — even if the standard were still in force — does not guarantee that material arrives ready for glass sealing.

Mechanical Properties​‌​​‌​

STRENGTH VALUES
Yield (MPa)Tensile (MPa)Annealed — strip and sheet517345Annealed — Special Metals NILO K520340Annealed — Aircraft Materials520340Annealed — upper bound (sheet and strip)565Annealed — upper bound (rod and wire)586Cold drawn (hard) — wire and strip850
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ConditionHardnessYield MPaTensile MPaElongation
Annealed — strip and sheet68 HRB​‌​​‌​345517​‌​​‌​30%
Annealed — Special Metals NILO K​‌​​‌​—340​‌​​‌​52042%​‌​​‌​
Annealed — Aircraft Materials—​‌​​‌​340520​‌​​‌​42%
Annealed — upper bound (sheet and strip)​‌​​‌​——​‌​​‌​565 max—​‌​​‌​
Annealed — upper bound (rod and wire)—​‌​​‌​—586 max​‌​​‌​—
Cold drawn (hard) — wire and strip​‌​​‌​——​‌​​‌​above 850—​‌​​‌​
Because ASTM F15 was withdrawn in 2024 there is NO ASTM specification minimum in force for this alloy; the specifications in force are AMS 7726/7727/7728, of which only the titles could be verified in this work — their mechanical tables were not read. Every row below is a PRODUCER TYPICAL VALUE and cannot be used as a specification minimum. Because Kovar is not precipitation hardenable, the rows are split by TEMPER, not by ageing condition. This alloy is bought for its expansion curve and not for its strength; the table is supplementary. There is NO ASTM SPECIFICATION MINIMUM in force; ASTM F15 was withdrawn in 2024. All rows are producer typical values. There are two clusters of elongation values: 30% (EFINEA/Ed Fagan/High Temp Metals) and 42% (Special Metals/Aircraft Materials). No average has been taken; the two clusters are given on separate rows. There is no precipitation hardening; the last row shows cold work. This alloy is bought for its expansion curve and not for its strength.

Kovar is a soft, ductile, deep-drawable alloy and is never bought for strength. Do not mix the two source groups below.​‌​​‌​

Annealed · Typical Values

Source A (US route)​‌​​‌​Rm 517 MPa (75 ksi) · Rp0.2 345 MPa (50 ksi) · Elongation 30 % (in 2 in) · 68 HRB · E 138 GPa (20 × 10³ ksi)
Source B (European manufacturer’s bulletin)​‌​​‌​20 °C: Rm 520 MPa · Rp0.2 340 MPa · A 42 % · Reduction of area 72 %
100 °C​‌​​‌​Rm 430 · Rp0.2 260 · A 42 % · 72 %
200 °C​‌​​‌​Rm 400 · Rp0.2 210 · A 42 % · 72 %
300 °C​‌​​‌​Rm 400 · Rp0.2 140 · A 45 % · 73 %
400 °C​‌​​‌​Rm 400 · Rp0.2 110 · A 49 % · 76 %
Source C (European mill sheet)​‌​​‌​Rm 450–585 MPa · Rp0.2 ≥200 MPa · A ≥25 % · 110–170 HV. Rm here is a BAND, not a single value
Elongation conflict​‌​​‌​[Conflict] Three sources give 30 %, 42 % and ≥25 %. Most of the difference comes from gauge length and product form. Do not impose an elongation requirement without stating the gauge length
Upper limits by product form​‌​​‌​One source gives Rm max 570 MPa (82 ksi) for sheet/strip and max 585 MPa (85 ksi) for rod/wire. In Kovar the upper limit matters too: material that is too hard tears in deep drawing and its expansion curve may shift after annealing
Hardness bands​‌​​‌​Annealed ≤160 HV (≤83 HRB) · full hard ≥230 HV (≥97 HRB). One US source gives 68 HRB annealed, another 120 HB. Always state the scale
Modulus conflict​‌​​‌​138–139 GPa (three sources) · 130 GPa (one manufacturer’s bulletin, as-rolled). Use 138 GPa for calculation

Physical Properties​‌​​‌​

Physical Properties · Kovar (K94610)

