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.
Evidence level
2 of 5
Lab-measured
- 0Predicted only. No one has made it, or no measurement exists.
- 1Calculated. Only calculated or predicted values from sources.
- 2Lab-measured. Measured properties with their conditions stated.
- 3Space-relevant tests. Measured in conditions relevant to space, such as vacuum or atomic oxygen.
- 4Ground-qualified. Qualified for an application on the ground.
- 5Flown or field-proven. Flight or field results exist.
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
| Property | Value | Basis |
|---|---|---|
| Density | 8.14 to 8.15 g/cm³ | 2 sourced values across conditions |
| Yield strength | 276 MPa | 2 sourced values across conditions |
| Tensile strength | 483 MPa | 2 sourced values across conditions |
| Thermal expansion (CTE) | 0.63 ppm/K | 1 sourced value |
| Electrical resistivity | 8.0e-7 Ω·m | 2 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.
| Ingredient | Share of the weight | What 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.
| Measurement | Super Invar | IN718 (UNS N07718) | IN625 (UNS N06625) | FeNi36 | Ni-Mo | C-22 | C-276 (UNS N10276) | X (UNS N06002) | UNS N07214 | H230 (UNS N06230) | UNS N08800 | Alloy 825 (UNS N08825) | Alloy 600 (UNS N06600, W.Nr. 2.4816) | Alloy 601 | Alloy 617 | X-750 (UNS N07750) | Fe-Ni-Co | Alloy 400 (UNS N04400) | K-500 | Ni | Ni3Al, NiAl | NiBe2 | Ni-alloys | UNS N07090 (W. Nr. 2.4632) | UNS N07001 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Physical and electrical | |||||||||||||||||||||||||
| DensityValue printed in a supplier technical data table | 8150 kg/m3 | 0.297 lb/in3 | 8.44 g/cm³ | 8.05 g/cm³ | 9.22 g/cm³ | 8.69 g/cm³ | 8.89 g/cm³ | 8.22 g/cm³ | 8.05 g/cm³ | 8.97 g/cm³ | 7.94 g/cm³ | 8.14 g/cm³ | 0.306 lb/in3 | 8.11 Mg/m3 | 8.36 g/cm³ | 8.28 g/cm³ | 8.36 g/cm³ | 8.8 g/cm³ | 8.45 g/cm³ | 8.89 g/cm³ | 7.5 g/cm³ | 8.27 g/cm³ | 8.2 g/cm³ | 8.18 g/cm³ | 8.19 g/cm³ |
| Density | 0.294 lb/in31 | 0.297 lb/in3 | 8.44 g/cm³ | 8.05 g/cm³ | 9.22 g/cm³ | 8.69 g/cm³ | 8.89 g/cm³ | 8.22 g/cm³ | 8.05 g/cm³ | 8.97 g/cm³ | 7.94 g/cm³ | 8.14 g/cm³ | 0.306 lb/in3 | 8.11 Mg/m3 | 8.36 g/cm³ | 8.28 g/cm³ | 8.36 g/cm³ | 8.8 g/cm³ | 8.45 g/cm³ | 8.89 g/cm³ | 7.5 g/cm³ | 8.27 g/cm³ | 8.2 g/cm³ | 8.18 g/cm³ | 8.19 g/cm³ |
| electrical resistivity | 481.3 ohm-cir-mil/ft5 | 725 ohm circ mil/ft | 129 µΩ-cm | 84 µΩ·cm | 1.37 μohm.m | 1.14 µΩ·m | 1.23 μohm.m | 114.8 µohm-cm | 135.9 µohm-cm | 125 µohm-m | 0.989 µΩ·m | 112 µΩ·cm | 1.03 µΩ·m | 1.18 µΩ·m | 1.22×10^-4 Ω·cm | 731 ohm circ mil/ft | 49 μΩcm | 0.511 µΩ·m | 0.615 µΩ·m | 0.096 µΩ·m | no data | < 28.7 µΩ·cm | 45 µΩ·cm | 1.18 µΩ·m | 1.24 µΩ·m |
| electrical resistivityValue printed in a supplier technical data table | 80 µΩ·cm | 725 ohm circ mil/ft | 129 µΩ-cm | 84 µΩ·cm | 1.37 μohm.m | 1.14 µΩ·m | 1.23 μohm.m | 114.8 µohm-cm | 135.9 µohm-cm | 125 µohm-m | 0.989 µΩ·m | 112 µΩ·cm | 1.03 µΩ·m | 1.18 µΩ·m | 1.22×10^-4 Ω·cm | 731 ohm circ mil/ft | 49 μΩcm | 0.511 µΩ·m | 0.615 µΩ·m | 0.096 µΩ·m | no data | < 28.7 µΩ·cm | 45 µΩ·cm | 1.18 µΩ·m | 1.24 µΩ·m |
