Polyvinyl fluoride (clear Tedlar) PVF
(-CH2-CHF-)n · CAS 24981-14-4
Clear Tedlar is a biaxially oriented polyvinyl fluoride film from DuPont with no plasticizers.
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.
Atomic oxygen
3.19e-24 cm3/atom (clear)
Pigmented atomic oxygen
1.01e-25 cm3/atom (white)
Continuous use
-72 to 107 degC
Recipe, share of the weight
- C 52.2%Carbon
- H 6.6%Hydrogen
- F 41.3%Fluorine
Best for
Weatherable, tough, flexible thin film for outdoor or decorative surfaces where a pigment can shield it from atomic oxygen
Weakest at
Clear film erodes under atomic oxygen about as fast as Kapton H (NASA MISSE 2), so it needs pigment or a shield in low Earth orbit
Risk at a glance
- People Low. No hazard sheet was read; treat as a plastic film
- If it fails No data. No failure risks recorded
- Corrosion Severe. DuPont rates Tedlar as having excellent weathering resistance.
Quick facts: PVF
| Property | Value | Basis |
|---|---|---|
| Density | 1.37 to 1.72 g/cm³ | 2 sourced values across conditions |
| Tensile strength | 55.2 to 110 MPa | 1 sourced value |
| Thermal expansion (CTE) | 15.6 ppm/K | 1 sourced value |
| Maximum service temperature | 107 °C | 1 sourced value |
What is the density of Polyvinyl fluoride (clear Tedlar) (PVF)?
Polyvinyl fluoride (clear Tedlar) (PVF) has a density of 1.37 to 1.72 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 Polyvinyl fluoride (clear Tedlar) (PVF)?
Polyvinyl fluoride (clear Tedlar) (PVF) has a coefficient of thermal expansion of 15.6 ppm/K. The source and test conditions are listed in the properties table on this page.
What is the tensile strength of Polyvinyl fluoride (clear Tedlar) (PVF)?
Polyvinyl fluoride (clear Tedlar) (PVF) has a tensile strength of 55.2 to 110 MPa. The source and test conditions are listed in the properties table on this page.
What is the maximum service temperature of Polyvinyl fluoride (clear Tedlar) (PVF)?
Polyvinyl fluoride (clear Tedlar) (PVF) has a maximum service temperature of 107 °C. The source and test conditions are listed in the properties table on this page.
What is Polyvinyl fluoride (clear Tedlar) (PVF) used for?
Uses recorded in the sources include Printed circuit board and composite part release sheet (Tedlar S surface); Clear PVF film on the MISSE 2 PEACE tray exposed outside the ISS airlock.
Why it exists
Polyvinyl fluoride is a tough, flexible fluoropolymer film. Clear Tedlar eroded under atomic oxygen on MISSE 2 at about the rate of Kapton H, but its white pigmented form eroded about 30 times more slowly.
Where it's used
Printed circuit board fabrication
DuPont says the S surface of Tedlar is especially suited as a release sheet for printed circuit board and composite part fabrication.
MISSE 2 flight test
Clear PVF was flown outside the ISS airlock on MISSE 2 from 2001 to 2005 to measure atomic oxygen erosion.
Recipe
(-CH2-CHF-)n
PVF is made by polymerizing vinyl fluoride, C2H3F, usually by suspension or emulsion polymerization in water with peroxide or azo initiators (Wikipedia). The polymer is then dissolved, mixed with additives, cast or extruded, and biaxially oriented into thin film (Wikipedia, DuPont). Its repeat unit is C2H3F, with two carbons, three hydrogens and one fluorine (NASA Table V).
| Ingredient | Atoms per unit | Share of the weight | What it does |
|---|---|---|---|
| Carbon C | 2 | 52.2% | The two backbone carbons of each repeat unit. |
| Hydrogen H | 3 | 6.6% | Three hydrogens on the backbone carbons. |
| Fluorine F | 1 | 41.3% | One fluorine on the backbone, which makes the polymer a fluoropolymer. |
Weight shares are calculated from standard atomic weights.
What it can do
Atomic oxygen
3.19e-24 cm3/atom (clear)
Clear PVF eroded at 3.19 × 10⁻²⁴ cm³/atom on MISSE 2, close to Kapton H at 3.00 × 10⁻²⁴ in the same table.
