Polybenzimidazole PBI
Polybenzimidazole, repeat unit C20H12N4 (molar mass 308.34 g/mol), poly[2,2'-(m-phenylene)-5,5'-bibenzimidazole] · CAS 32075-68-6
Polybenzimidazole (PBI) is an all-aromatic heterocyclic polymer, first developed in 1961 by Vogel and Marvel.
Evidence level
5 of 5
Flown or field-proven
- 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.
Hold a heat
435 degC
Resist a flame
58 percent
Survive orbit
2.21e-24 cm3/atom
Recipe, share of the weight
- C not statedCarbon
- H not statedHydrogen
- N not statedNitrogen
Best for
Flame-resistant protective fabrics and high-temperature parts that must keep stiffness, with a glass transition of 425 degC
Weakest at
Atomic oxygen in low Earth orbit (erosion yield of at least 2.21e-24 cm3/atom on MISSE 2); fine dust is flammable and explosive when suspended in air
Risk at a glance
- People Low. Dust is the watch point
- If it fails No data. No failure risks recorded
- Corrosion Moderate. PBI erodes under atomic oxygen, and the MISSE 2 flight value is only a lower bound.
Quick facts: PBI
| Property | Value | Basis |
|---|---|---|
| Density | 1.28 to 1.3 g/cm³ | 2 sourced values across conditions |
| Tensile strength | 160 MPa | 1 sourced value |
| Young's modulus | 5.9 GPa | 1 sourced value |
| Thermal conductivity | 0.41 W/(m·K) | 1 sourced value |
| Thermal expansion (CTE) | 23 ppm/K | 1 sourced value |
| Electrical resistivity | 8,000,000,000,000 Ω·m | 1 sourced value |
| Maximum service temperature | 260 to 400 °C | 2 sourced values across conditions |
What is the density of Polybenzimidazole (PBI)?
Polybenzimidazole (PBI) has a density of 1.28 to 1.3 g/cm³. The range covers 2 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.
What is the thermal conductivity of Polybenzimidazole (PBI)?
Polybenzimidazole (PBI) has a thermal conductivity of 0.41 W/(m·K). The source and test conditions are listed in the properties table on this page.
What is the coefficient of thermal expansion of Polybenzimidazole (PBI)?
Polybenzimidazole (PBI) has a coefficient of thermal expansion of 23 ppm/K. The source and test conditions are listed in the properties table on this page.
What is the tensile strength of Polybenzimidazole (PBI)?
Polybenzimidazole (PBI) has a tensile strength of 160 MPa. The source and test conditions are listed in the properties table on this page.
What is the Young's modulus of Polybenzimidazole (PBI)?
Polybenzimidazole (PBI) has a Young's modulus of 5.9 GPa. The source and test conditions are listed in the properties table on this page.
What is Polybenzimidazole (PBI) used for?
Uses recorded in the sources include Apollo-era tethers, belts and restraints; Space Shuttle stowage partitions and Skylab apparel; Protective apparel and flame-resistant clothing.
Why it exists
PBI keeps its shape and stiffness at high temperature and does not burn easily. Its glass transition is 425 degC (TotalMateria), and its limiting oxygen index is 58 percent (Goodfellow). NASA used it for Apollo tethers and Shuttle-era textiles.
Where it's used
Space textiles
NASA reports that PBI staple and multifilament fibres were used in Apollo tethers and restraints, Skylab apparel and Space Shuttle stowage partitions.
Protective clothing
Wikipedia lists protective apparel as the main use of PBI fibre.
Recipe
Polybenzimidazole, repeat unit C20H12N4 (molar mass 308.34 g/mol), poly[2,2'-(m-phenylene)-5,5'-bibenzimidazole]
PBI is an all-aromatic polymer. Its repeat unit is C20H12N4, with a molar mass of 308.34 g/mol, built from benzimidazole rings linked through a meta-phenylene group (Wikipedia). It is made by condensing diphenyl isophthalate with 3,3',4,4'-tetraaminodiphenyl, and the intermediate cyclises spontaneously (Wikipedia, Synthesis).
| Ingredient | Share of the weight | What it does |
|---|---|---|
| Carbon C | not stated | Forms the aromatic benzimidazole rings and the meta-phenylene link of the backbone. |
| Hydrogen H | not stated | Sits on the aromatic rings; the all-aromatic backbone gives the high thermal stability. |
| Nitrogen N | not stated | Forms the imidazole rings. Their hydrogen-bond network helps the polymer stay stiff and oxidation resistant. |
Weight shares are as printed in the sources.
What it can do
Hold a heat
435 degC
Holds a heat-deflection temperature of 435 degC at 0.45 MPa (Goodfellow).
Resist a flame
58 percent
Limiting oxygen index of 58 percent (Goodfellow); the page says the material does not burn.
Survive orbit
2.21e-24 cm3/atom
Atomic oxygen erosion yield on MISSE 2 is greater than 2.21e-24 cm3/atom, a lower bound (NASA Table I).
How it compares
The Goodfellow PBI product page gives a density of 1.3 g/cm3 and a tensile strength of 160 MPa, with a tensile modulus of 5.9 GPa, a glass transition of 425 degC on TotalMateria and a limiting oxygen index of 58 percent. Its density in the NASA polymer table is 1.2758 g/cm3. The APSO datasheet gives a glass transition of 415 degC and a long-term maximum service temperature of 310 degC.