| Hardness, Rockwell B (custom name, not in property-canon) | 75 HRB13 | no data | no data | no data | no data | no data | 88 HRBW | 87 HRBW | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data |
| Hardness, Rockwell B (custom name, not in property-canon) | 90 HRB14 | no data | no data | no data | no data | no data | 88 HRBW | 87 HRBW | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data |
| Other measurements | |||||||||||||||||||||||||
| Specific gravity (custom name, not in property-canon) | 8.15 -2 | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data |
| Thermal expansion (CTE)Value printed in a supplier technical data table | 0.63 ppm/°C3 | 8.91 ppm/°F | 12.8 ppm/°C | 1.3 ppm/K | 10.6 μm/m.°C | 12.4 ppm/K | 11.2 μm/m.°C | 13.9 µm/(m·K) | 14.6 µm/m-°C | 11.8 ppm/K | 14.4 µm/m/°C | 13.9 ppm/K | 10.4 ppm/K | 13.75 µm/m/°C | 11.6 µm/(m·K) | 7 10-6 in./in./°F | 5.86 10-6/°C | 14.2 µm/m°C | 13.7 10-6/°C | 13.3 ppm/K | no data | 14.5 ppm/K | 8 ppm/K | 12.7 µm/(m·K) | 14.3 µm/m·°C |
| poissons ratio | 0.23 -4 | 0.294 - | 0.278 - | no data | no data | no data | 0.31 - | 0.32 - | no data | 0.31 - | 0.339 - | no data | 0.324 - | 0.272 - | no data | 0.29 - | no data | 0.32 - | no data | no data | no data | 0.3 - | no data | no data | no data |
| Martensite start temperature (custom name, not in property-canon) | -80 °C6 | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data |
| yield strength | 276 MPa7 | 171 ksi | 60 to 95 ksi | 40 ksi | 421 MPa | > 310 MPa | 356 MPa | 340 MPa | 577 MPa | 417 MPa | 250 MPa | 338 MPa | 170 to 345 MPa | 292 MPa | 340 MPa | > 105 ksi | > 200 N/mm2 | 25 to 50 ksi | 276 to 414 MPa | 105 to 210 MPa | no data | 280 to 480 MPa | 280 MPa | 752 MPa | 586 MPa |
| yield strength | 276 MPa8 | 171 ksi | 60 to 95 ksi | 40 ksi | 421 MPa | > 310 MPa | 356 MPa | 340 MPa | 577 MPa | 417 MPa | 250 MPa | 338 MPa | 170 to 345 MPa | 292 MPa | 340 MPa | > 105 ksi | > 200 N/mm2 | 25 to 50 ksi | 276 to 414 MPa | 105 to 210 MPa | no data | 280 to 480 MPa | 280 MPa | 752 MPa | 586 MPa |
| ultimate tensile strength | 483 MPa9 | 201 ksi | 120 to 150 ksi | 65 ksi | 862 MPa | 690 to 950 MPa | 792 MPa | 760 MPa | 975 MPa | 837 MPa | 590 MPa | 662 MPa | 550 to 690 MPa | 675 MPa | 710 MPa | > 165 ksi | 450 to 585 N/mm2 | 75 to 90 ksi | 621 to 758 MPa | 380 to 520 MPa | 2300 MPa | 660 to 900 MPa | 500 MPa | 1175 MPa | 1027 MPa |
| ultimate tensile strength | 483 MPa10 | 201 ksi | 120 to 150 ksi | 65 ksi | 862 MPa | 690 to 950 MPa | 792 MPa | 760 MPa | 975 MPa | 837 MPa | 590 MPa | 662 MPa | 550 to 690 MPa | 675 MPa | 710 MPa | > 165 ksi | 450 to 585 N/mm2 | 75 to 90 ksi | 621 to 758 MPa | 380 to 520 MPa | 2300 MPa | 660 to 900 MPa | 500 MPa | 1175 MPa | 1027 MPa |
| elongation | 40 %11 | 26 % | 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 % |
| elongation | 40 %12 | 26 % | 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.
| System | Codes |
|---|---|
| UNS | K93500 |
| ASTM | F1684 (applicable designation for this alloy) |
| Trade name | Super Invar 32-5 |
Notes
The method, full conditions and any caveat for the numbered rows above.