Density​‌​​‌​8.36 g/cm³ (0.302 lb/in³) — three independent sources. [Conflict] One manufacturer’s bulletin gives 8.16, one distributor 8.25. 8.36 is the majority and mill position; use it and footnote the difference
Melting point​‌​​‌​1450 °C (2640 °F) — three sources agree. One publisher gives a band of 1440–1460 °C
Thermal conductivity (20 °C)​‌​​‌​17 W/m·K (three sources in the 16.7–17.6 range; 0.17 W/cm·°C is the same number). Clearly above Invar 36’s ~10 W/m·K — a real difference for heat removal in a hermetic package, but still less than half that of carbon steel
Electrical resistivity​‌​​‌​49 µΩ·cm at 20 °C — two independent sources (294 ohm-cir-mil/ft is the same number). [Conflict] One manufacturer’s bulletin gives 43 µΩ·cm at 20 °C, rising to 114 µΩ·cm at 600 °C. 49 µΩ·cm is the majority value
Specific heat​‌​​‌​~0.46 kJ/kg·K (0.11 Btu/lb·°F) · one distributor gives 0.50 J/g·°C
Modulus of elasticity​‌​​‌​138 GPa (20 × 10³ ksi) · one bulletin 130 GPa
Curie temperature​‌​​‌​435 °C (815 °F) — three sources. [Conflict] one distributor writes 425 °C
Inflection point​‌​​‌​450 °C (840 °F)
Magnetic behaviour​‌​​‌​FERROMAGNETIC below the Curie temperature. This is a real constraint that is missed in electronic package design: a Kovar-bodied package distorts the local magnetic field and causes trouble for magnetically sensitive circuits (Hall sensors, magnetometers, some MEMS gyroscopes, RF ferrite components). No numerical relative permeability value could be found — do not publish a µr figure
The commercially meaningful point​‌​​‌​Kovar is magnetic, rust-prone, soft and expensive. All of that is accepted for one thing: an expansion curve that matches borosilicate glass and alumina ceramic between −80 and +450 °C. Outside that window Kovar has no advantage at all
MEAN COEFFICIENT OF THERMAL EXPANSION · 10⁻⁶/K · THE MOST IMPORTANT TABLE ON THIS PAGE

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25 → 100 °C5.85 · second manufacturer 5.86 · third manufacturer (20–100 °C) 6.0​‌​​‌​
25 → 200 °C5.20 · third manufacturer (20–200 °C) 5.5​‌​​‌​
25 → 300 °C5.13 · second manufacturer 5.13 · third manufacturer 5.1​‌​​‌​
25 → 350 °C4.90 · third manufacturer 4.9 — the MINIMUM of the curve is here​‌​​‌​
25 → 400 °C5.06 · third manufacturer 4.9​‌​​‌​
25 → 450 °C5.26 · second manufacturer 5.25 · third manufacturer 5.3 — the upper edge of the matching window​‌​​‌​
25 → 500 °C6.14 · third manufacturer 6.2 — past the inflection point​‌​​‌​
25 → 600 °C7.81​‌​​‌​
25 → 700 °C9.11​‌​​‌​
25 → 800 °C10.31​‌​​‌​
25 → 900 °C11.25 — now it behaves like ordinary steel​‌​​‌​
VerificationThis table is a unit conversion of a US manufacturer’s °F table and it matches a European mill’s °C table exactly at three points (5.86 / 5.13 / 5.25). A third manufacturer’s 20 °C-based table gives the same curve within ±0.3. Three independent publishers show the same curve​‌​​‌​
The SHAPE of the curve — the real pointNote that the value is 5.85 over 25–100 °C, then FALLS to 4.90 over 25–350 °C, then rises again. That dip is not an accident; it is engineered to match the glass curve. What separates Kovar from Invar is not a low number but this S shape​‌​​‌​
Compared with the glass7052 borosilicate glass: 4.6–4.7 × 10⁻⁶/K over 0–300 °C, and 5.3 × 10⁻⁶/K from 25 °C to the setting point. Kovar over the same ranges is 5.13 and 5.26. The difference is a few percent and it is deliberate — because the metal contracts slightly more, the glass is left in compression. Glass is strong in compression and weak in tension; a good glass-to-metal seal keeps the glass in slight compression​‌​​‌​