Pigmented atomic oxygen
1.01e-25 cm3/atom (white)
White pigmented PVF eroded at 1.01 × 10⁻²⁵ cm³/atom, because titanium dioxide shields the polymer.
Continuous use
-72 to 107 degC
DuPont rates continuous use from -72 to 107 degC.
How it compares
On the MISSE 2 flight, clear PVF eroded at 3.19 × 10⁻²⁴ cm³/atom, against 3.00 × 10⁻²⁴ for Kapton H in the same NASA table, while white pigmented PVF eroded at only 1.01 × 10⁻²⁵. Its tensile strength and elongation are modest, with DuPont giving 8 to 16 kpsi and 90 to 250 percent elongation.
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 | PVF | AF | PCTFE (CTFE, Kel-F) | ECTFE (Halar) | ETFE | FEP | PFA | PTFE | PVDF (Kynar) | PVF (white Tedlar) |
|---|---|---|---|---|---|---|---|---|---|---|
| Physical and electrical | ||||||||||
| Density (clear PVF, MISSE 2 sample) | 1.379 g/cm³1 | 2.146 g/cm³ | 2.133 g/cm³ | 1.68 g/cm³ | 1.74 g/cm³ | 2.144 g/cm³ | 2.138 g/cm³ | 2.17 g/cm³ | no data | 1.624 g/cm³ |
| Density range (Tedlar PVF film) | 1.37 g/cc2 | 2.146 g/cm³ | 2.133 g/cm³ | 1.68 g/cm³ | 1.74 g/cm³ | 2.144 g/cm³ | 2.138 g/cm³ | 2.17 g/cm³ | no data | 1.624 g/cm³ |
| Temperature behavior | ||||||||||
| Zero strength temperature | 260 °C7 | no data | no data | no data | no data | no data | no data | no data | no data | no data |
| Other measurements | ||||||||||
| Atomic oxygen erosion yield, clear PVF (MISSE 2) | 3.19×10^-24 cm³/atom3 | 1.98×10^-25 cm³/atom | 8.31×10^-25 cm³/atom | 1.79×10^-24 cm³/atom | 9.61×10^-25 cm³/atom | 2×10^-25 cm³/atom | 1.73×10^-25 cm³/atom | 1.42×10^-25 cm³/atom | 1.29×10^-24 cm³/atom | 1.01×10^-25 cm³/atom |
| Atomic oxygen erosion yield, white pigmented PVF (MISSE 2) | 1.01×10^-25 cm³/atom4 | 1.98×10^-25 cm³/atom | 8.31×10^-25 cm³/atom | 1.79×10^-24 cm³/atom | 9.61×10^-25 cm³/atom | 2×10^-25 cm³/atom | 1.73×10^-25 cm³/atom | 1.42×10^-25 cm³/atom | 1.29×10^-24 cm³/atom | 1.01×10^-25 cm³/atom |
| Continuous use lower limit | -72 °C5 | no data | no data | -76 °C | no data | no data | no data | -200 °C | no data | -72 °C |
| Continuous use upper limit | 107 °C6 | no data | 175 °C | 149 °C | 150 °C | 204 °C | 260 °C | 260 °C | no data | 107 °C |
| Ultimate tensile strength (ASTM D-882) | 8 kpsi8 | 26.9 MPa | 34 MPa | 7000 psi | 40 MPa | 20 MPa | 21 MPa | no data | no data | 55 MPa |
| Ultimate elongation (ASTM D-882)Typical range printed in the DuPont table | 90 % | 17.1 % | 100 % | 200 % | 300 % | 300 % | 300 % | no data | no data | 90 % |
| Moisture absorption (upper limit) | 0.5 %9 | 0.01 % | no data | 0.1 % | no data | 0.01 % | no data | no data | no data | 0.5 % |
| Refractive index (nD)Value printed in the DuPont table | 1.46 nD | 1.31 unitless | no data | no data | no data | no data | 1.35 - | no data | no data | 1.46 nD |
| Linear coefficient of expansion | 2.8×10^-5 in/in/degF10 | no data | no data | 5.6×10^-5 in/in/°F | no data | no data | no data | 12 x 10^-5 per °C | no data | 9.7×10^-5 m/mK |
| Molar mass of the repeat unit (C2H3F) | 46.04 g/mol11 | no data | 116.5 g/mole | no data | no data | no data | no data | no data | no data | no data |
Why choose it, and why not
Good for
- Weatherable, tough flexible film for outdoor or decorative surfaces (DuPont).