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 | PBI | PAI | PBO (Zylon) | PEEK | PEI | PEK | PEKK | PES | PPS | PPSU | PSU |
|---|---|---|---|---|---|---|---|---|---|---|---|
| Thermal behavior and safety | |||||||||||
| heat deflection temperature | 435 °C4 | 278 °C | no data | no data | 173 °C | 163 °C | 164 °C | 205 °C | 400 °F | 207 °C | 174 °C |
| Thermal conductivity | 0.41 W m-1 K-16 | 0.53 W/m/K | no data | 0.29 W/(m K) | 0.22 W/m-°C | 0.29 W/m/K | no data | no data | no data | no data | no data |
| Physical and electrical | |||||||||||
| Density | 1.276 g/cm³1 | 1.41 g/cc | 1.398 g/cm³ | 1.3 g/cm³ | 1.34 g/cm³ | 1.3 g/cm³ | 1.29 g/cm³ | 1370 kg/m3 | 1.36 g/cm³ | 1.29 g/cm³ | 1.22 g/cm³ |
| Density | 1.3 g/cm³2 | 1.41 g/cc | 1.398 g/cm³ | 1.3 g/cm³ | 1.34 g/cm³ | 1.3 g/cm³ | 1.29 g/cm³ | 1370 kg/m3 | 1.36 g/cm³ | 1.29 g/cm³ | 1.22 g/cm³ |
| electrical resistivity | 8×10^14 Ohm cm11 | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data |
| Temperature behavior | |||||||||||
| glass transition temperature | 425 °C3 | 275 °C | no data | no data | 186 °C | 160 °C | 165 °C | 225 °C | 90 °C | 220 °C | 190 °C |
| glass transition temperature | 415 °C13 | 275 °C | no data | no data | 186 °C | 160 °C | 165 °C | 225 °C | 90 °C | 220 °C | 190 °C |
| Other measurements | |||||||||||
| Maximum service temperature | 260 °C5 | 260 °C | no data | no data | no data | no data | no data | 220 °C | 338 °F | no data | no data |
| Thermal expansion (CTE)Value printed as x10-6 K-1 on the product page | 23 10-6 K-1 | 3.1×10^-5 1/°C | no data | no data | 5.2×10^-5 1/°C | 55 ppm/K | 23 µm/m/K | 52 E-6/K | 2.6×10^-5 cm/cm/°C | 55 E-6/K | 5.6×10^-5 1/°C |
| elastic modulusValue printed on the Goodfellow product page | 5.9 GPa | 4136 MPa | 147.1 GPa | no data | 3200 MPa | 4300 MPa | 4000 MPa | 2640 MPa | 8.37×10^5 psi | 2340 MPa | 2480 MPa |
| ultimate tensile strength | 160 MPa7 | 138 MPa | 5.34 GPa | no data | no data | no data | 116 MPa | no data | 200 MPa | 69.6 MPa | 70.3 MPa |
| elongationValue printed on the Goodfellow product page | 3 % | 20 % | 3.52 % | no data | 50 % | 15 % | 3 to 10 % | no data | 2.5 % | 60 to 120 % | 50 % |
| limiting oxygen index | 58 %8 | no data | no data | no data | no data | no data | 38 % O2 | no data | no data | no data | no data |
| moisture absorption | 0.4 %9 | 0.4 % | no data | no data | 0.25 % | 0.6 % | 0.4 % | 2.2 % | 0.01 % | 1.1 % | 0.3 % |
| dielectric constant | 3.2 -10 | 4.2 - | no data | no data | no data | no data | 3 - | 3.9 - | 3 - | 3.44 - | 3.03 - |
| dielectric strengthValue printed on the Goodfellow product page | 21 kV/mm | 580 V/mil | no data | no data | no data | 23 kV/mm | 84 kV/mm | 37 kV/mm | 450 V/mil | 15 kV/mm | 17 kV/mm |
| Atomic oxygen erosion | > 2.21×10^-24 cm³/atom12 | no data | 1.36×10^-24 cm³/atom | 2.99×10^-24 cm³/atom | > 3.31×10^-24 cm³/atom | no data | no data | no data | no data | no data | 2.94×10^-24 cm³/atom |
| Maximum service temperature | 310 °C14 | 260 °C | no data | no data | no data | no data | no data | 220 °C | 338 °F | no data | no data |
| Minimum service temperature | -50 °C15 | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data |
| moisture absorption | 7.5 %16 | 0.4 % | no data | no data | 0.25 % | 0.6 % | 0.4 % | 2.2 % | 0.01 % | 1.1 % | 0.3 % |
| Atomic oxygen erosion | 2.27×10^-24 cm³/atom17 | no data | 1.36×10^-24 cm³/atom | 2.99×10^-24 cm³/atom | > 3.31×10^-24 cm³/atom | no data | no data | no data | no data | no data | 2.94×10^-24 cm³/atom |
Why choose it, and why not
Good for
- High-temperature parts that must keep stiffness near 400 degC, such as flame-resistant textiles and space stowage.
- Space textiles where flame resistance matters more than atomic oxygen resistance.
Watch out for
- The atomic oxygen erosion yield is a lower bound. The true erosion is higher than 2.21e-24 cm3/atom.