| # | Measurement | Method | Conditions | Caveat |
|---|---|---|---|---|
| 1 | Density | Value printed in the manufacturer's physical properties table | form not statedunit in source 0.2940 lb/in3, English Units column | — |
| 2 | Specific gravity (custom name, not in property-canon) | Value printed in the manufacturer's physical properties table | printed in English and metric columns, both printed as 8.15 | — |
| 3 | Thermal expansion (CTE) | — | temperature range -55 to 95 °Cbasis mean coefficient of thermal expansionunit in source 0.63 under the column heading 10(-6)/°C | — |
| 4 | poissons ratio | Value printed in the manufacturer's physical properties table | basis printed with no unit | — |
| 5 | electrical resistivity | Value printed in the manufacturer's physical properties table | temperature 73 °F (23 °C) | — |
| 6 | Martensite start temperature (custom name, not in property-canon) | Value printed in the manufacturer's physical properties table | printed as -112 °F and -80 °C | — |
| 7 | yield strength | Typical value printed in the manufacturer's mechanical properties table | heat treatment annealedbasis typical mechanical properties table, 0.2% yield | — |
| 8 | yield strength | Typical value printed in the manufacturer's mechanical properties table | heat treatment cold workedbasis typical mechanical properties table, 0.2% yield | — |
| 9 | ultimate tensile strength | Typical value printed in the manufacturer's mechanical properties table | heat treatment annealedbasis typical mechanical properties table | — |
| 10 | ultimate tensile strength | Typical value printed in the manufacturer's mechanical properties table | heat treatment cold workedbasis typical mechanical properties table | — |
| 11 | elongation | Typical value printed in the manufacturer's mechanical properties table | heat treatment annealedgauge 2 in (50.8 mm)basis typical mechanical properties table | — |
| 12 | elongation | Typical value printed in the manufacturer's mechanical properties table | heat treatment cold workedgauge 2 in (50.8 mm)basis typical mechanical properties table | — |
| 13 | Hardness, Rockwell B (custom name, not in property-canon) | Typical value printed in the manufacturer's mechanical properties table | heat treatment annealedbasis typical mechanical properties table | — |
| 14 | Hardness, Rockwell B (custom name, not in property-canon) | Typical value printed in the manufacturer's mechanical properties table | heat treatment cold workedbasis typical mechanical properties table | — |
Corrosion and compatibility
What happens when it meets other materials and environments.
| Environment | Concern | What 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 |
| # | Environment | Details | Test 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 | Trigger and consequence |
|---|---|
| Dimensional drift after fabricationmoderate severity | Machining, 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 severity | Service 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 severity | Long 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 severity | Residual 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
| Affects | Effect |
|---|---|
| Machining operations | Machined 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.
Documents
Datasheets, safety data sheets, papers and standards you can open.
| Document | Type | Year |
|---|---|---|
| Carpenter Technology Super Invar 32-5 data sheet (ASTM F1684, UNS K93500) | datasheet | |
| Hi-Temp Metals: Super Invar 32-5 technical data | datasheet | |
| Outer Planets Mission Television Subsystem Optics Study, final report, 28 July 1972 (NASA NTRS 19720025731) | report | 1972 |
| USGS Mineral Commodity Summaries 2026: Nickel | report | 2026 |
| USGS Mineral Commodity Summaries 2026: Cobalt | report | 2026 |
| USGS Mineral Commodity Summaries 2026: Iron ore | report | 2026 |
| PubChem: Cobalt (CID 104730) | database | 2026 |
| PubChem: Nickel (CID 935) | database | 2026 |
| PubChem: Iron (CID 23925) | database | 2026 |
Full record
The complete spore, as stored. Free to reuse under CC-BY-4.0. Images keep the licence shown with each one.
Show the full YAML
spore: profile
id: super-invar-32-5
spore_version: 0.2
family: nickel-alloys
name: Super Invar 32-5
abbreviation: Super Invar
role: low-expansion structural alloy
category: metals
type: nickel-superalloys
summary: |
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. 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 typical yield strength is 276 MPa in the annealed condition. The 1972 JPL telescope study did not use it, because its expansion properties were unstable over long periods.