- Release sheet for printed circuit board and composite part fabrication (DuPont).
- Pigmented films where atomic oxygen resistance matters, such as the white Tedlar on MISSE 2 (NASA).
Watch out for
- Atomic oxygen. The clear film eroded at 3.19 × 10⁻²⁴ cm³/atom on MISSE 2, so it needs a pigment or a shield in low Earth orbit.
- Temperature. DuPont rates continuous use to 107 degC and zero strength at 260 to 300 degC.
- Gaps in the record. No hazard sheet, PubChem record, melting point or radiation value was read in this run.
Clear Tedlar is a weatherable, flexible fluoropolymer film with good aging and chemical resistance, but on the MISSE 2 flight it eroded in low Earth orbit about as fast as Kapton H. Pigmented PVF is much more durable under atomic oxygen, so the pigment is the key choice for space use.
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 (clear PVF, MISSE 2 sample) | Value printed in the NASA table of polymer densities | form clear Tedlar film used on MISSE 2test standard density gradient column (ref. 12 in the NASA report) | — |
| 2 | Density range (Tedlar PVF film) | Typical-value range printed in the DuPont general properties table | form DuPont Tedlar PVF film, all typestest standard ASTM D-1505 | — |
| 3 | Atomic oxygen erosion yield, clear PVF (MISSE 2) | Measured on the MISSE 2 PEACE flight sample and reported in the NASA predictive-tool report | environment low Earth orbit, ISS, MISSE 2 PEACE trayfluence 8.43e21 atoms/cm2 (from the NASA report text) | — |
| 4 | Atomic oxygen erosion yield, white pigmented PVF (MISSE 2) | Measured on the MISSE 2 PEACE flight sample; the NASA report attributes the difference to pigment shielding | environment low Earth orbit, ISS, MISSE 2 PEACE trayform crystalline PVF with white (titanium dioxide) pigment | — |
| 5 | Continuous use lower limit | Printed manufacturer temperature range (printed as -72 to 107 degC, -98 to 225 degF) | form DuPont Tedlar PVF filmuse continuous use | — |
| 6 | Continuous use upper limit | Printed manufacturer temperature range (printed as -72 to 107 degC, -98 to 225 degF) | form DuPont Tedlar PVF filmuse continuous use | — |
| 7 | Zero strength temperature | Range printed in the DuPont general properties table (printed as 260 to 300 degC, 500 to 570 degF) | test method hot bar | — |
| 8 | Ultimate tensile strength (ASTM D-882) | Printed as 8 to 16 x 10^3 psi in the DuPont table; entered as kpsi with the same numbers | test standard ASTM D-882temperature 22 °C (72 degF) | — |
| 9 | Moisture absorption (upper limit) | Upper bound printed in the DuPont table; not a typical value | test method water immersiontemperature 22 °C (72 degF)note printed as less than 0.5 percent for most types | — |
| 10 | Linear coefficient of expansion | Value printed in the DuPont table as 2.8 x 10-5 in/in/degF | form Tedlar PVF film | — |
| 11 | Molar mass of the repeat unit (C2H3F) | Value printed in the NASA table of atomic mass units per repeat unit | basis repeat unit C2H3F | — |
Corrosion and compatibility
What happens when it meets other materials and environments.
