Super Invar 32-5 Super Invar

Fe-32Ni-5.5Co (Super Invar 32-5): iron balance, nickel 32.00 %, cobalt 5.50 %, manganese 0.40 %, silicon 0.25 %, carbon 0.02 % (Carpenter nominal type analysis)

Also known as UNS K93500, ASTM F1684, Super Invar 32-5

Super Invar 32-5 is an iron-nickel-cobalt alloy with a nominal 32.00 % nickel and 5.50 % cobalt, balance iron, that Carpenter Technology designs to give minimum thermal expansion at room temperatures.

9 sources · Updated 2026-11-01 · CC BY 4.0

Evidence level

2 of 5

Lab-measured

Expansion

0.63 ppm/°C

Strength

276 MPa

Ductility

40 %

Density

8150 kg/m3

Resistivity

481.3 ohm-cir-mil/ft

Recipe, share of the weight

  • Fe balanceIron
  • Ni wt%, nominal 32.00Nickel
  • Co wt%, nominal 5.50Cobalt

Best for

Parts that must hold a length near room temperature, where Carpenter says its thermal expansion is less than that of Invar 36 over -67 to 203 °F (-55 to 95 °C)

Weakest at

Long-term expansion stability (the reason the 1972 JPL study gave for not using it), and oxidation during heat treatment above about 1000 °F (538 °C)

Risk at a glance

  • People Low. Cobalt and nickel are sensitisers; control dust
  • If it fails Moderate. Dimensional drift after fabrication
  • Corrosion Moderate. Super Invar 32-5 oxidises readily above about 1000 °F (538 °C), so heat treatment needs a protective atmosphere.

Quick facts: Super Invar

Key properties of Super Invar
PropertyValueBasis
Density8.14 to 8.15 g/cm³2 sourced values across conditions
Yield strength276 MPa2 sourced values across conditions
Tensile strength483 MPa2 sourced values across conditions
Thermal expansion (CTE)0.63 ppm/K1 sourced value
Electrical resistivity8.0e-7 Ω·m2 sourced values across conditions

What is the density of Super Invar 32-5?

Super Invar 32-5 has a density of 8.14 to 8.15 g/cm³. The range covers 2 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.

What is the coefficient of thermal expansion of Super Invar 32-5?

Super Invar 32-5 has a coefficient of thermal expansion of 0.63 ppm/K. The source and test conditions are listed in the properties table on this page.

What is the yield strength of Super Invar 32-5?

Super Invar 32-5 has a yield strength of 276 MPa. The range covers 2 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.

What is the tensile strength of Super Invar 32-5?

Super Invar 32-5 has a tensile strength of 483 MPa. The range covers 2 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.

What are the other names and codes for Super Invar 32-5?

Super Invar 32-5 is also written as UNS K93500, ASTM F1684, Super Invar 32-5. Each code is printed in the source listed beside it in the designations table.

What is Super Invar 32-5 used for?

Uses recorded in the sources include Optical and laser systems; Semiconductor components; Wave guide tubes and other low-expansion glass or quartz assemblies.

Why it exists

Super Invar 32-5 is used where a metal must keep its length near room temperature. Hi-Temp Metals prints a mean coefficient of thermal expansion of 0.63 ppm/°C from -55 to 95 °C and a density of 8150 kg/m3. The cost is strength: the typical yield strength is 276 MPa and the typical tensile strength is 483 MPa, both in the annealed condition.

Where it's used

Optical and laser systems

Carpenter lists optical and laser systems among the applications of Super Invar 32-5 on its datasheet.

Semiconductor components and wave guide tubes

Carpenter lists semiconductor components, wave guide tubes and other systems with low expansion glass or quartz assemblies.

Recipe

Fe-32Ni-5.5Co (Super Invar 32-5): iron balance, nickel 32.00 %, cobalt 5.50 %, manganese 0.40 %, silicon 0.25 %, carbon 0.02 % (Carpenter nominal type analysis); UNS K93500

Super Invar 32-5 is a magnetic, austenitic solid solution of iron, nickel and cobalt. Carpenter's nominal type analysis is 32.00 % nickel, 5.50 % cobalt, 0.40 % manganese, 0.25 % silicon and 0.02 % carbon, with iron as the balance. It is supplied as bar, billet, strip and wire.