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)
identity:
formula: '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'
source: carpenter-super-invar
where: Type analysis table, page 1 (nominal values, weight %); UNS K93500 on the same page under Associated specifications
designations:
- system: UNS
code: K93500
source: carpenter-super-invar
where: Page 1, Associated specifications line
- system: ASTM
code: F1684
note: applicable designation for this alloy
source: carpenter-super-invar
where: Page 1, Applicable designation line
- system: Trade name
code: Super Invar 32-5
source: carpenter-super-invar
where: Page 1 title
tags:
environments: []
stresses:
- extreme-cold
applications:
- optics-and-cameras
- electronics-and-chips
properties:
- benchmark: density
value: 8150
unit: kg/m3
scope: material
conditions:
form: not stated
unit_in_source: 8150 kg/cu m
method: Value printed in a supplier technical data table
status: ground
source: hightempmetals-super-invar
where: Physical Properties table, row Density, metric line
- benchmark: density
value: 0.294
unit: lb/in3
scope: material
conditions:
form: not stated
unit_in_source: 0.2940 lb/in3, English Units column
method: Value printed in the manufacturer's physical properties table
status: ground
source: carpenter-super-invar
where: Physical properties table (page 2), row DENSITY, English Units column
- benchmark: specific_gravity
label: Specific gravity (custom name, not in property-canon)
value: 8.15
unit: '-'
scope: material
conditions:
printed_in: English and metric columns, both printed as 8.15
method: Value printed in the manufacturer's physical properties table
status: ground
source: carpenter-super-invar
where: Physical properties table (page 2), row SPECIFIC GRAVITY
- benchmark: cte
value: 0.63
unit: ppm/°C
scope: material
conditions:
temperature_range: '-55 to 95 °C'
basis: mean coefficient of thermal expansion
unit_in_source: 0.63 under the column heading 10(-6)/°C
method: Value printed in a supplier technical data table
status: ground
source: hightempmetals-super-invar
where: Physical Properties table, row Mean coefficient of thermal expansion, 10(-6)/°C line for -55 to 95°C
- benchmark: poissons_ratio
value: 0.23
unit: '-'
scope: material
conditions:
basis: printed with no unit
method: Value printed in the manufacturer's physical properties table
status: ground
source: carpenter-super-invar
where: Physical properties table (page 2), row POISSON'S RATIO, English Units column
- benchmark: electrical_resistivity
value: 481.3
unit: ohm-cir-mil/ft
scope: material
conditions:
temperature: 73 °F (23 °C)
method: Value printed in the manufacturer's physical properties table
status: ground
source: carpenter-super-invar
where: Physical properties table (page 2), row ELECTRICAL RESISTIVITY, 73°F (23°C) line
- benchmark: electrical_resistivity
value: 80
unit: µΩ·cm
scope: material
conditions:
temperature: room temperature (RT), as printed
method: Value printed in a supplier technical data table
status: ground
source: hightempmetals-super-invar
where: Physical Properties table, row Electrical resistivity (RT)
- benchmark: martensite_start
label: Martensite start temperature (custom name, not in property-canon)
value: -80
unit: °C
scope: material
conditions:
printed_as: '-112 °F and -80 °C'
method: Value printed in the manufacturer's physical properties table
status: ground
source: carpenter-super-invar
where: Physical properties table (page 2), row MARTENSITE START, metric column
- benchmark: yield_strength
value: 276
unit: MPa
scope: material
conditions:
heat_treatment: annealed
basis: typical mechanical properties table, 0.2% yield
method: Typical value printed in the manufacturer's mechanical properties table
status: ground
source: carpenter-super-invar
where: Typical mechanical properties table (page 3), row Annealed, 0.2% YIELD STRENGTH, MPa column
- benchmark: yield_strength
value: 276
unit: MPa
scope: material
conditions:
heat_treatment: cold worked
basis: typical mechanical properties table, 0.2% yield
method: Typical value printed in the manufacturer's mechanical properties table
status: ground
source: carpenter-super-invar
where: Typical mechanical properties table (page 3), row Cold worked, 0.2% YIELD STRENGTH, MPa column
- benchmark: ultimate_tensile_strength
value: 483
unit: MPa
scope: material
conditions:
heat_treatment: annealed
basis: typical mechanical properties table
method: Typical value printed in the manufacturer's mechanical properties table
status: ground
source: carpenter-super-invar
where: Typical mechanical properties table (page 3), row Annealed, ULTIMATE TENSILE STRENGTH, MPa column
- benchmark: ultimate_tensile_strength
value: 483
unit: MPa
scope: material
conditions:
heat_treatment: cold worked
basis: typical mechanical properties table
method: Typical value printed in the manufacturer's mechanical properties table
status: ground
source: carpenter-super-invar
where: Typical mechanical properties table (page 3), row Cold worked, ULTIMATE TENSILE STRENGTH, MPa column
- benchmark: elongation
value: 40
unit: '%'
scope: material
conditions:
heat_treatment: annealed
gauge: 2 in (50.8 mm)
basis: typical mechanical properties table
method: Typical value printed in the manufacturer's mechanical properties table
status: ground
source: carpenter-super-invar
where: Typical mechanical properties table (page 3), row Annealed, ELONGATION IN 2 IN (50.8 MM) column
- benchmark: elongation
value: 40
unit: '%'
scope: material
conditions:
heat_treatment: cold worked
gauge: 2 in (50.8 mm)
basis: typical mechanical properties table
method: Typical value printed in the manufacturer's mechanical properties table
status: ground
source: carpenter-super-invar
where: Typical mechanical properties table (page 3), row Cold worked, ELONGATION IN 2 IN (50.8 MM) column
- benchmark: hardness_rockwell_b
label: Hardness, Rockwell B (custom name, not in property-canon)
value: 75
unit: HRB
scope: material
conditions:
heat_treatment: annealed
basis: typical mechanical properties table
method: Typical value printed in the manufacturer's mechanical properties table
status: ground
source: carpenter-super-invar
where: Typical mechanical properties table (page 3), row Annealed, HARDNESS HRB column
- benchmark: hardness_rockwell_b
label: Hardness, Rockwell B (custom name, not in property-canon)
value: 90
unit: HRB
scope: material
conditions:
heat_treatment: cold worked
basis: typical mechanical properties table
method: Typical value printed in the manufacturer's mechanical properties table
status: ground
source: carpenter-super-invar
where: Typical mechanical properties table (page 3), row Cold worked, HARDNESS HRB column
corrosion:
- environment: Heat treatment at or above about 1000 °F (538 °C)
headline: Super Invar 32-5 oxidises readily above about 1000 °F (538 °C), so heat treatment needs a protective atmosphere.