Heat Treatment — the Wet Hydrogen Decarburising Anneal and Controlled Oxidation

Heat treatment in Kovar is done for the GLASS INTERFACE, not for strength. This is the section anyone making glass-to-metal seals must read.​‌​​‌​

Four Distinct Operations — Their ORDER and PURPOSE Must Not Be Confused

1 · Standard anneal (softening)​‌​​‌​850–1000 °C (1560–1830 °F), preferably in hydrogen or cracked ammonia (one manufacturer’s bulletin). A European mill specifies 850 °C for 30 minutes in a protective atmosphere (wet or dry hydrogen, dissociated ammonia or a similar neutral atmosphere) and requires furnace cooling to about 175 °C to prevent oxidation and thermal shock. This step restores ductility; it does not prepare the part for glass sealing
2 · WET HYDROGEN DECARBURISING ANNEAL — MANDATORY for glass sealing​‌​​‌​900–1050 °C (1650–1920 °F) for 1 hour in a wet hydrogen atmosphere (one manufacturer’s bulletin). A US mill describes the same operation as: “all degreased, fabricated Kovar alloy parts should be degassed and annealed in a wet hydrogen atmosphere”; temperature 838–1099 °C (1540–2010 °F), time about 2 hours at the low end and 20 minutes at the high end, then cool below 300 °C (570 °F)
Why WET hydrogen?​‌​​‌​Dry hydrogen degasses but does NOT remove carbon. The water vapour in wet hydrogen oxidises the dissolved carbon to CO and CO₂, which escape. At the end of the operation the alloy is both decarburised and has a controlled surface condition. Skip this step and the carbon produces CO/CO₂ in the sealing furnace, leaves bubbles and blisters at the interface, and HERMETICITY IS LOST
The ORDER of operations is critical​‌​​‌​Fabricate first, then degrease, then decarburise. Machining and drawing oils leave carbon on the surface; a decarburising anneal performed BEFORE those operations is wasted. One mill’s own wording makes this explicit: the treatment is applied to “degreased, fabricated” parts
3 · Controlled oxidation (immediately before glass sealing)​‌​​‌​600–1000 °C (1110–1830 °F) in air, depending on the film thickness required (one manufacturer’s bulletin). A US mill gives a narrower window: 650–700 °C (1200–1290 °F) until a dark grey to slightly brown oxide forms. That film is NiO–CoO based and it is what the glass wets and dissolves
Oxide COLOUR is a quality indicator​‌​​‌​Grey, grey-blue or grey-brown = a good seal. A metallic colour = insufficient oxide (the glass does not wet, the bond is weak). Black = over-oxidised (the film is thick and brittle, the bond is again weak). Both extremes mean a weak joint. This is a shop-floor visual check that no distributor page publishes
4 · Stress relief​‌​​‌​No separate stress relief temperature or time for Kovar could be independently verified. In practice the annealing and decarburising treatments also relieve stress. Do not invent a number
Cooling rule​‌​​‌​One European mill requires furnace cooling to ~175 °C after annealing; a US mill requires cooling below 300 °C after decarburisation. The purpose is the same: prevent a hot part from meeting air and oxidising uncontrollably, and prevent thermal shock