| Environment | Concern | What happens |
|---|---|---|
| Atomic oxygen in low Earth orbit | moderate | Clear PVF eroded at about the same rate as Kapton H on the ISS, but pigmented PVF eroded about 30 times more slowly.1 |
| Sunlight and weathering | severe | DuPont rates Tedlar as having excellent weathering resistance.2 |
| Heat ageing | severe | Tedlar has no plasticizers, so it keeps its properties on heat ageing.3 |
| Chemical exposure | severe | PVF shows no visible effect after one year of immersion in acids, bases and solvents at 25 degC.4 |
| # | Environment | Details | Test conditions |
|---|---|---|---|
| 1 | Atomic oxygen in low Earth orbit | MISSE 2 erosion yield was 3.19e-24 cm3/atom for clear PVF, against 3.00e-24 for Kapton H, and 1.01e-25 for white pigmented PVF. The NASA report says titanium dioxide pigment shields the film. | flight MISSE 2, fluence 8.43e21 atoms/cm2 |
| 2 | Sunlight and weathering | The DuPont table lists weatherability as excellent for Florida exposure facing south at 45 degrees. The brochure says outdoor weathering tests on pigmented films have run for more than 20 years. A 2025 Frontiers review attributes the aging resistance of Tedlar composite films to inorganic fillers that block light. | exposure Florida, facing south at 45 degrees to horizontal |
| 3 | Heat ageing | DuPont lists an aging test of 3000 hours in a circulating air oven at 150 degC for Tedlar, without a retained-property figure. The sheet says the lack of plasticizer gives good aging properties. | test 3000 hr circulating air oven at 150 °C |
| 4 | Chemical exposure | DuPont reports no visible effect after 1 year immersion at 25 degC and after 2 hours at boiling for acids, bases and solvents, and says strength and appearance were not affected by 5 years soil burial. | test 1 yr immersion at 25 °C; 2 hr at boiling |
Risks and side effects
Hazards to people, what happens when a cell overheats, and how the material is handled and stored.
For people
No manufacturer safety data sheet or GHS classification for PVF was read in this run, so no hazard is stated for people.
- Not checked
- The ChemicalBook PVF safety sheet has no hazard data, and PubChem was blocked in this run.
Test details
The original wording and numbers from the sources, for readers who want them.
Failure risks
| Failure | Trigger and consequence |
|---|---|
| Clear film erodes under atomic oxygen | Exposed clear PVF in low Earth orbit with no pigment or shieldErosion yield of 3.19e-24 cm3/atom on MISSE 2, about 30 times the yield of the white pigmented film |
Mitigations
- Add a white or pigmented titanium dioxide layer, which the NASA report measured at 1.01e-25 cm3/atom on MISSE 2
Supply and geography
How common the raw materials are and where they come from.
Fluorine feedstock (fluorspar, calcium fluoride)
- Top producers (2025)
- China 60%, Mexico 15%, Mongolia 15%, South Africa 4.1%
- Recycling
- USGS: synthetic fluorspar may be produced from neutralization of waste in uranium enrichment, petroleum alkylation and stainless-steel pickling, though undesirable impurities constrain its use.
- Substitutes
- USGS: fluosilicic acid from phosphate rock has been used as an alternative to fluorspar (about 73,000 tons of fluorspar equivalent was recovered in 2025).
PVF film producer
- Top producers (2026)
- United States
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: pvf-clear-tedlar
spore_version: 0.2
family: fluoropolymers
name: Polyvinyl fluoride (clear Tedlar)
abbreviation: PVF
role: weatherable fluoropolymer film with good atomic oxygen resistance
category: polymers
type: fluoropolymers
summary: |
Clear Tedlar is a biaxially oriented polyvinyl fluoride film from DuPont with no plasticizers. On the NASA MISSE 2 flight it eroded under atomic oxygen at 3.19e-24 cm3/atom, close to Kapton H at 3.00e-24 in the same table, and a white pigmented Tedlar eroded at only 1.01e-25 because its titanium dioxide shields the polymer. DuPont rates its continuous use range at -72 to 107 degC.
best_for: Weatherable, tough, flexible thin film for outdoor or decorative surfaces where a pigment can shield it from atomic oxygen
weakest_at: Clear film erodes under atomic oxygen about as fast as Kapton H (NASA MISSE 2), so it needs pigment or a shield in low Earth orbit
identity:
formula: (-CH2-CHF-)n
cas: 24981-14-4
source: wiki-pvf
where: Chembox at the top of the page (formula and CAS 24981-14-4); repeat unit given as (-CH2CHF-)n in the lead. Atoms per repeat unit (C2H3F) from NASA/TM-2008-215490 Table V.