effect: 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.
rating: moderate
conditions:
process: heat treatment at or above about 1000 °F (538 °C)
source: carpenter-super-invar
where: Heat treatment section (page 3), paragraph on protective environments
- environment: Forging furnace with a long soak
headline: A long soak in the forging furnace can leave a checked surface.
effect: Carpenter says long soaking may give a checked surface from oxygen and sulfur contamination, and suggests forging at 2000/2150 °F (1093/1177 °C).
rating: moderate
conditions:
process: forging
source: carpenter-super-invar
where: Workability, Forging paragraph (page 4)
- environment: Humid air and corrosion protection (no test of Super Invar 32-5 read)
headline: No humidity or salt-spray test of Super Invar 32-5 was read; the datasheet names plating and zinc coating as the usual finishes.
effect: 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.
rating: unknown
conditions:
basis: datasheet statement on finishes; no corrosion test data
source: carpenter-super-invar
where: Workability, Plating paragraph (page 4)
risks:
hazards:
- text: |
Cobalt is the main hazard in this alloy. PubChem's aggregation of ECHA C&L notifications for cobalt gives H317 (more than 99.9 %, may cause an allergic skin reaction), H334 (more than 99.9 %, may cause allergy or asthma symptoms if inhaled), H341 (65.8 %), H350 (64.5 %) and H360F (61.6 %). These are ratios for the element, not for Super Invar 32-5 itself.
ghs:
- H317
- H334
- H341
- H350
- H360F
source: pubchem-cobalt
where: Safety and Hazards, GHS Classification (CID 104730), aggregated ECHA C&L notifications
- text: |
Nickel (32.00 % of the alloy) is also a sensitiser. PubChem's aggregation of ECHA C&L notifications for nickel gives H317 for 99.9 % of reports, H372 (damage to organs through prolonged or repeated exposure) for 99.7 %, and H351 (suspected of causing cancer) for 72.9 %.
ghs:
- H317
- H372
- H351
source: pubchem-nickel
where: Safety and Hazards, GHS Classification (CID 935), aggregated ECHA C&L notifications
failure_risks:
- mode: Dimensional drift after fabrication
trigger: Machining, forming or deep drawing introduces stresses
consequence: Carpenter says fabricating stresses promote variation in thermal expansion behaviour, so parts should be heat treated at or as close to finish size as possible.
severity: moderate
source: carpenter-super-invar
where: Heat treatment section (page 3), first paragraph
- mode: Transformation at low temperature
trigger: Service below -67 °F (-55 °C)
consequence: 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).
severity: moderate
source: carpenter-super-invar
where: Description (page 1) and Physical properties table (page 2), row MARTENSITE START
- mode: Checked surface from furnace soaking
trigger: Long soak in a forging furnace
consequence: Carpenter says a long soaking time may give a checked surface from oxygen and sulfur contamination.
severity: moderate
source: carpenter-super-invar
where: Workability, Forging paragraph (page 4)
- mode: Grain boundary embrittlement after machining
trigger: Residual sulfur left on machined parts
consequence: Carpenter says residual sulfur can cause grain boundary embrittlement, so parts should be degreased and cleaned as soon after machining as possible.
severity: moderate
source: carpenter-super-invar
where: Machinability, additional notes (page 4)
side_effects:
- text: Machined chips are gummy and stringy, so the alloy is somewhat difficult to machine.
affects: Machining operations
source: carpenter-super-invar
where: Machinability paragraph (page 4)
handling:
- text: '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.'
source: carpenter-super-invar
where: Heat treatment, heat treating for lowest thermal expansion (page 3)
- text: Above about 1000 °F (538 °C), heat-treat in a protective environment such as vacuum, hydrogen, dissociated ammonia or inert gas.
source: carpenter-super-invar
where: Heat treatment section (page 3)
- text: Forge at 2000/2150 °F (1093/1177 °C), heat rapidly and avoid soaking in the forging furnace.
source: carpenter-super-invar
where: Workability, Forging paragraph (page 4)
- text: Degrease and clean machined parts as soon as possible after machining to remove residual sulfur.
source: carpenter-super-invar
where: Machinability, additional notes (page 4)
mitigations:
- text: Heat-treat parts at or as close to finish size as possible, using the schedule under handling.
source: carpenter-super-invar
where: Heat treatment section (page 3)
uses:
- application: optics-and-cameras
device: Optical and laser systems
example: Carpenter lists optical and laser systems as an application of Super Invar 32-5 on its datasheet.