- Values come from different grades and forms (film, rod, fibre, bulk). Check the grade named on each row.
- The two CAS numbers (32075-68-6 and 25928-81-8) appear in different sources.
PBI is a high-temperature, flame-resistant aromatic polymer with a glass transition near 425 degC and a limiting oxygen index of 58 percent. Its weakness in low Earth orbit is atomic oxygen erosion, where NASA gives a flight lower bound of 2.21e-24 cm3/atom.
Technical details
For scientists and researchers. Everything above comes from the record below: every number with its method, its conditions and its source.
Notes
The method, full conditions and any caveat for the numbered rows above.
| # | Measurement | Method | Conditions | Caveat |
|---|---|---|---|---|
| 1 | Density | Table II density column, reported with the mass fraction of sodium ash | basis polymer density from the MISSE 2 PEACE polymer table, supplier information or density gradient | — |
| 2 | Density | Density value printed on the Goodfellow product page | basis polybenzimidazole film product listing, form not stated on the page beyond film | — |
| 3 | glass transition temperature | Value printed on the TotalMateria material data page (page lists temperature bands with the value) | basis single glass transition value printed in the material data table for the PBI entry | — |
| 4 | heat deflection temperature | Heat-deflection temperature printed in the thermal properties table | stress 0.45 MPa | — |
| 5 | Maximum service temperature | Range printed on the Goodfellow product page as 260-400 | basis upper working temperature range printed on the product page | — |
| 6 | Thermal conductivity | Value printed as 0.41@23 degC on the product page | temperature 23 °C | — |
| 7 | ultimate tensile strength | Value printed on the Goodfellow product page; Wikipedia infobox gives the same 160 MPa | basis tensile strength printed on the product page (unnotched) | — |
| 8 | limiting oxygen index | Value printed on the Goodfellow product page; the page also says Does not burn in its flammability row | basis oxygen concentration at which the sample burns, printed on the product page | — |
| 9 | moisture absorption | Value printed as water absorption over 24 hours on the product page | time over 24 hours | — |
| 10 | dielectric constant | Value printed on the Goodfellow product page at 1 MHz | frequency 1 MHz | — |
| 11 | electrical resistivity | Printed as 8x10 to the power 14 Ohmcm on the Goodfellow product page | basis volume resistivity printed on the product page | — |
| 12 | Atomic oxygen erosion | Measured erosion yield from the MISSE 2 flight sample, read from NASA Table I; NASA prints it as a lower bound | environment low Earth orbit, ISS outside Quest airlock, MISSE 2 PEACE tray, 3.95 yearsbound lower bound, printed as greater than 2.21e-24 | — |
| 13 | glass transition temperature | Value printed on the APSOplast PBI technical data sheet (compound PBI 00.004-00) | standard ISO 11357-1,-2 | — |
| 14 | Maximum service temperature | Value printed on the APSOplast PBI technical data sheet | basis maximum operating temperature, long term | — |
| 15 | Minimum service temperature | Value printed on the APSOplast PBI technical data sheet | basis minimum operating temperature | — |
| 16 | moisture absorption | Value printed on the APSOplast PBI technical data sheet | basis at saturation in air of 23 °C and 50 percent relative humidity | — |
| 17 | Atomic oxygen erosion | Predicted erosion yield from the NASA atomic oxygen predictive tool, compared with the measured value in Table VII | environment low Earth orbit prediction, MISSE 2 exposure | — |
Corrosion and compatibility
What happens when it meets other materials and environments.
| Environment | Concern | What happens |
|---|---|---|
| Low Earth orbit, atomic oxygen (MISSE 2, ISS outside the Quest airlock, 3.95 years) | moderate | PBI erodes under atomic oxygen, and the MISSE 2 flight value is only a lower bound.1 |
| Elevated temperature in air | low | PBI keeps its service range to about 400 degC.2 |
| Humid air and water | low | Water uptake is low.3 |
| Phosphoric acid in fuel-cell membranes | moderate | Phosphoric acid-doped PBI leaches out of the membrane.4 |
| # | Environment | Details | Test conditions |
|---|---|---|---|
| 1 | Low Earth orbit, atomic oxygen (MISSE 2, ISS outside the Quest airlock, 3.95 years) | The flight erosion yield was greater than 2.21e-24 cm3/atom. NASA gives a predicted value of 2.27e-24 cm3/atom for the same exposure, so the prediction and flight value are close. | fluence not printed on the PBI row of Table Iduration 3.95 years |
| 2 | Elevated temperature in air | The product page gives an upper working temperature of 260 to 400 degC and a heat-deflection temperature of 435 degC at 0.45 MPa. Wikipedia says PBI is stable above 400 degC and does not melt. | basis upper working temperature range from the product page |
| 3 | Humid air and water | Water absorption over 24 hours is 0.4 percent. Wikipedia gives a moisture regain of 13 percent, close to cotton at 16 percent. | time 24 hours |
| 4 | Phosphoric acid in fuel-cell membranes | Leaching and condensation on the phosphate groups limited phosphoric acid-doped PBI membranes. A higher acid loading degrades mechanical properties. | basis doped membranes, not the neat polymer |
Risks and side effects
Hazards to people, what happens when a cell overheats, and how the material is handled and stored.