tags:
environments:
- low-earth-orbit
stresses:
- atomic-oxygen
- uv
- vacuum-and-outgassing
applications:
- electronics-and-chips
- thermal-control
properties:
- benchmark: density
label: Density (clear PVF, MISSE 2 sample)
value: 1.3792
unit: g/cm3
scope: material
conditions:
form: clear Tedlar film used on MISSE 2
test_standard: density gradient column (ref. 12 in the NASA report)
method: Value printed in the NASA table of polymer densities
status: ground
source: banks2008
where: Table II (Density, PVF Clear Tedlar row)
- benchmark: density
label: Density range (Tedlar PVF film)
value: 1.37
value_high: 1.72
unit: g/cc
scope: material
conditions:
form: DuPont Tedlar PVF film, all types
test_standard: ASTM D-1505
method: Typical-value range printed in the DuPont general properties table
status: ground
source: tedlar-gp
where: Table 1 (General Properties), Density row
- benchmark: atomic_oxygen_erosion_yield
label: Atomic oxygen erosion yield, clear PVF (MISSE 2)
value: 3.19e-24
unit: cm3/atom
scope: material
conditions:
environment: low Earth orbit, ISS, MISSE 2 PEACE tray
fluence: 8.43e21 atoms/cm2 (from the NASA report text)
method: Measured on the MISSE 2 PEACE flight sample and reported in the NASA predictive-tool report
status: flight
source: banks2008
where: Table I (MISSE 2 PEACE polymers erosion yield data, PVF clear Tedlar row); section 2.2 gives the fluence
- benchmark: atomic_oxygen_erosion_yield
label: Atomic oxygen erosion yield, white pigmented PVF (MISSE 2)
value: 1.01e-25
unit: cm3/atom
scope: material
conditions:
environment: low Earth orbit, ISS, MISSE 2 PEACE tray
form: crystalline PVF with white (titanium dioxide) pigment
method: Measured on the MISSE 2 PEACE flight sample; the NASA report attributes the difference to pigment shielding
status: flight
source: banks2008
where: Table I (PVF white pigment row); section 2.2 text on pigment shielding
- benchmark: min_service_temp
label: Continuous use lower limit
value: -72
unit: degC
scope: material
conditions:
form: DuPont Tedlar PVF film
use: continuous use
method: Printed manufacturer temperature range (printed as -72 to 107 degC, -98 to 225 degF)
status: ground
source: tedlar-gp
where: Table 1 (General Properties), Temperature Range, Continuous Use row
- benchmark: max_service_temp
label: Continuous use upper limit
value: 107
unit: degC
scope: material
conditions:
form: DuPont Tedlar PVF film
use: continuous use
method: Printed manufacturer temperature range (printed as -72 to 107 degC, -98 to 225 degF)
status: ground
source: tedlar-gp
where: Table 1 (General Properties), Temperature Range, Continuous Use row
- benchmark: zero_strength_temperature
label: Zero strength temperature
value: 260
value_high: 300
unit: degC
scope: material
conditions:
test_method: hot bar
method: Range printed in the DuPont general properties table (printed as 260 to 300 degC, 500 to 570 degF)
status: ground
source: tedlar-gp
where: Table 1 (General Properties), Temperature Range, Zero Strength row
- benchmark: ultimate_tensile_strength
label: Ultimate tensile strength (ASTM D-882)
value: 8
value_high: 16
unit: kpsi
scope: material
conditions:
test_standard: ASTM D-882
temperature: 22 degC (72 degF)
method: Printed as 8 to 16 x 10^3 psi in the DuPont table; entered as kpsi with the same numbers
status: ground
source: tedlar-gp
where: Table 1 (General Properties), Ultimate Tensile Strength row
- benchmark: elongation
label: Ultimate elongation (ASTM D-882)
value: 90
value_high: 250
unit: '%'
scope: material
conditions:
test_standard: ASTM D-882
temperature: 22 degC (72 degF)
method: Typical range printed in the DuPont table
status: ground
source: tedlar-gp
where: Table 1 (General Properties), Ultimate Elongation row
- benchmark: moisture_absorption
label: Moisture absorption (upper limit)
value: 0.5
unit: '%'
scope: material
conditions:
test_method: water immersion
temperature: 22 degC (72 degF)
note: printed as less than 0.5 percent for most types
method: Upper bound printed in the DuPont table; not a typical value
status: ground
source: tedlar-gp
where: Table 1 (General Properties), Moisture Absorption row
- benchmark: refractive_index
label: Refractive index (nD)
value: 1.46
unit: nD
scope: material
conditions:
test_method: ASTM D-542 Abbe refractometer
temperature: 30 degC (86 degF)
method: Value printed in the DuPont table
status: ground
source: tedlar-gp
where: Table 1 (General Properties), Refractive Index row
- benchmark: cte
label: Linear coefficient of expansion
value: 0.000028
unit: in/in/degF
scope: material
conditions:
form: Tedlar PVF film
method: Value printed in the DuPont table as 2.8 x 10-5 in/in/degF
status: ground
source: tedlar-gp
where: Table 1 (General Properties), Thermal, Linear Coefficient of Expansion row
- benchmark: molar_mass
label: Molar mass of the repeat unit (C2H3F)
value: 46.0437
unit: g/mol
scope: material
conditions:
basis: repeat unit C2H3F
method: Value printed in the NASA table of atomic mass units per repeat unit
status: calculated
source: banks2008
where: Table IV (Atomic mass units, g/mole, PVF clear row)
checked_values: 13
corrosion:
- environment: Atomic oxygen in low Earth orbit
headline: Clear PVF eroded at about the same rate as Kapton H on the ISS, but pigmented PVF eroded about 30 times more slowly.