Welding, Soldering and Plating​‌​​‌​

Joining Methods

Suitable welding processes​‌​​‌​TIG (GTAW), electron beam, laser and resistance (seam) welding — all four are published and established in the field. Hermetic package lids are typically closed by parallel seam resistance welding or laser
Filler metal​‌​​‌​No AWS classification. Matched Kovar wire is sold to proprietary specification. Using a foreign filler creates a band in the weld that expands differently
Welding near a glass feedthrough — the most common mistake​‌​​‌​Weld heat damages the glass-to-metal joint. The weld must be far enough from the feedthrough and the heat sink path must be considered; otherwise the glass cracks or the interface separates. A part decarburised before welding can locally pick up carbon again in the HEAT AFFECTED ZONE — if glass sealing follows welding, review the operation sequence
Soldering and brazing​‌​​‌​Kovar is routinely soldered and brazed, but not directly: with no chromium the surface oxidises rapidly and solder will not wet it. That is why it is nickel plated first
NICKEL PLATING — why it is mandatory​‌​​‌​Three separate reasons. (1) Corrosion: Kovar has no chromium and rusts in humid air; the nickel underplate is the barrier. (2) Solderability: a nickel surface is wetted by solder and braze alloys, bare Kovar is not. (3) Conductivity and interconnect: Kovar’s electrical conductivity is poor (49 µΩ·cm); the gold top layer provides wire bonding and a low-resistance contact. Established practice: 1.3–3.8 µm (50–150 microinches) nickel + 1.3–2.5 µm (50–100 microinches) gold
A caution on gold plating​‌​​‌​Gold thickness must be controlled: excess gold forms brittle gold-tin intermetallics in a solder joint. There is no published plating specification for Kovar; you must write the thickness and acceptance criterion yourself
The sequence of sealing and plating​‌​​‌​Glass sealing FIRST, plating AFTERWARDS. Glass is not sealed to a plated surface — what the glass bonds to is the nickel-cobalt oxide film, not the nickel plate. A production flow that reverses this order will not pass a hermeticity test
Hydrogen embrittlement​‌​​‌​Hydrogen from an electrolytic nickel plating bath can cause trouble in stressed thin sections. No published bake-out schedule for Kovar could be found — do not invent a temperature and time; use your plater’s own qualified schedule

Machining​‌​​‌​

Kovar is not as difficult as Invar 36, but it is not easy either. It comes from the same family and behaves the same way: it work-hardens like austenitic stainless, produces stringy, gummy chips and wraps them around the tool. The one thing in its favour is a thermal conductivity about 1.7 times that of Invar (17 W/m·K versus 10 W/m·K), so heat leaves the tool tip a little better. Do not raise speeds on the strength of that.

Machining · Kovar (parameters published for the NILO family)

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General ruleMachine in the annealed condition, with high speed steel or tungsten carbide tipped tools (manufacturer’s bulletin). Machining in the hard temper increases work hardening and distortion​‌​​‌​
Rough turning30–45 m/min (98–148 ft/min) · feed 0.25–0.40 mm/rev (typical values published by the manufacturer for the NILO family)​‌​​‌​
Tool geometryLarge, sharp, rigidly supported tools; positive top rake. Interrupted cuts, dwelling and successive thin cuts create a glazed, work-hardened surface — restarting a cut in it is very difficult​‌​​‌​
CoolantSulphurised/chlorinated cutting oils break chips well. BUT a Kovar-specific warning: cutting oil and cutting fluid leave carbon on the surface. On parts destined for glass sealing this demands complete degreasing before the decarburising anneal​‌​​‌​
MANDATORY post-fabrication stepEvery finished Kovar part must be degreased and decarburised in wet hydrogen before glass sealing. Machining adds both cold work and surface carbon; both are removed in that anneal. This is not an optional step​‌​​‌​
Deep drawing and stampingHermetic package bodies are typically produced by deep drawing. Kovar takes it well but intermediate anneals are required; material forced in the hard temper tears. The sulphur ceiling is directly a yield question here​‌​​‌​
Magnetic workholdingKovar is ferromagnetic, so a magnetic chuck works. But demagnetise afterwards: residual magnetism makes fine chips cling to the part and contaminates the plating and sealing steps​‌​​‌​

Corrosion — Kovar Is NOT Stainless

Kovar is not a corrosion alloy. It rusts. The fact that it is used in hermetic packages does not change that — those packages are plated.​‌​​‌​

Why it rusts

In Kovar chromium exists only as an impurity ceiling (≤0.20 %), which is nowhere near enough to form a passive oxide film. The bulk of the alloy is iron (~53 %). Nickel and cobalt add some resistance but do not passivate. For corrosion purposes, think of Kovar as a low-alloy steel. That is not what the alloy was designed for anyway: its chemistry is chosen entirely for the expansion curve and the glass interface.​‌​​‌​

Where it is GOOD

It is good when plated and enclosed. The field reality is that almost all Kovar components are used nickel + gold plated, and corrosion resistance comes from the plating, not from the alloy. In vacuum and inside a dry hermetic cavity there is no corrosion problem — keeping the inside dry and inert is the whole point of a hermetic package. Bare Kovar stored in a dry, climate-controlled environment is fine for reasonable periods.​‌​​‌​