For people
The MCAM SDS gives no GHS hazard classification, but it warns that fine dust is flammable and explosive, and that inhalation of particulates is the main route of entry.
For the mission
The MISSE 2 flight sample shows an erosion yield greater than 2.21e-24 cm3/atom, a lower bound from NASA Table I.
Test details
The original wording and numbers from the sources, for readers who want them.
Failure risks
| Failure | Trigger and consequence |
|---|---|
| Atomic oxygen erosion in low Earth orbit | Atomic oxygen fluence in LEO (MISSE 2, 3.95 years)Surface erosion, with a flight erosion yield greater than 2.21e-24 cm3/atom |
| Acid leaching in phosphoric acid-doped membranes | Phosphoric acid doping in fuel-cell electrolytesLoss of acid and conductivity; higher acid loading degrades mechanical properties |
Side effects on surrounding parts
| Affects | Effect |
|---|---|
| Surroundings | Processing can release dust; the primary route of entry is inhalation of particulates. |
Handling and storage
- Keep particulate exposure under the limits in the SDS: ACGIH TLV 10 mg/m3, OSHA PEL 15 mg/m3 total and 5 mg/m3 respirable.
- Use local exhaust ventilation and ground transfer equipment where dust can form, and remove ignition sources.
Mitigations
- Use local exhaust ventilation and dust control as the SDS directs.
Supply and geography
How common the raw materials are and where they come from.
Producer
PBI fibre and filament were developed by Hoechst Celanese under US government contracts from the Department of Defense and NASA. The company dedicated a facility to PBI filaments. No current production volume or country share was found in a source read in this run.
- Top producers
- United States
- Recycling
- Not sourced.
- Substitutes
- Wikipedia names phosphoric acid-doped PBI as one of the most mature membrane options for high-temperature PEM fuel cells.
Feedstock
PBI is made by condensing diphenyl isophthalate with 3,3',4,4'-tetraaminodiphenyl, then the intermediate cyclises (Wikipedia, Synthesis). No feedstock tonnage or price was found.
- Recycling
- Not sourced.
Documents
Datasheets, safety data sheets, papers and standards you can open.
| Document | Type | Year |
|---|---|---|
| APSOplast PBI technical data sheet (compound PBI 00.004-00) | datasheet | |
| MCAM Duratron CU60 PBI safety data sheet (SDS-2700) | sds | 2019 |
| NASA/TM-2008-215490 (MISSE 2 PEACE polymers erosion yield and density tables) | report | 2008 |
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: pbi
spore_version: 0.2
family: high-performance-polymers
name: Polybenzimidazole
abbreviation: PBI
role: High-temperature aromatic polymer used as flame-resistant fibre and moulded resin, and in NASA space textiles
category: polymers
type: high-performance
summary: |
Polybenzimidazole (PBI) is an all-aromatic heterocyclic polymer, first developed in 1961 by Vogel and Marvel. It has no melting point and is usually yellow to brown. Goodfellow lists a density of 1.3 g/cm3, a heat deflection temperature of 435 degC at 0.45 MPa, a tensile strength of 160 MPa, a tensile modulus of 5.9 GPa and a limiting oxygen index of 58 percent. TotalMateria gives a glass transition of 425 degC. As a sample on the MISSE 2 PEACE experiment in low Earth orbit it had an atomic oxygen erosion yield of more than 2.21e-24 cm3/atom, which NASA prints as a lower bound (greater-than sign).
best_for: Flame-resistant protective fabrics and high-temperature parts that must keep stiffness, with a glass transition of 425 degC
weakest_at: Atomic oxygen in low Earth orbit (erosion yield of at least 2.21e-24 cm3/atom on MISSE 2); fine dust is flammable and explosive when suspended in air
identity:
formula: Polybenzimidazole, repeat unit C20H12N4 (molar mass 308.34 g/mol), poly[2,2'-(m-phenylene)-5,5'-bibenzimidazole]
cas: 32075-68-6
source: wiki-pbi
where: 'Wikipedia Polybenzimidazole page (infobox: repeat-unit formula and molar mass; chemical name). CAS 32075-68-6 is also printed on the Goodfellow PBI film page. The MCAM SDS gives CAS 25928-81-8 for polybenzimidazole, so both numbers are recorded and the difference is listed in gaps.'