effect: MISSE 2 erosion yield was 3.19e-24 cm3/atom for clear PVF, against 3.00e-24 for Kapton H, and 1.01e-25 for white pigmented PVF. The NASA report says titanium dioxide pigment shields the film.
rating: moderate
conditions:
flight: MISSE 2, fluence 8.43e21 atoms/cm2
source: banks2008
where: Table I; section 2.2
- environment: Sunlight and weathering
headline: DuPont rates Tedlar as having excellent weathering resistance.
effect: The DuPont table lists weatherability as excellent for Florida exposure facing south at 45 degrees. The brochure says outdoor weathering tests on pigmented films have run for more than 20 years. A 2025 Frontiers review attributes the aging resistance of Tedlar composite films to inorganic fillers that block light.
rating: severe
conditions:
exposure: Florida, facing south at 45 degrees to horizontal
source: tedlar-gp
where: Table 1, Weatherability row; Summary of Properties text
- environment: Heat ageing
headline: Tedlar has no plasticizers, so it keeps its properties on heat ageing.
effect: DuPont lists an aging test of 3000 hours in a circulating air oven at 150 degC for Tedlar, without a retained-property figure. The sheet says the lack of plasticizer gives good aging properties.
rating: severe
conditions:
test: 3000 hr circulating air oven at 150 degC
source: tedlar-gp
where: Table 1, Aging row; Summary of Properties text
- environment: Chemical exposure
headline: PVF shows no visible effect after one year of immersion in acids, bases and solvents at 25 degC.
effect: DuPont reports no visible effect after 1 year immersion at 25 degC and after 2 hours at boiling for acids, bases and solvents, and says strength and appearance were not affected by 5 years soil burial.
rating: severe
conditions:
test: 1 yr immersion at 25 degC; 2 hr at boiling
source: tedlar-gp
where: Table 1, Chemical Resistance rows
risks:
hazards: []
failure_risks:
- mode: Clear film erodes under atomic oxygen
trigger: Exposed clear PVF in low Earth orbit with no pigment or shield
consequence: Erosion yield of 3.19e-24 cm3/atom on MISSE 2, about 30 times the yield of the white pigmented film
source: banks2008
where: Table I; section 2.2
side_effects: []
handling: []
mitigations:
- text: Add a white or pigmented titanium dioxide layer, which the NASA report measured at 1.01e-25 cm3/atom on MISSE 2
source: banks2008
where: Table I; section 2.2
gaps_text: No manufacturer hazard sheet, PubChem record or GHS classification for PVF was read in this run.
uses:
- application: electronics-and-chips
device: Printed circuit board and composite part release sheet (Tedlar S surface)
example: DuPont says the S surface has excellent anti-stick properties and is especially suited as a release sheet for printed circuit board and composite part fabrication.
source: tedlar-brochure
where: Summary text, paragraph on the S surface
- application: thermal-control
device: Clear PVF film on the MISSE 2 PEACE tray exposed outside the ISS airlock
example: Clear PVF was one of the polymers flown on MISSE 2 to measure atomic oxygen erosion in low Earth orbit (2001 to 2005).