WHERE IT FAILS — the list that must be published

1. Bare Kovar plus humid air. Unplated Kovar rusts in a humid environment. Condensation in storage, moisture in transit, sweating in the shop all produce surface rust — and you cannot seal glass to a rusted surface.
2. Seawater, chlorides and salt spray. No resistance whatsoever. Electronic packages in marine environments are protected by plating and enclosure, not by the alloy.
3. Acids. With no chromium and no molybdenum it is unprotected in both reducing and oxidising acids. Kovar is not a process equipment material.
4. Plating pinholes. This is the most insidious failure mode. Micro-pores in the nickel plate create galvanically accelerated local corrosion beneath the gold: gold is the cathode and Kovar the anode, and that couple accelerates corrosion at the bottom of the pore. This is why nickel underplate thickness and freedom from porosity are critical — gold alone is not enough.
5. Fingerprints. Kovar parts destined for glass sealing must not be handled with bare hands. Hand perspiration contains chloride and organic acids; it both pits the surface and prevents the oxide film from forming evenly.
6. Furnace atmosphere upsets. If atmosphere control is lost in the decarburising or oxidising furnace, the surface ends up with an oxide of the wrong thickness or wrong composition; a black (over-oxidised) surface gives a weak bond to glass. That is not corrosion, but it leads to the same outcome — a leak.
7. Long open storage. For unplated Kovar strip and bar, VCI packaging, dry storage and a protective film are mandatory.​‌​​‌​

Be honest about numerical corrosion data: no published corrosion rate table, PREN value or critical pitting temperature for Kovar could be found — and none of those would be meaningful for this alloy anyway. Do not publish a corrosion rate figure.

Frequently Asked Questions​‌​​‌​

Can we skip the decarburising anneal and go straight to glass sealing? Furnace time is expensive.

No. This is the most expensive shortcut in glass-to-metal sealing, and its failures often show up not in the hermeticity test but in the field.
Here is why. Carbon dissolved in Kovar reacts in the sealing furnace with the surface oxide and with the glass to produce carbon monoxide and carbon dioxide. That gas becomes trapped inside the molten glass and precisely at the glass-metal interface: bubbles and blisters form. They have two consequences — the bonded area shrinks and the joint weakens mechanically; and when blisters coalesce they open a leak path along the interface. A part that barely passes a helium leak test drifts outside the limit after a few thermal cycles.
The correct sequence is: finish fabrication → complete degreasing (cutting and drawing oils leave carbon on the surface) → wet hydrogen decarburising anneal (900–1050 °C for 1 hour; another mill says 838–1099 °C, about 2 hours at the low end and 20 minutes at the high end, then cool below 300 °C) → controlled oxidation (650–700 °C until a dark grey to slightly brown film forms) → glass sealing → plating.
The difference between wet and dry hydrogen lies exactly here: dry hydrogen degasses but does not remove carbon. What removes carbon is the water vapour in wet hydrogen oxidising it to CO and CO₂.
Commercial advice: if you want to save furnace time, this is not the step to save it on. Write “delivered decarburised in wet hydrogen” into the order and buy the material in that condition — but remember it must be repeated after fabrication.​‌​​‌​

Our package goes through a furnace that reaches 500 °C. Will Kovar be a problem?

Yes. 450 °C is a genuine red line in this alloy, and for two reasons — both of which occur at about the same temperature.
The first is in the metal: the inflection point of Kovar’s expansion curve is 450 °C and the Curie temperature is 435 °C. Above these points expansion climbs rapidly: the 25–450 °C mean is 5.26, but at 25–500 °C it is 6.14, at 25–600 °C 7.81 and at 25–700 °C 9.11 × 10⁻⁶/K. In a cycle reaching 500 °C the metal expands more than the glass expects.
The second is in the glass: the strain point of 7052 borosilicate glass is 435–440 °C. Above that the glass is no longer elastic and relieves stress permanently. When the part cools, the joint is left with a residual stress distribution different from the one that was designed. The design holds the glass in slight compression; when that balance is disturbed, the glass can be driven into tension — and glass is weak in tension.
Practical outcome: a 500 °C process cycle may not break a hermetic Kovar–borosilicate transition in one pass, but it raises the probability of a leak with cycle count. What to do: bring the process temperature below 450 °C; or replace the transition with a ceramic-to-metal solution (alumina with an active metal braze); or change the assembly sequence so the glass feedthrough stays out of the furnace cycle. What not to do is reason that “Kovar melts at 1450 °C” and treat 500 °C as safe. The melting point is completely irrelevant here.​‌​​‌​

Our datasheet says Corning 7052. Our supplier says they cannot get 7052. Now what?