tags:
environments:
- low-earth-orbit
stresses:
- atomic-oxygen
applications:
- habitats-and-suits
properties:
- benchmark: density
value: 1.2758
unit: g/cm3
scope: material
conditions:
basis: polymer density from the MISSE 2 PEACE polymer table, supplier information or density gradient
method: Table II density column, reported with the mass fraction of sodium ash
status: ground
source: nasa-misse2-pbi
where: Table II (MISSE 2 PEACE polymers density and fractional ash content), row Polybenzimidazole PBI
- benchmark: density
value: 1.3
unit: g/cm3
scope: material
conditions:
basis: polybenzimidazole film product listing, form not stated on the page beyond film
method: Density value printed on the Goodfellow product page
status: ground
source: goodfellow-pbi
where: Mechanical and Physical Properties table, Density( gcm-3 ) row
- benchmark: glass_transition_temperature
value: 425
unit: degC
scope: material
conditions:
basis: single glass transition value printed in the material data table for the PBI entry
method: Value printed on the TotalMateria material data page (page lists temperature bands with the value)
status: ground
source: totalmateria-pbi
where: Physical properties, row Glass Transition Temperature, Tg
- benchmark: heat_deflection_temperature
value: 435
unit: degC
scope: material
conditions:
stress: 0.45 MPa
method: Heat-deflection temperature printed in the thermal properties table
status: ground
source: goodfellow-pbi
where: Thermal Properties table, row Heat-deflection temperature - 0.45MPa( C )
- benchmark: max_service_temp
value: 260
value_high: 400
unit: degC
scope: material
conditions:
basis: upper working temperature range printed on the product page
method: Range printed on the Goodfellow product page as 260-400
status: ground
source: goodfellow-pbi
where: Thermal Properties table, row Upper working temperature( C ) 260-400
- benchmark: thermal_conductivity
value: 0.41
unit: W m-1 K-1
scope: material
conditions:
temperature: 23 degC
method: Value printed as 0.41@23 degC on the product page
status: ground
source: goodfellow-pbi
where: Thermal Properties table, row Thermal conductivity
- benchmark: cte
value: 23
unit: 10-6 K-1
scope: material
conditions:
basis: coefficient of thermal expansion as printed on the product page, temperature not stated
method: Value printed as x10-6 K-1 on the product page
status: ground
source: goodfellow-pbi
where: Thermal Properties table, row Coefficient of thermal expansion
- benchmark: elastic_modulus
value: 5.9
unit: GPa
scope: material
conditions:
basis: tensile modulus printed on the product page
method: Value printed on the Goodfellow product page
status: ground
source: goodfellow-pbi
where: Mechanical Properties table, row Tensile modulus( GPa )
- benchmark: ultimate_tensile_strength
value: 160
unit: MPa
scope: material
conditions:
basis: tensile strength printed on the product page (unnotched)
method: Value printed on the Goodfellow product page; Wikipedia infobox gives the same 160 MPa
status: ground
source: goodfellow-pbi
where: Mechanical Properties table, row Tensile strength( MPa )
- benchmark: elongation
value: 3
unit: '%'
scope: material
conditions:
basis: elongation at break printed on the product page
method: Value printed on the Goodfellow product page
status: ground
source: goodfellow-pbi
where: Mechanical Properties table, row Elongation at break( % )
- benchmark: limiting_oxygen_index
value: 58
unit: '%'
scope: material
conditions:
basis: oxygen concentration at which the sample burns, printed on the product page
method: Value printed on the Goodfellow product page; the page also says Does not burn in its flammability row
status: ground
source: goodfellow-pbi
where: Physical Properties table, row Limiting oxygen index( % )
- benchmark: moisture_absorption
value: 0.4
unit: '%'
scope: material
conditions:
time: over 24 hours
method: Value printed as water absorption over 24 hours on the product page
status: ground
source: goodfellow-pbi
where: Physical Properties table, row Water absorption - over 24 hours( % )
- benchmark: dielectric_constant
value: 3.2
unit: '-'
scope: material
conditions:
frequency: 1 MHz
method: Value printed on the Goodfellow product page at 1 MHz
status: ground
source: goodfellow-pbi
where: Electrical Properties table, row Dielectric constant @1MHz
- benchmark: dielectric_strength
value: 21
unit: kV/mm
scope: material
conditions:
basis: dielectric strength printed on the product page
method: Value printed on the Goodfellow product page
status: ground
source: goodfellow-pbi
where: Electrical Properties table, row Dielectric strength( kV mm-1 )
- benchmark: electrical_resistivity
value: 800000000000000
unit: Ohm cm
scope: material
conditions:
basis: volume resistivity printed on the product page
method: Printed as 8x10 to the power 14 Ohmcm on the Goodfellow product page
status: ground
source: goodfellow-pbi
where: Electrical Properties table, row Volume resistivity( Ohmcm )
- benchmark: atomic_oxygen_erosion_yield
value: 2.21e-24
unit: cm3/atom
bound: lower
scope: material
conditions:
environment: low Earth orbit, ISS outside Quest airlock, MISSE 2 PEACE tray, 3.95 years
bound: lower bound, printed as greater than 2.21e-24
method: Measured erosion yield from the MISSE 2 flight sample, read from NASA Table I; NASA prints it as a lower bound
status: flight
source: nasa-misse2-pbi
where: Table I (MISSE 2 PEACE polymers erosion yield data), row Polybenzimidazole PBI
- benchmark: glass_transition_temperature
value: 415
unit: degC
scope: material
conditions:
standard: ISO 11357-1,-2
method: Value printed on the APSOplast PBI technical data sheet (compound PBI 00.004-00)
status: ground
source: apso-pbi
where: Thermal attributes, row Glass transition temperature (ISO 11357-1,-2)
- benchmark: max_service_temp
value: 310
unit: degC
scope: material
conditions:
basis: maximum operating temperature, long term
method: Value printed on the APSOplast PBI technical data sheet
status: ground
source: apso-pbi
where: Thermal attributes, row Max. operating temperature long term
- benchmark: min_service_temp
value: -50
unit: degC
scope: material
conditions:
basis: minimum operating temperature
method: Value printed on the APSOplast PBI technical data sheet
status: ground
source: apso-pbi
where: Thermal attributes, row Min. operating temperature
- benchmark: moisture_absorption
value: 7.5
unit: '%'
scope: material
conditions:
basis: at saturation in air of 23 degC and 50 percent relative humidity
method: Value printed on the APSOplast PBI technical data sheet
status: ground
source: apso-pbi
where: Other attributes, row Moisture absorption
- benchmark: atomic_oxygen_erosion_yield
value: 2.27e-24
unit: cm3/atom
scope: material
conditions:
environment: low Earth orbit prediction, MISSE 2 exposure
method: Predicted erosion yield from the NASA atomic oxygen predictive tool, compared with the measured value in Table VII
status: calculated
source: nasa-misse2-pbi
where: Table VII (comparison of the predicted and actual erosion yields), row Polybenzimidazole PBI, predicted column
corrosion:
- environment: Low Earth orbit, atomic oxygen (MISSE 2, ISS outside the Quest airlock, 3.95 years)
headline: PBI erodes under atomic oxygen, and the MISSE 2 flight value is only a lower bound.