source: banks2008
where: Table I (flight data for the MISSE 2 PEACE polymers)
supply:
- subject: Fluorine feedstock (fluorspar, calcium fluoride)
producers:
- country: China
share_percent: 60
year: 2025
- country: Mexico
share_percent: 15
year: 2025
- country: Mongolia
share_percent: 15
year: 2025
- country: South Africa
share_percent: 4.1
year: 2025
recycling: 'USGS: synthetic fluorspar may be produced from neutralization of waste in uranium enrichment, petroleum alkylation and stainless-steel pickling, though undesirable impurities constrain its use.'
substitutes:
- 'USGS: fluosilicic acid from phosphate rock has been used as an alternative to fluorspar (about 73,000 tons of fluorspar equivalent was recovered in 2025).'
source: usgs-mcs2026-fluorspar
where: World Mine Production and Reserves table, 2025; Recycling and Substitutes sections. Shares are calculated by Space Mushroom against the printed world total of 10,000 thousand t, so they are approximate.
- subject: PVF film producer
producers:
- country: United States
year: 2026
source: tedlar-brochure
where: Title and product name (DuPont Tedlar PVF films); the brochure gives no production share
gaps:
- 'Not entered: a melting point from a primary source. Wikipedia gives 185 to 210 degC but is limited to history and composition in this profile.'
- 'Not entered: the NASA erosion-prediction value 1.38e-24 cm3/atom (Table VII), because its benchmark is a model prediction and no canonical name fits.'
- 'No hazard data: the ChemicalBook PVF safety sheet has no GHS data, and PubChem (CID search page) was blocked by a captcha in this run, so hazards and GHS codes are left empty.'
- No handling guidance from a manufacturer safety sheet was read in this run.
- The MISSE-S post-flight report (De Groh, NTRS 20070031938) mentions Tedlar specimens on the anti-solar side with low UV exposure, but its tables are OCR text and no Tedlar number was legible, so none is entered.
- The Frontiers 2025 review was read for qualitative aging claims only; it gives no PVF number.
- No PVF radiation dose, thermal-cycling or outgassing value from a fetched page was found; the passport's 3.95-year duration and -30 to 40 degC range were not re-read, so they are not entered.
- The DuPont table's dielectric and volume resistivity columns are split across grades, so none is entered.
- Erosion yield is entered under the snake_case name atomic_oxygen_erosion_yield because no canonical name exists in property-canon.yaml.
- zero_strength_temperature is a snake_case name not in property-canon.yaml.
- 'Atomic weights: NIST gives C as [12.0096, 12.0116] and H as [1.00784, 1.00811]; the parts list uses the lower bound of each interval.'
sources:
banks2008:
title: Atomic Oxygen Erosion Yield Predictive Tool for Spacecraft Polymers in Low Earth Orbit
id: NASA/TM-2008-215490, NTRS 20090011780
url: https://ntrs.nasa.gov/citations/20090011780
year: 2008
kind: report
license: public domain (NASA)
usgs-mcs2026-fluorspar:
title: 'Mineral Commodity Summaries 2026: Fluorspar (USGS)'
id: USGS MCS 2026, February 2026
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-fluorspar.pdf
year: 2026
kind: report
license: public domain (USGS)
tedlar-gp:
title: 'DuPont Tedlar PVF Films: General Properties'
id: DuPont Tedlar General Properties (mirror at polymerfilms.com, uploaded 2023)
url: https://polymerfilms.com/wp-content/uploads/2023/07/DuPont_Tedlar-General-Properties.pdf
year: 2023
kind: datasheet
license: manufacturer datasheet
tedlar-brochure:
title: DuPont Tedlar Polyvinyl Fluoride (PVF) Films brochure
id: DuPont Tedlar PVF brochure 3 (mirror at metalcoffeeshop.com)
url: https://www.metalcoffeeshop.com/uploads/media/2022/01/dupont-tedlar-polyvinyl-fluoride-pvf-films-brochure-3.pdf
kind: datasheet
license: manufacturer brochure
nasa-misse-s-de-groh:
title: Post-Flight Analysis of Selected Fluorocarbon and Other Thin Film Polymer Specimens flown on MISSE-S (De Groh et al.)