source: carpenter-super-invar
where: Description (page 1), Applications list
- application: electronics-and-chips
device: Semiconductor components
example: Carpenter lists semiconductor components among the applications of Super Invar 32-5 on its datasheet.
source: carpenter-super-invar
where: Description (page 1), Applications list
- application: electronics-and-chips
device: Wave guide tubes and other low-expansion glass or quartz assemblies
example: Carpenter lists wave guide tubes and other systems with low expansion glass or quartz assemblies as applications.
source: carpenter-super-invar
where: Description (page 1), Applications list
supply:
- subject: Nickel (32.00 % of the alloy)
producers:
- country: Indonesia
share_percent: 66.7
year: 2025
- country: Philippines
share_percent: 6.9
year: 2025
- country: Russia
share_percent: 5.1
year: 2025
- country: Canada
share_percent: 3.6
year: 2025
- country: New Caledonia
share_percent: 3.6
year: 2025
- country: China
share_percent: 3.1
year: 2025
critical_lists:
- list: 'USGS MCS 2026 nickel chapter: the Executive Order 14285 text names critical minerals such as nickel'
listed: true
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.'
source: usgs-nickel-2026
where: World Mine Production and Reserves table, 2025e column (world total 3,900,000 t); shares computed by Space Mushroom from that table; Recycling and Substitutes paragraphs; critical-minerals wording in the Events section
- subject: Cobalt (5.50 % of the alloy)
producers:
- country: Congo (Kinshasa)
share_percent: 73
year: 2025
- country: Indonesia
share_percent: 14
year: 2025
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.'
source: usgs-cobalt-2026
where: Events, Trends, and Issues paragraph (shares printed as 73% and 14% of world total); Recycling line; Substitutes paragraph; World Mine Production table, 2025 column (world total 310,000 t)
- subject: Iron (balance of the alloy)
producers:
- country: Australia
share_percent: 37.7
year: 2025
- country: Brazil
share_percent: 16.2
year: 2025
- country: India
share_percent: 11.9
year: 2025
- country: China
share_percent: 11.2
year: 2025
recycling: 'USGS: none for iron ore; see the separate Iron and Steel Scrap chapter.'
source: usgs-iron-ore-2026
where: World Mine Production and Reserves table, 2025e usable-ore column (world total 2,600,000 thousand t); shares computed by Space Mushroom from that table; Recycling line
documents:
- title: Carpenter Technology Super Invar 32-5 data sheet (ASTM F1684, UNS K93500)
type: datasheet
url: https://www.carpentertechnology.com/hubfs/7407324/Material%20Saftey%20Data%20Sheets/Super%20Invar%2032-5.pdf
- title: 'Hi-Temp Metals: Super Invar 32-5 technical data'
type: datasheet
url: https://www.hightempmetals.com/techdata/hitempSuperInvardata.php
- title: Outer Planets Mission Television Subsystem Optics Study, final report, 28 July 1972 (NASA NTRS 19720025731)
type: report
url: https://ntrs.nasa.gov/api/citations/19720025731/downloads/19720025731.pdf
year: 1972
- title: 'USGS Mineral Commodity Summaries 2026: Nickel'
type: report
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-nickel.pdf
year: 2026
- title: 'USGS Mineral Commodity Summaries 2026: Cobalt'
type: report
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-cobalt.pdf
year: 2026
- title: 'USGS Mineral Commodity Summaries 2026: Iron ore'
type: report
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-iron-ore.pdf
year: 2026
- title: 'PubChem: Cobalt (CID 104730)'
type: database
url: https://pubchem.ncbi.nlm.nih.gov/compound/104730
year: 2026
- title: 'PubChem: Nickel (CID 935)'
type: database
url: https://pubchem.ncbi.nlm.nih.gov/compound/935
year: 2026
- title: 'PubChem: Iron (CID 23925)'
type: database
url: https://pubchem.ncbi.nlm.nih.gov/compound/23925
year: 2026
gaps:
- 'Not found in the datasheet and supplier pages read in this run: melting point, Curie temperature, thermal conductivity and specific heat. Nothing was entered for them.'
- Carpenter gives the mean CTE as 0.350 x 10-6 in/in/°F for -67 to 203 °F (-55 to 95 °C), with the exponent in the value cell. Under the exponent rule it was left out; the expansion value recorded is the Hi-Temp Metals figure of 0.63 ppm/°C from -55 to 95 °C.
- Elastic modulus was left out. Hi-Temp Metals prints 144 under the unit x 10(6) MPa beside 21 under x 10(6) psi, which do not agree on the printed exponent. Carpenter prints 21.0 x 103 ksi with the exponent in the value. No modulus was entered rather than choose a unit.
- No corrosion rate, humidity exposure or salt-spray result for Super Invar 32-5 was read. The corrosion entries rest on the heat-treatment oxidation statement, the forging soak statement and the plating statement.