effect: The flight erosion yield was greater than 2.21e-24 cm3/atom. NASA gives a predicted value of 2.27e-24 cm3/atom for the same exposure, so the prediction and flight value are close.
rating: moderate
conditions:
fluence: not printed on the PBI row of Table I
duration: 3.95 years
source: nasa-misse2-pbi
where: Table I and Table VII (NASA/TM-2008-215490)
- environment: Elevated temperature in air
headline: PBI keeps its service range to about 400 degC.
effect: The product page gives an upper working temperature of 260 to 400 degC and a heat-deflection temperature of 435 degC at 0.45 MPa. Wikipedia says PBI is stable above 400 degC and does not melt.
rating: low
conditions:
basis: upper working temperature range from the product page
source: goodfellow-pbi
where: Thermal Properties table
- environment: Humid air and water
headline: Water uptake is low.
effect: Water absorption over 24 hours is 0.4 percent. Wikipedia gives a moisture regain of 13 percent, close to cotton at 16 percent.
rating: low
conditions:
time: 24 hours
source: goodfellow-pbi
where: Physical Properties table, Water absorption row
- environment: Phosphoric acid in fuel-cell membranes
headline: Phosphoric acid-doped PBI leaches out of the membrane.
effect: Leaching and condensation on the phosphate groups limited phosphoric acid-doped PBI membranes. A higher acid loading degrades mechanical properties.
rating: moderate
conditions:
basis: doped membranes, not the neat polymer
source: pmc-pa-pbi-review
where: Introduction and PBI membrane sections
risks:
hazards:
- text: 'The MCAM safety data sheet gives no GHS classification for polybenzimidazole: classification none, no signal word, no hazard statements.'
ghs: []
source: mcam-sds-pbi
where: Section 2 (GHS classifications)
- text: Dust is flammable and explosive when finely divided and suspended in air, so dust control and grounding apply during handling.
ghs: []
source: mcam-sds-pbi
where: Section 5 (fire-fighting measures) and Section 7 (dust handling)
failure_risks:
- mode: Atomic oxygen erosion in low Earth orbit
trigger: Atomic oxygen fluence in LEO (MISSE 2, 3.95 years)
consequence: Surface erosion, with a flight erosion yield greater than 2.21e-24 cm3/atom
source: nasa-misse2-pbi
where: Table I
- mode: Acid leaching in phosphoric acid-doped membranes
trigger: Phosphoric acid doping in fuel-cell electrolytes
consequence: Loss of acid and conductivity; higher acid loading degrades mechanical properties
source: pmc-pa-pbi-review
where: PBI membrane section
side_effects:
- text: Processing can release dust; the primary route of entry is inhalation of particulates.
source: mcam-sds-pbi
where: Section 11 (toxicological information), primary route of entry
handling:
- text: 'Keep particulate exposure under the limits in the SDS: ACGIH TLV 10 mg/m3, OSHA PEL 15 mg/m3 total and 5 mg/m3 respirable.'
source: mcam-sds-pbi
where: Section 8 (exposure controls), particulates table
- text: Use local exhaust ventilation and ground transfer equipment where dust can form, and remove ignition sources.
source: mcam-sds-pbi
where: Section 7 (handling and storage)
mitigations:
- text: Use local exhaust ventilation and dust control as the SDS directs.
source: mcam-sds-pbi
where: Section 8 (exposure controls)
uses:
- application: habitats-and-suits
device: Apollo-era tethers, belts and restraints
example: NASA reports that PBI multifilament yarns were used in tethers, belts and restraints in the Apollo program.
source: ntrs-flame-fibers-2017
where: Section on the development of polybenzimidazole fibers
- application: habitats-and-suits
device: Space Shuttle stowage partitions and Skylab apparel
example: NASA reports that PBI staple fibre was used in apparel fabrics for Skylab and in stowage partitions for the Space Shuttle programme.
source: ntrs-flame-fibers-2017
where: Section on the development of polybenzimidazole fibers
- application: habitats-and-suits
device: Protective apparel and flame-resistant clothing
example: Wikipedia lists protective apparel as the first application of PBI fibre, and the Goodfellow page lists flammability as Does not burn.