Your supplier is right. Corning 7052 has been discontinued since 1991. The published succession is: 7052 → Corning 7056 → Corning 7720 → today Schott 8250. When you ask for “Kovar sealing glass” today, what you actually get is Schott 8250 or an equivalent.
This does not make old specifications worthless — but you must rewrite the specification against the glass PROPERTY, not the glass brand. The numbers to hold on to, for 7052: 46–47 × 10⁻⁷/°C over 0–300 °C (i.e. 4.6–4.7 × 10⁻⁶/K), 53 × 10⁻⁷/°C from 25 °C to the setting point, strain point 435–440 °C, annealing point 480–484 °C, softening point 710–712 °C, density 2.27 g/cm³. Ask how close the new glass is to those values.
Why it matters: Kovar over the same ranges gives 5.13 and 5.26 × 10⁻⁶/K. The metal contracts a few percent more than the glass, and that difference keeps the glass in compression — which is the design principle of a good glass-to-metal seal. If the new glass expands appreciably differently, that balance is disturbed and the transition must be requalified.
What to do: write the specification as “borosilicate sealing glass matched to Kovar (K94610), expansion 4.6–4.7 × 10⁻⁶/K over 0–300 °C, strain point ≥435 °C” and give the brand name as an example. Any document that makes a brand name the specification eventually goes out of supply.​‌​​‌​

Invar 36 expands less and costs less. Can we use it instead of Kovar?

No — and “expands less” is precisely the wrong part of that sentence.
What a hermetic glass-to-metal transition needs is not low expansion but MATCHED expansion. Invar 36 gives 1.5 × 10⁻⁶/K over 20–100 °C; borosilicate glass over the same region gives 4.6–4.7. The difference is more than threefold. In a glass-to-metal seal that means a mismatch accumulating through cooldown that puts the glass into tension — and glass is weak in tension and cracks.
The second and less known difference is the SHAPE of the curve. Kovar’s coefficient is 5.85 over 25–100 °C, falls to 4.90 over 25–350 °C, then rises again to 5.26 over 25–450 °C. That dip is not an accident; it is engineered to follow the glass’s own curve. Invar’s curve, by contrast, climbs continuously above 220 °C (5.5 over 20–300 °C, 10.1 over 20–500 °C). The two curves are nowhere parallel.
The third difference is cobalt. The seal bonds through a nickel-cobalt oxide film grown on the metal surface, and cobalt makes that oxide easier to melt and to dissolve in the glass. Invar has no cobalt; its oxide is largely iron oxide and does not behave the same way in glass.
In short: buy Invar 36 for dimensional stability — optical benches, metrology frames, composite tooling, LNG membranes. Buy Kovar for a hermetic glass-to-metal transition. The price difference is trivial next to the cost of a single leaking package.​‌​​‌​