What Super Invar is made of
IngredientShare of the weightWhat it does
Iron Fe balance Balance of the alloy. Carpenter describes the alloy as magnetic and austenitic.
Nickel Ni wt%, nominal 32.00 Carpenter says the alloy is designed to give minimum thermal expansion at room temperatures, and nickel is the main element in the type analysis.
Cobalt Co wt%, nominal 5.50 Named in the type analysis. The datasheet does not state its role.

Weight shares are as printed in the sources.

What it can do

Expansion

0.63 ppm/°C

measured

0.63 ppm/°C from -55 to 95 °C, as a mean coefficient (Hi-Temp Metals).

Strength

276 MPa

measured

276 MPa yield and 483 MPa tensile in the annealed condition (Carpenter typical values).

Ductility

40 %

measured

40 % elongation in 2 in (50.8 mm) in the annealed condition (Carpenter typical value).

Density

8150 kg/m3

measured

8150 kg/m3 (Hi-Temp Metals).

Resistivity

481.3 ohm-cir-mil/ft

measured

481.3 ohm-cir-mil/ft at 73 °F (23 °C) (Carpenter).

How it compares

Carpenter says the thermal expansion of Super Invar 32-5 is less than that of Invar 36 over -67/203 °F (-55/95 °C). The datasheet prints no Invar 36 value, so that comparison is qualitative here. Against other low-expansion metals, the figures to weigh are the 0.63 ppm/°C mean coefficient and the 276 MPa annealed yield strength for this grade.

The same measurements for each material, so you can compare them. Each row names the key condition under the value; the full conditions and methods are in the numbered notes under Technical details. Other materials are shown beside it; each was measured under its own conditions, so open its page before comparing closely. Compare every grade in the family.