source: wiki-pbi
where: Applications, 4.1 Protective apparel; Goodfellow Physical Properties table
supply:
- subject: Producer
abundance: PBI fibre and filament were developed by Hoechst Celanese under US government contracts from the Department of Defense and NASA. The company dedicated a facility to PBI filaments. No current production volume or country share was found in a source read in this run.
producers:
- name: Hoechst Celanese
note: Named as the developer and the producer of PBI filaments in the NASA report
country: United States
critical_lists: []
recycling: Not sourced.
substitutes:
- Wikipedia names phosphoric acid-doped PBI as one of the most mature membrane options for high-temperature PEM fuel cells.
source: ntrs-flame-fibers-2017
where: Section on the development of polybenzimidazole fibers and the closing section on the Hoechst-Celanese facility
- subject: Feedstock
abundance: PBI is made by condensing diphenyl isophthalate with 3,3',4,4'-tetraaminodiphenyl, then the intermediate cyclises (Wikipedia, Synthesis). No feedstock tonnage or price was found.
producers: []
critical_lists: []
recycling: Not sourced.
substitutes: []
source: wiki-pbi
where: Synthesis section
story:
recipe:
line: PBI is an all-aromatic polymer. Its repeat unit is C20H12N4, with a molar mass of 308.34 g/mol, built from benzimidazole rings linked through a meta-phenylene group (Wikipedia). It is made by condensing diphenyl isophthalate with 3,3',4,4'-tetraaminodiphenyl, and the intermediate cyclises spontaneously (Wikipedia, Synthesis).
parts:
- name: Carbon
symbol: C
role: Forms the aromatic benzimidazole rings and the meta-phenylene link of the backbone.
- name: Hydrogen
symbol: H
role: Sits on the aromatic rings; the all-aromatic backbone gives the high thermal stability.
- name: Nitrogen
symbol: 'N'
role: Forms the imidazole rings. Their hydrogen-bond network helps the polymer stay stiff and oxidation resistant.
risk_groups:
- title: For people
level: 1
verdict: Dust is the watch point
lead: The MCAM SDS gives no GHS hazard classification, but it warns that fine dust is flammable and explosive, and that inhalation of particulates is the main route of entry.
- title: For the mission
level: 2
verdict: Atomic oxygen erodes it
lead: The MISSE 2 flight sample shows an erosion yield greater than 2.21e-24 cm3/atom, a lower bound from NASA Table I.
why: PBI keeps its shape and stiffness at high temperature and does not burn easily. Its glass transition is 425 degC (TotalMateria), and its limiting oxygen index is 58 percent (Goodfellow). NASA used it for Apollo tethers and Shuttle-era textiles.
uses:
- where: Space textiles
line: NASA reports that PBI staple and multifilament fibres were used in Apollo tethers and restraints, Skylab apparel and Space Shuttle stowage partitions.
- where: Protective clothing
line: Wikipedia lists protective apparel as the main use of PBI fibre.
can_do:
- label: Hold a heat
value: 435 degC
line: Holds a heat-deflection temperature of 435 degC at 0.45 MPa (Goodfellow).
- label: Resist a flame
value: 58 percent
line: Limiting oxygen index of 58 percent (Goodfellow); the page says the material does not burn.
- label: Survive orbit
value: 2.21e-24 cm3/atom
line: Atomic oxygen erosion yield on MISSE 2 is greater than 2.21e-24 cm3/atom, a lower bound (NASA Table I).
compare: The Goodfellow PBI product page gives a density of 1.3 g/cm3 and a tensile strength of 160 MPa, with a tensile modulus of 5.9 GPa, a glass transition of 425 degC on TotalMateria and a limiting oxygen index of 58 percent. Its density in the NASA polymer table is 1.2758 g/cm3. The APSO datasheet gives a glass transition of 415 degC and a long-term maximum service temperature of 310 degC.
compare_rows:
- label: Density
benchmark: density
- label: Glass transition
benchmark: glass_transition_temperature
- label: Atomic oxygen erosion yield in LEO
benchmark: atomic_oxygen_erosion_yield
handling:
- 'Keep dust levels within the SDS limits: 10 mg/m3 ACGIH TLV, 15 mg/m3 OSHA PEL total and 5 mg/m3 respirable.'
- Use local exhaust ventilation and grounding where dust forms, and keep ignition sources away from processing areas.
good_for:
- High-temperature parts that must keep stiffness near 400 degC, such as flame-resistant textiles and space stowage.
- Space textiles where flame resistance matters more than atomic oxygen resistance.
watch_out:
- The atomic oxygen erosion yield is a lower bound. The true erosion is higher than 2.21e-24 cm3/atom.
- Values come from different grades and forms (film, rod, fibre, bulk). Check the grade named on each row.
- The two CAS numbers (32075-68-6 and 25928-81-8) appear in different sources.
verdict: PBI is a high-temperature, flame-resistant aromatic polymer with a glass transition near 425 degC and a limiting oxygen index of 58 percent. Its weakness in low Earth orbit is atomic oxygen erosion, where NASA gives a flight lower bound of 2.21e-24 cm3/atom.
gaps:
- No PBI composition or CAS number was read from PubChem; the PubChem lookup by name and by CAS 25928-81-8 returned no CID in this run.
- No flight result beyond the MISSE 2 erosion yield; no UV, radiation or thermal-cycling result for PBI was found in a fetched page.