- 'The two typical analyses disagree: Hi-Temp Metals prints nickel 31.75 and cobalt 5.36 (weight units not printed), against Carpenter''s nominal 32.00 and 5.50 %. The Carpenter nominal values are used in the record and both are noted here.'
- Carpenter's description gives the -67/203 °F (-55/95 °C) range as the one for which the alloy's thermal expansion is less than Invar 36's. Carpenter prints no Invar 36 value, so no Invar 36 number is recorded here.
- 'Custom benchmark names not in property-canon.yaml: specific_gravity, martensite_start and hardness_rockwell_b (Rockwell B values 75 and 90 HRB, annealed and cold worked).'
- The taxonomy has no controlled-expansion-alloy type, so this profile is filed under nickel-superalloys, as Invar 36 is. Super Invar is not a superalloy.
- 'Cobalt''s critical-mineral status was not read: the USGS 2025 critical minerals list was not fetched in this run. The nickel critical-mineral entry cites the wording in the USGS nickel chapter.'
- No vacuum outgassing, radiation, atomic-oxygen or thermal-vacuum data for Super Invar 32-5 were read. The only space source is the 1972 JPL/Itek study, a design report, which says Super-Invar was not used because its expansion properties were unstable over long periods of time.
- Atomic weights are given for iron, nickel and cobalt only. Manganese, silicon and carbon appear in the type analysis without atomic weights.
- No cryogenic expansion data below -55 °C were read.
- No cost or lead-time data were read.
sources:
carpenter-super-invar:
title: 'Carpenter Technology: Super Invar 32-5 data sheet'
id: Carpenter Technology data sheet, Super Invar 32-5 (ASTM F1684, UNS K93500)
url: https://www.carpentertechnology.com/hubfs/7407324/Material%20Saftey%20Data%20Sheets/Super%20Invar%2032-5.pdf
kind: datasheet
license: Manufacturer datasheet, cited not reproduced
hightempmetals-super-invar:
title: 'Hi-Temp Metals: Super Invar 32-5 technical data'
id: Hi-Temp Metals technical data page, Super Invar 32-5
url: https://www.hightempmetals.com/techdata/hitempSuperInvardata.php
kind: web
license: Supplier page, cited not reproduced
usgs-nickel-2026:
title: 'Mineral Commodity Summaries 2026: Nickel'
id: USGS MCS 2026, nickel
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-nickel.pdf
year: 2026
kind: report
license: USGS public domain
usgs-cobalt-2026:
title: 'Mineral Commodity Summaries 2026: Cobalt'
id: USGS MCS 2026, cobalt
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-cobalt.pdf
year: 2026
kind: report
license: USGS public domain
usgs-iron-ore-2026:
title: 'Mineral Commodity Summaries 2026: Iron ore'
id: USGS MCS 2026, iron ore
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-iron-ore.pdf
year: 2026
kind: report
license: USGS public domain
ntrs-19720025731:
title: Outer Planets Mission Television Subsystem Optics Study, final report, 28 July 1972
id: NASA NTRS 19720025731 (Itek 72-9320-1, for JPL)
url: https://ntrs.nasa.gov/api/citations/19720025731/downloads/19720025731.pdf
year: 1972
kind: report
license: NASA NTRS public document
pubchem-cobalt:
title: 'PubChem: Cobalt (CID 104730), Safety and Hazards'
id: PubChem CID 104730
url: https://pubchem.ncbi.nlm.nih.gov/compound/104730
year: 2026
kind: database
license: PubChem, U.S. National Library of Medicine
pubchem-nickel:
title: 'PubChem: Nickel (CID 935), Safety and Hazards'
id: PubChem CID 935
url: https://pubchem.ncbi.nlm.nih.gov/compound/935
year: 2026
kind: database
license: PubChem, U.S. National Library of Medicine
pubchem-iron:
title: 'PubChem: Iron (CID 23925), molecular weight'
id: PubChem CID 23925
url: https://pubchem.ncbi.nlm.nih.gov/compound/23925
year: 2026
kind: database
license: PubChem, U.S. National Library of Medicine
license: CC-BY-4.0
updated: '2026-11-01'
review:
status: draft
method: assistant
checked_values: 16
unreachable: 0
caveats: 4
note: |
Values were read by an AI assistant on 2026-11-01 from the Carpenter Technology Super Invar 32-5 datasheet (PDF, converted with pdftotext), the Hi-Temp Metals technical data page, the USGS Mineral Commodity Summaries 2026 chapters for nickel, cobalt and iron ore (PDF), the 1972 JPL/Itek optics study (NASA NTRS PDF) and PubChem records. Caveats: the strengths and hardness are typical values of one manufacturer; the elastic modulus and the Carpenter expansion value are left out under the exponent rule; the specific gravity, martensite start and hardness names are custom; the space use comes from a 1972 design report rather than a test.
story:
recipe:
line: |
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.