Benchmarks
MeasurementSuper InvarIN718 (UNS N07718)IN625 (UNS N06625)FeNi36Ni-MoC-22C-276 (UNS N10276)X (UNS N06002)UNS N07214H230 (UNS N06230)UNS N08800Alloy 825 (UNS N08825)Alloy 600 (UNS N06600, W.Nr. 2.4816)Alloy 601Alloy 617X-750 (UNS N07750)Fe-Ni-CoAlloy 400 (UNS N04400)K-500NiNi3Al, NiAlNiBe2Ni-alloysUNS N07090 (W. Nr. 2.4632)UNS N07001
Physical and electrical
DensityValue printed in a supplier technical data table8150 kg/m30.297 lb/in38.44 g/cm³8.05 g/cm³9.22 g/cm³8.69 g/cm³8.89 g/cm³8.22 g/cm³8.05 g/cm³8.97 g/cm³7.94 g/cm³8.14 g/cm³0.306 lb/in38.11 Mg/m38.36 g/cm³8.28 g/cm³8.36 g/cm³8.8 g/cm³8.45 g/cm³8.89 g/cm³7.5 g/cm³8.27 g/cm³8.2 g/cm³8.18 g/cm³8.19 g/cm³
Density0.294 lb/in310.297 lb/in38.44 g/cm³8.05 g/cm³9.22 g/cm³8.69 g/cm³8.89 g/cm³8.22 g/cm³8.05 g/cm³8.97 g/cm³7.94 g/cm³8.14 g/cm³0.306 lb/in38.11 Mg/m38.36 g/cm³8.28 g/cm³8.36 g/cm³8.8 g/cm³8.45 g/cm³8.89 g/cm³7.5 g/cm³8.27 g/cm³8.2 g/cm³8.18 g/cm³8.19 g/cm³
electrical resistivity481.3 ohm-cir-mil/ft5725 ohm circ mil/ft129 µΩ-cm84 µΩ·cm1.37 μohm.m1.14 µΩ·m1.23 μohm.m114.8 µohm-cm135.9 µohm-cm125 µohm-m0.989 µΩ·m112 µΩ·cm1.03 µΩ·m1.18 µΩ·m1.22×10^-4 Ω·cm731 ohm circ mil/ft49 μΩcm0.511 µΩ·m0.615 µΩ·m0.096 µΩ·mno data< 28.7 µΩ·cm45 µΩ·cm1.18 µΩ·m1.24 µΩ·m
electrical resistivityValue printed in a supplier technical data table80 µΩ·cm725 ohm circ mil/ft129 µΩ-cm84 µΩ·cm1.37 μohm.m1.14 µΩ·m1.23 μohm.m114.8 µohm-cm135.9 µohm-cm125 µohm-m0.989 µΩ·m112 µΩ·cm1.03 µΩ·m1.18 µΩ·m1.22×10^-4 Ω·cm731 ohm circ mil/ft49 μΩcm0.511 µΩ·m0.615 µΩ·m0.096 µΩ·mno data< 28.7 µΩ·cm45 µΩ·cm1.18 µΩ·m1.24 µΩ·m
Hardness, Rockwell B (custom name, not in property-canon)75 HRB13no datano datano datano datano data88 HRBW87 HRBWno datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano data
Hardness, Rockwell B (custom name, not in property-canon)90 HRB14no datano datano datano datano data88 HRBW87 HRBWno datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano data
Other measurements
Specific gravity (custom name, not in property-canon)8.15 -2no datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano data
Thermal expansion (CTE)Value printed in a supplier technical data table0.63 ppm/°C38.91 ppm/°F12.8 ppm/°C1.3 ppm/K10.6 μm/m.°C12.4 ppm/K11.2 μm/m.°C13.9 µm/(m·K)14.6 µm/m-°C11.8 ppm/K14.4 µm/m/°C13.9 ppm/K10.4 ppm/K13.75 µm/m/°C11.6 µm/(m·K)7 10-6 in./in./°F5.86 10-6/°C14.2 µm/m°C13.7 10-6/°C13.3 ppm/Kno data14.5 ppm/K8 ppm/K12.7 µm/(m·K)14.3 µm/m·°C
poissons ratio0.23 -40.294 -0.278 -no datano datano data0.31 -0.32 -no data0.31 -0.339 -no data0.324 -0.272 -no data0.29 -no data0.32 -no datano datano data0.3 -no datano datano data
Martensite start temperature (custom name, not in property-canon)-80 °C6no datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano data
yield strength276 MPa7171 ksi60 to 95 ksi40 ksi421 MPa> 310 MPa356 MPa340 MPa577 MPa417 MPa250 MPa338 MPa170 to 345 MPa292 MPa340 MPa> 105 ksi> 200 N/mm225 to 50 ksi276 to 414 MPa105 to 210 MPano data280 to 480 MPa280 MPa752 MPa586 MPa
yield strength276 MPa8171 ksi60 to 95 ksi40 ksi421 MPa> 310 MPa356 MPa340 MPa577 MPa417 MPa250 MPa338 MPa170 to 345 MPa292 MPa340 MPa> 105 ksi> 200 N/mm225 to 50 ksi276 to 414 MPa105 to 210 MPano data280 to 480 MPa280 MPa752 MPa586 MPa
ultimate tensile strength483 MPa9201 ksi120 to 150 ksi65 ksi862 MPa690 to 950 MPa792 MPa760 MPa975 MPa837 MPa590 MPa662 MPa550 to 690 MPa675 MPa710 MPa> 165 ksi450 to 585 N/mm275 to 90 ksi621 to 758 MPa380 to 520 MPa2300 MPa660 to 900 MPa500 MPa1175 MPa1027 MPa
ultimate tensile strength483 MPa10201 ksi120 to 150 ksi65 ksi862 MPa690 to 950 MPa792 MPa760 MPa975 MPa837 MPa590 MPa662 MPa550 to 690 MPa675 MPa710 MPa> 165 ksi450 to 585 N/mm275 to 90 ksi621 to 758 MPa380 to 520 MPa2300 MPa660 to 900 MPa500 MPa1175 MPa1027 MPa
elongation40 %1126 %30 to 60 %35 %53 %> 45 %61 %48.9 %37.3 %47.3 %17 %45 %35 to 55 %46 %62 %> 20 %> 25 %35 to 60 %20 to 35 %40 to 55 %no data> 30 %35 %30 %43 %
elongation40 %1226 %30 to 60 %35 %53 %> 45 %61 %48.9 %37.3 %47.3 %17 %45 %35 to 55 %46 %62 %> 20 %> 25 %35 to 60 %20 to 35 %40 to 55 %no data> 30 %35 %30 %43 %

Why choose it, and why not

Good for

  • Parts that must hold a length near room temperature: mean coefficient 0.63 ppm/°C from -55 to 95 °C.
  • Optical and laser systems, semiconductor components and wave guide tubes, per Carpenter's applications list.
  • Assemblies that must match low expansion glass or quartz, per Carpenter.