Common Datasheet Errors — Check Before You Order

1. Missing the withdrawal of ASTM F15. F15 was withdrawn in 2024 with no replacement — and F1684 and F30 went with it. Most pages that still say “conforms to ASTM F15” do not know this. Cite the edition year, and know that AMS 7726/7727/7728 are still in force.
2. Not separating the AMS numbers by form. 7726 = WIRE, 7727 = BAR and FORGINGS, 7728 = SHEET, STRIP and PLATE. Listing all three as “the Kovar specification” leads to a wire specification being written onto a plate order.
3. Skipping the decarburising anneal, or mistaking it for a cleaning step. Wet hydrogen decarburisation is a MANDATORY metallurgical operation for glass-to-metal sealing, not degreasing. Skip it and carbon produces CO/CO₂, leaves blisters at the interface and hermeticity is lost. Most distributor pages never mention it at all.
4. Confusing dry hydrogen with wet hydrogen. Dry hydrogen degasses; it does NOT remove carbon. What decarburises is the water vapour in wet hydrogen.
5. Writing the operation sequence backwards. The correct order is fabricate → degrease → decarburise → controlled oxidation → glass seal → plate. Glass is not sealed to a plated surface; what the glass bonds to is the nickel-cobalt oxide film, not the nickel plate.
6. Confusing the Curie temperature with the inflection point. Curie 435 °C, inflection 450 °C. One distributor writes 425 °C for Curie. The design ceiling is 450 °C, and that temperature also sits just above the strain point of 7052 glass (435–440 °C) — two separate reasons, one line.
7. Publishing a single expansion number. In Kovar expansion is a curve that falls, then rises: 25–100 °C 5.85 · 25–350 °C 4.90 (minimum) · 25–450 °C 5.26 · 25–500 °C 6.14 · 25–900 °C 11.25. The entire value of the alloy is in the SHAPE of that curve; a single number destroys it.
8. Assuming Corning 7052 is still made. 7052 has been discontinued since 1991. The succession is 7056 → 7720 → Schott 8250. Tie the specification to expansion and strain point values, not to a brand name.
9. Density conflict. 8.36 g/cm³ is the majority and mill value. One manufacturer’s bulletin gives 8.16, one distributor 8.25. If you price by weight, state which density you used.
10. Resistivity conflict. 49 µΩ·cm is confirmed by two independent sources (294 ohm-cir-mil/ft is the same number). One manufacturer’s bulletin gives 43 µΩ·cm. State which you used in RF and power calculations.
11. DIN name confusion. FeNi29Co17 and FeNi29Co18 are the same alloy; the difference is which end of the cobalt band (17.0–18.0 %) went into the name. The material number is 1.3981 in both cases.
12. Material number confusion. 1.3981 = Kovar, 1.3912 = Invar 36, 1.3917 = alloy 42. All three are called “low-expansion Fe-Ni” and all three do entirely different jobs.
13. Confusion with “Invar 42”. Alloy 42 (K94100) is sometimes sold as “Invar 42”. It is neither Invar 36 nor Kovar: Fe–42 Ni, inflection 370 °C, matched to silicon and alumina. Read the UNS number on the certificate, not the trade name.
14. Treating the chemistry table as the only acceptance criterion. The specification’s own note reads: the iron, nickel and cobalt percentages are NOMINAL and are adjusted by the manufacturer so that the alloy meets the expansion requirements. So the governing acceptance criterion is EXPANSION. With F15 withdrawn, you must write the expansion acceptance band into the order yourself; otherwise the only property that matters is never measured.
15. Omitting the carbon ceiling, or hiding the conflict in it. Published ceilings range over ≤0.02 · ≤0.03 · ≤0.04 · ≤0.05. If you are sealing to glass this difference matters; demand the lowest ceiling and write it into the order.
16. Assuming Kovar is “stainless”. Chromium is only a ≤0.20 % impurity ceiling; no passive film forms and bare Kovar rusts in a humid environment. Field corrosion resistance comes from nickel + gold plating, not from the alloy.
17. Treating nickel plating as cosmetic. The nickel underplate does three jobs at once: corrosion barrier, solderability, and a pore-free base for the gold top layer. Gold alone is not enough: micro-pores in the nickel accelerate local corrosion under the gold–Kovar galvanic couple.
18. Omitting the magnetic behaviour. Kovar is ferromagnetic below 435 °C and is a constraint for magnetically sensitive circuits. Do not publish a relative permeability (µr) figure — no verifiable value could be found.
19. Mistaking the melting point for a safety margin. 1450 °C is correct and completely irrelevant. Kovar’s service ceiling is 450 °C, set by the glass match, not by melting.
20. Specifying elongation without a gauge length. Published elongation values range over 25 %, 30 % and 42 %; most of the spread comes from gauge length and product form. Do not impose an elongation requirement without stating the gauge length.​‌​​‌​

COMPARISON
MEAN LINEAR COEFFICIENT OF THERMAL EXPANSION (10-6/°C) over the same temperature ranges referenced to 20 °C. The values for the two alloys come from the SAME measurement basis in the SAME source (the Special Metals NILO alloys bulletin), and each row has additionally been cross-checked against independent sources. These two alloys are distinguished by their expansion behaviour rather than by their mechanical strength, so the comparison is built on that criterion.
​‌​​‌​