parts:
- name: Iron
symbol: Fe
share_note: balance
role: Balance of the alloy. Carpenter describes the alloy as magnetic and austenitic.
source: pubchem-iron
where: Elemental iron, PubChem CID 23925 (molecular weight read there, not entered)
- name: Nickel
symbol: Ni
share_percent: 32
share_note: wt%, nominal 32.00
role: Carpenter says the alloy is designed to give minimum thermal expansion at room temperatures, and nickel is the main element in the type analysis.
source: carpenter-super-invar
where: Type analysis table, Nickel 32.00 %; elemental nickel, PubChem CID 935 (molecular weight read there, not entered)
- name: Cobalt
symbol: Co
share_percent: 5.5
share_note: wt%, nominal 5.50
role: Named in the type analysis. The datasheet does not state its role.
source: carpenter-super-invar
where: Type analysis table, Cobalt 5.50 %; elemental cobalt, PubChem CID 104730 (molecular weight read there, not entered)
risk_groups:
- title: For people
level: 1
verdict: Cobalt and nickel are sensitisers; control dust
lead: The alloy is mostly iron, but its cobalt and nickel are the health hazards, and machining produces dust and chips that carry them.
points:
- label: Skin
line: 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.
- label: Breathing
line: Cobalt is H334 (may cause allergy or asthma symptoms if inhaled) for more than 99.9 % of reports.
- title: In service
level: 2
verdict: Stable only if heat-treated near finish size
lead: Its low expansion depends on stress relief after fabrication, and the alloy oxidises during heat treatment.
points:
- label: Dimensional drift
line: Fabricating stresses change the expansion behaviour, so Carpenter says to heat-treat at or as close to finish size as possible.
- label: Oxidation
line: Above about 1000 °F (538 °C) the alloy oxidises readily, so heat treatment needs a protective atmosphere.
- title: In space
level: 1
verdict: Rejected for a 1972 telescope design
lead: The space record here is a 1972 design study. No flight or test data for Super Invar 32-5 were read.
points:
- label: What the report says
line: The 1972 JPL/Itek study did not use Super-Invar, because the expansion properties of the material were unstable over long periods of time.
- label: What is missing
line: No thermal-vacuum, outgassing or radiation test of Super Invar 32-5 was read.
why: |
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.
uses:
- where: Optical and laser systems
line: Carpenter lists optical and laser systems among the applications of Super Invar 32-5 on its datasheet.
- where: Semiconductor components and wave guide tubes
line: Carpenter lists semiconductor components, wave guide tubes and other systems with low expansion glass or quartz assemblies.
can_do:
- label: Expansion
benchmark: cte
line: 0.63 ppm/°C from -55 to 95 °C, as a mean coefficient (Hi-Temp Metals).
- label: Strength
benchmark: yield_strength
line: 276 MPa yield and 483 MPa tensile in the annealed condition (Carpenter typical values).
- label: Ductility
benchmark: elongation
line: 40 % elongation in 2 in (50.8 mm) in the annealed condition (Carpenter typical value).
- label: Density
benchmark: density
line: 8150 kg/m3 (Hi-Temp Metals).
- label: Resistivity
benchmark: electrical_resistivity
line: 481.3 ohm-cir-mil/ft at 73 °F (23 °C) (Carpenter).
compare: |
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.
compare_rows:
- label: Thermal expansion
benchmark: cte
- label: Density
benchmark: density
- label: Strength
benchmark: yield_strength
handling:
- '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.'
- Above about 1000 °F (538 °C), use a protective atmosphere such as vacuum, hydrogen, dissociated ammonia or inert gas.
- Forge at 2000/2150 °F (1093/1177 °C) and do not soak long in the furnace, which can check the surface.
- Degrease and clean machined parts soon after machining to remove residual sulfur, which can cause grain boundary embrittlement.
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:
- '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.
verdict: |
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.
References
Every number above carries a reference number. Click one to see the source and where in it the value comes from.
| # | Source | Type | Year | Used for |
|---|---|---|---|---|
| Carpenter Technology: Super Invar 32-5 data sheet | datasheet | 30 values | ||
| Hi-Temp Metals: Super Invar 32-5 technical data | web | 3 values | ||
| Mineral Commodity Summaries 2026: Nickel | report | 2026 | 1 value | |
| Mineral Commodity Summaries 2026: Cobalt | report | 2026 | 1 value | |
| Mineral Commodity Summaries 2026: Iron ore | report | 2026 | 1 value | |
| Outer Planets Mission Television Subsystem Optics Study, final report, 28 July 1972 | report | 1972 | 0 values | |
| PubChem: Cobalt (CID 104730), Safety and Hazards | database | 2026 | 1 value | |
| PubChem: Nickel (CID 935), Safety and Hazards | database | 2026 | 1 value | |
| PubChem: Iron (CID 23925), molecular weight | database | 2026 | 0 values |
Updated