- 'Two CAS numbers are printed for PBI: 32075-68-6 (Wikipedia, Goodfellow) and 25928-81-8 (MCAM SDS). The source of each is recorded.'
- No production volume or country share was found in a fetched source; the only producer named is Hoechst Celanese from the NASA report.
- Limiting oxygen index, compressive modulus and atomic oxygen erosion yield are not in the canonical property list; they use short names (limiting_oxygen_index, atomic_oxygen_erosion_yield).
- Hazard data rest on one MCAM SDS for the polymer. The Newtex sulfonated PBI SDS was not fetched.
- Glass transition in Wikipedia is given as about 430 degC; only the TotalMateria value (425 degC) is recorded as a property.
sources:
nasa-misse2-pbi:
title: 'NASA/TM-2008-215490: Atomic Oxygen Erosion Yield Predictive Tool for Spacecraft Polymers in Low Earth Orbit (Banks, Backus and de Groh, 2008)'
kind: report
url: https://ntrs.nasa.gov/api/citations/20090011780/downloads/20090011780.pdf
year: 2008
wiki-pbi:
title: Polybenzimidazole (Wikipedia)
kind: web
url: https://en.wikipedia.org/wiki/Polybenzimidazole
year: 2026
goodfellow-pbi:
title: 'Goodfellow: Polybenzimidazole Film, PBI, CAS 32075-68-6 (product page)'
kind: datasheet
url: https://www.goodfellow.com/usa/polybenzimidazole-film-group
totalmateria-pbi:
title: 'TotalMateria: PBI material data page (material 5094597)'
kind: datasheet
url: https://www.totalmateria.com/en-us/material/5094597
mcam-sds-pbi:
title: 'Mitsubishi Chemical Advanced Materials: Duratron CU60 PBI safety data sheet (SDS-2700, revised 23 October 2019)'
kind: datasheet
url: https://www.boedeker.com/Portals/0/Safety Data Sheets SDS/MCAM/MCAM-Duratron-CU60-PBI-EN-SDS-2700-191023.pdf
ntrs-flame-fibers-2017:
title: 'Flame Retardant Fibers for Human Space Exploration: Past, Present, and Future (NASA NTRS 20170008542)'
kind: report
url: https://ntrs.nasa.gov/api/citations/20170008542/downloads/20170008542.pdf
year: 2017
apso-pbi:
title: APSOplast PBI technical data sheet (compound PBI 00.004-00)
kind: datasheet
url: https://www.apsoparts.com/media/downloads/asset//std.lang.all/0_/en/PBI_00_004-00_EN.pdf
pmc-pa-pbi-review:
title: 'Ionic Liquid in Phosphoric Acid-Doped Polybenzimidazole (PA-PBI) as Electrolyte Membranes for PEM Fuel Cells: A Review (PMC8541579)'
kind: paper
url: https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8541579/
documents:
- title: APSOplast PBI technical data sheet (compound PBI 00.004-00)
type: datasheet
url: https://www.apsoparts.com/media/downloads/asset//std.lang.all/0_/en/PBI_00_004-00_EN.pdf
- title: MCAM Duratron CU60 PBI safety data sheet (SDS-2700)
type: sds
url: https://www.boedeker.com/Portals/0/Safety Data Sheets SDS/MCAM/MCAM-Duratron-CU60-PBI-EN-SDS-2700-191023.pdf
year: 2019
- title: NASA/TM-2008-215490 (MISSE 2 PEACE polymers erosion yield and density tables)
type: report
url: https://ntrs.nasa.gov/api/citations/20090011780/downloads/20090011780.pdf
year: 2008
status: draft
updated: '2026-10-20'
review: {}
license: CC-BY-4.0
meta:
status: draft
method: assistant
checked_values: 21
unreachable: 1
caveats: 4
note: 'Written on 2026-10-20 by an AI assistant from pages read in this run: the NASA PDF (NTRS 20090011780) read with curl and pdftotext, Wikipedia, the Goodfellow PBI page, the TotalMateria PBI page, the MCAM SDS PDF, the NASA NTRS 20170008542 PDF and the PMC8541579 review. The PubChem record was not 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 |
|---|---|---|---|---|
| NASA/TM-2008-215490: Atomic Oxygen Erosion Yield Predictive Tool for Spacecraft Polymers in Low Earth Orbit (Banks, Backus and de Groh, 2008) | report | 2008 | 5 values | |
| Polybenzimidazole (Wikipedia) | web | 2026 | 3 values | |
| Goodfellow: Polybenzimidazole Film, PBI, CAS 32075-68-6 (product page) | datasheet | 15 values | ||
| TotalMateria: PBI material data page (material 5094597) | datasheet | 1 value | ||
| Mitsubishi Chemical Advanced Materials: Duratron CU60 PBI safety data sheet (SDS-2700, revised 23 October 2019) | datasheet | 6 values | ||
| Flame Retardant Fibers for Human Space Exploration: Past, Present, and Future (NASA NTRS 20170008542) | report | 2017 | 3 values | |
| APSOplast PBI technical data sheet (compound PBI 00.004-00) | datasheet | 4 values | ||
| Ionic Liquid in Phosphoric Acid-Doped Polybenzimidazole (PA-PBI) as Electrolyte Membranes for PEM Fuel Cells: A Review (PMC8541579) | paper | 2 values |