GradeUNSW.-Nr.Cte 20 100Cte 20 200Cte 20 250Cte 20 300Cte 20 400Cte 20 500Donum noktasiCurieDavranisNe icin secilirCapraz kontrol
KovarK94610​‌​​‌​1.39816.0​‌​​‌​5.55.3​‌​​‌​5.14.9​‌​​‌​6.2450 °C (Special Metals, EFINEA)​‌​​‌​435 °CThe coefficient FALLS from room temperature to the inflection point and stays flat across the 20-450 °C band, then rises sharply. The value is higher than Invar’s, but THE CURVE IS FLAT.​‌​​‌​Hermetic glass-to-metal seals. What is wanted is not a low coefficient but a curve that MATCHES the borosilicate glass curve all the way to 450 °C.EFINEA / Carpenter 5.86 for 25-100 °C; 5.06 for 25-400 °C; 5.25 for 25-450 °C · NiWire 6.4 for 20-100 °C; 5.3 for 20-450 °C · Wikipedia 5.5 for 25-200 °C; 5.3 for 25-450 °C · ASTM F15 acceptance band 4.60-5.20 for 30-400 °C and 5.10-5.50 for 30-450 °C​‌​​‌​
Invar 36K93600 (also K93601, K93603)​‌​​‌​1.39121.5​‌​​‌​2.63.5​‌​​‌​5.58.4​‌​​‌​10.1220 °C (Special Metals); ESPI gives 190 °C​‌​​‌​277-279 °CThe coefficient is at its lowest around room temperature and RISES RAPIDLY with temperature. Above the Curie temperature the Invar effect disappears entirely.​‌​​‌​Work below 200 °C in which the dimension must not change with temperature. It is NOT SUITABLE for glass-to-metal seals; its curve matches no technical glass.Carpenter 1.30 at 93 °C · Rolled Alloys 1.44 for 21-100 °C · Nickel Institute 1.26 for -18/93 °C · NeoNickel 1.2-1.5 for -100/+100 °C​‌​​‌​

Additional information
Kritik fark​‌​​‌​Kovar’s coefficient is about four times that of Invar 36 over the 20-100 °C band. Even so it is Kovar that is used in glass-to-metal seals, because the criterion is not the SMALLNESS of the coefficient but the SHAPE OF THE CURVE. The seal is formed as the glass cools from its setting temperature to room temperature; if glass and metal contract at different rates through that cooling, the joint cracks. Because Kovar’s curve follows the borosilicate glass curve up to 450 °C, the seal stays free of stress throughout that cooling. Invar 36’s curve, by contrast, diverges rapidly above 220 °C and matches no technical glass. The two alloys are not interchangeable. NEITHER alloy is precipitation hardenable.
Glass note​‌​​‌​The glass family Kovar is matched to is BOROSILICATE; the matching glass most often named is Corning 7052. Special Metals states that the expansion characteristics of NILO alloy K ‘match those of borosilicate glasses and alumina type ceramics’; NiWire writes that the match holds between -80 and 450 °C; EFINEA states that 450 °C is ‘the working range for sealing to borosilicate glasses’ and names Corning 7052 as the matching glass. The borosilicate glass family has a coefficient of about 5 ppm/K over 30-200 °C. THE NAME CORNING 7052 APPEARS EXPLICITLY IN ONLY ONE INDEPENDENT SOURCE, so it is written on the card as the ‘typical matching glass’, while the glass family (borosilicate) rests on four sources.
Siparis notu​‌​​‌​An expansion coefficient is NEVER ordered without stating its temperature range. The statement ‘Kovar, 5 ppm/K’ is incomplete; it must be written as ‘mean linear coefficient of expansion over 30-450 °C, 5.10-5.50 µm/m·°C’. Because ASTM F15 (Kovar) and ASTM F1684 (Invar) were both withdrawn in 2024, the acceptance range must be written into the purchase order.
Same criterion, same reference temperature (20 °C), same measurement basis: Tables 7 and 10 of the Special Metals NILO bulletin. The coefficients are given TOGETHER WITH THEIR TEMPERATURE RANGES; a coefficient given without a range cannot be used. The values in the cross-check rows use different reference temperatures (20, 25, 30 °C), so they are not expected to agree exactly and have not been averaged. The name Corning 7052 appears explicitly in one independent source; the glass FAMILY (borosilicate) is verified by four. NEITHER alloy is precipitation hardenable.

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