Watch out for

  • Long-term expansion drift: the 1972 JPL/Itek study rejected Super-Invar for this reason.
  • Cold work changes the expansion, so heat-treat parts at or as close to finish size as possible.
  • No corrosion rate or humidity test was read; the datasheet lists plating and zinc coating as the usual finishes.

Super Invar 32-5 suits parts that must hold a length near room temperature, where Carpenter says its expansion is lower than Invar 36's. Design with its 0.63 ppm/°C mean coefficient and 276 MPa annealed yield strength, but note that the 1972 JPL study rejected it for long-term expansion stability, and that no corrosion rate was found.

Technical details

For scientists and researchers. Everything above comes from the record below: every number with its method, its conditions and its source.

Other names and standards

The same grade under other systems, as datasheets and standards print them. Each code was checked against the page it comes from.

Other names and standards
SystemCodes
UNSK93500
ASTMF1684 (applicable designation for this alloy)
Trade nameSuper Invar 32-5

Notes

The method, full conditions and any caveat for the numbered rows above.

Notes for the numbered rows
#MeasurementMethodConditionsCaveat
1DensityValue printed in the manufacturer's physical properties tableform not statedunit in source 0.2940 lb/in3, English Units column—
2Specific gravity (custom name, not in property-canon)Value printed in the manufacturer's physical properties tableprinted in English and metric columns, both printed as 8.15—
3Thermal expansion (CTE)—temperature range -55 to 95 °Cbasis mean coefficient of thermal expansionunit in source 0.63 under the column heading 10(-6)/°C—
4poissons ratioValue printed in the manufacturer's physical properties tablebasis printed with no unit—
5electrical resistivityValue printed in the manufacturer's physical properties tabletemperature 73 °F (23 °C)—
6Martensite start temperature (custom name, not in property-canon)Value printed in the manufacturer's physical properties tableprinted as -112 °F and -80 °C—
7yield strengthTypical value printed in the manufacturer's mechanical properties tableheat treatment annealedbasis typical mechanical properties table, 0.2% yield—
8yield strengthTypical value printed in the manufacturer's mechanical properties tableheat treatment cold workedbasis typical mechanical properties table, 0.2% yield—
9ultimate tensile strengthTypical value printed in the manufacturer's mechanical properties tableheat treatment annealedbasis typical mechanical properties table—
10ultimate tensile strengthTypical value printed in the manufacturer's mechanical properties tableheat treatment cold workedbasis typical mechanical properties table—
11elongationTypical value printed in the manufacturer's mechanical properties tableheat treatment annealedgauge 2 in (50.8 mm)basis typical mechanical properties table—
12elongationTypical value printed in the manufacturer's mechanical properties tableheat treatment cold workedgauge 2 in (50.8 mm)basis typical mechanical properties table—
13Hardness, Rockwell B (custom name, not in property-canon)Typical value printed in the manufacturer's mechanical properties tableheat treatment annealedbasis typical mechanical properties table—
14Hardness, Rockwell B (custom name, not in property-canon)Typical value printed in the manufacturer's mechanical properties tableheat treatment cold workedbasis typical mechanical properties table—

Corrosion and compatibility

What happens when it meets other materials and environments.

Corrosion and compatibility
EnvironmentConcernWhat happens
Heat treatment at or above about 1000 °F (538 °C) moderate Super Invar 32-5 oxidises readily above about 1000 °F (538 °C), so heat treatment needs a protective atmosphere.1
Forging furnace with a long soak moderate A long soak in the forging furnace can leave a checked surface.2
Humid air and corrosion protection (no test of Super Invar 32-5 read) not rated No humidity or salt-spray test of Super Invar 32-5 was read; the datasheet names plating and zinc coating as the usual finishes.3
Corrosion details
#EnvironmentDetailsTest conditions
1 Heat treatment at or above about 1000 °F (538 °C) Carpenter says the alloy oxidises readily at heat-treating temperatures above about 1000 °F (538 °C) and recommends vacuum, hydrogen, dissociated ammonia or inert gases. process heat treatment at or above about 1000 °F (538 °C)
2 Forging furnace with a long soak Carpenter says long soaking may give a checked surface from oxygen and sulfur contamination, and suggests forging at 2000/2150 °F (1093/1177 °C). process forging
3 Humid air and corrosion protection (no test of Super Invar 32-5 read) Carpenter says the alloy can be chromium, cadmium and nickel plated or zinc coated by the usual methods used for ferrous alloys. No corrosion rate or humidity rating is printed for the bare alloy. basis datasheet statement on finishes; no corrosion test data

Risks and side effects

Hazards to people, what happens when a cell overheats, and how the material is handled and stored.

For people

The alloy is mostly iron, but its cobalt and nickel are the health hazards, and machining produces dust and chips that carry them.

Skin
PubChem's aggregated reports give H317 (may cause an allergic skin reaction) for more than 99.9 % of cobalt reports and for 99.9 % of nickel reports.
Breathing
Cobalt is H334 (may cause allergy or asthma symptoms if inhaled) for more than 99.9 % of reports.

In service

Its low expansion depends on stress relief after fabrication, and the alloy oxidises during heat treatment.

Dimensional drift
Fabricating stresses change the expansion behaviour, so Carpenter says to heat-treat at or as close to finish size as possible.
Oxidation
Above about 1000 °F (538 °C) the alloy oxidises readily, so heat treatment needs a protective atmosphere.

In space

The space record here is a 1972 design study. No flight or test data for Super Invar 32-5 were read.

What the report says
The 1972 JPL/Itek study did not use Super-Invar, because the expansion properties of the material were unstable over long periods of time.
What is missing
No thermal-vacuum, outgassing or radiation test of Super Invar 32-5 was read.

Test details
The original wording and numbers from the sources, for readers who want them.

Failure risks

Failure risks
FailureTrigger and consequence
Dimensional drift after fabricationmoderate severityMachining, forming or deep drawing introduces stressesCarpenter says fabricating stresses promote variation in thermal expansion behaviour, so parts should be heat treated at or as close to finish size as possible.
Transformation at low temperaturemoderate severityService below -67 °F (-55 °C)Carpenter gives austenite stability to service temperatures of at least -67 °F (-55 °C) and prints martensite start at -112 °F (-80 °C); the datasheet gives no expansion values below -67 °F (-55 °C).
Checked surface from furnace soakingmoderate severityLong soak in a forging furnaceCarpenter says a long soaking time may give a checked surface from oxygen and sulfur contamination.
Grain boundary embrittlement after machiningmoderate severityResidual sulfur left on machined partsCarpenter says residual sulfur can cause grain boundary embrittlement, so parts should be degreased and cleaned as soon after machining as possible.

Side effects on surrounding parts

Side effects on surrounding parts
AffectsEffect
Machining operationsMachined chips are gummy and stringy, so the alloy is somewhat difficult to machine.

Handling and storage

  • Heat-treat before final machining: heat to 1550 °F (843 °C) for 1 hour, water quench, stress-relieve at 600 °F (316 °C) for 1 hour, air cool, then age at 200 °F (93 °C) for 24 hours and air cool.
  • Above about 1000 °F (538 °C), heat-treat in a protective environment such as vacuum, hydrogen, dissociated ammonia or inert gas.
  • Forge at 2000/2150 °F (1093/1177 °C), heat rapidly and avoid soaking in the forging furnace.
  • Degrease and clean machined parts as soon as possible after machining to remove residual sulfur.

Mitigations

  • Heat-treat parts at or as close to finish size as possible, using the schedule under handling.

Supply and geography

How common the raw materials are and where they come from.

Nickel (32.00 % of the alloy)

Top producers (2025)
Indonesia 66.7%, Philippines 6.9%, Russia 5.1%, Canada 3.6%, New Caledonia 3.6%, China 3.1%
Critical mineral lists
US: listed
Recycling
USGS: in 2025 nickel recovered from scrap accounted for approximately 60% of apparent consumption.
Substitutes
USGS: low-nickel, duplex or ultrahigh-chromium stainless steels have been substituted for austenitic grades in construction; titanium alloys can substitute for nickel-base alloys in corrosive environments.

Cobalt (5.50 % of the alloy)

Top producers (2025)
Congo (Kinshasa) 73%, Indonesia 14%
Recycling
USGS: in 2025, cobalt content of purchased scrap represented 25% of estimated cobalt consumption.
Substitutes
USGS: depending on the application, substitution for cobalt could result in a loss in product performance or increased cost.

Iron (balance of the alloy)

Top producers (2025)
Australia 37.7%, Brazil 16.2%, India 11.9%, China 11.2%
Recycling
USGS: none for iron ore; see the separate Iron and Steel Scrap chapter.

Updated