id: NTRS 20070031938
url: https://ntrs.nasa.gov/api/citations/20070031938/downloads/20070031938.pdf
year: 2007
kind: report
license: public domain (NASA)
frontiers2025:
title: Frontiers in Materials 2025 article on Tedlar PVF composite films (doi 10.3389/fmats.2025.1531950)
id: doi 10.3389/fmats.2025.1531950
url: https://www.frontiersin.org/journals/materials/articles/10.3389/fmats.2025.1531950/pdf
year: 2025
kind: paper
license: open access
nist-atomic-weights:
title: Atomic Weights and Isotopic Compositions (NIST)
id: NIST Physical Measurement Laboratory, carbon, hydrogen and fluorine tables
url: https://physics.nist.gov/cgi-bin/Compositions/stand_alone.pl
kind: database
license: public domain (NIST)
wiki-pvf:
title: Polyvinyl fluoride (Wikipedia)
id: CAS 24981-14-4; history and composition only
url: https://en.wikipedia.org/wiki/Polyvinyl_fluoride
kind: web
license: CC BY-SA 4.0
story:
recipe:
line: PVF is made by polymerizing vinyl fluoride, C2H3F, usually by suspension or emulsion polymerization in water with peroxide or azo initiators (Wikipedia). The polymer is then dissolved, mixed with additives, cast or extruded, and biaxially oriented into thin film (Wikipedia, DuPont). Its repeat unit is C2H3F, with two carbons, three hydrogens and one fluorine (NASA Table V).
parts:
- name: Carbon
symbol: C
atoms: 2
atomic_weight: 12.0096
role: The two backbone carbons of each repeat unit.
- name: Hydrogen
symbol: H
atoms: 3
atomic_weight: 1.00784
role: Three hydrogens on the backbone carbons.
- name: Fluorine
symbol: F
atoms: 1
atomic_weight: 18.998403163
role: One fluorine on the backbone, which makes the polymer a fluoropolymer.
risk_groups:
- title: For people
level: 1
verdict: No hazard sheet was read; treat as a plastic film
lead: No manufacturer safety data sheet or GHS classification for PVF was read in this run, so no hazard is stated for people.
points:
- label: Not checked
line: The ChemicalBook PVF safety sheet has no hazard data, and PubChem was blocked in this run.
why: Polyvinyl fluoride is a tough, flexible fluoropolymer film. Clear Tedlar eroded under atomic oxygen on MISSE 2 at about the rate of Kapton H, but its white pigmented form eroded about 30 times more slowly.
uses:
- where: Printed circuit board fabrication
line: DuPont says the S surface of Tedlar is especially suited as a release sheet for printed circuit board and composite part fabrication.
- where: MISSE 2 flight test
line: Clear PVF was flown outside the ISS airlock on MISSE 2 from 2001 to 2005 to measure atomic oxygen erosion.
can_do:
- label: Atomic oxygen
value: 3.19e-24 cm3/atom (clear)
line: Clear PVF eroded at 3.19 × 10⁻²⁴ cm³/atom on MISSE 2, close to Kapton H at 3.00 × 10⁻²⁴ in the same table.
- label: Pigmented atomic oxygen
value: 1.01e-25 cm3/atom (white)
line: White pigmented PVF eroded at 1.01 × 10⁻²⁵ cm³/atom, because titanium dioxide shields the polymer.
- label: Continuous use
value: '-72 to 107 degC'
line: DuPont rates continuous use from -72 to 107 degC.
compare: On the MISSE 2 flight, clear PVF eroded at 3.19 × 10⁻²⁴ cm³/atom, against 3.00 × 10⁻²⁴ for Kapton H in the same NASA table, while white pigmented PVF eroded at only 1.01 × 10⁻²⁵. Its tensile strength and elongation are modest, with DuPont giving 8 to 16 kpsi and 90 to 250 percent elongation.
handling:
- No manufacturer hazard or handling sheet was read in this run, so handling guidance is not given here.
- Pigmented film is the better choice where atomic oxygen is expected, since the clear film eroded about 30 times faster.
good_for:
- Weatherable, tough flexible film for outdoor or decorative surfaces (DuPont).
- Release sheet for printed circuit board and composite part fabrication (DuPont).
- Pigmented films where atomic oxygen resistance matters, such as the white Tedlar on MISSE 2 (NASA).
watch_out:
- Atomic oxygen. The clear film eroded at 3.19 × 10⁻²⁴ cm³/atom on MISSE 2, so it needs a pigment or a shield in low Earth orbit.
- Temperature. DuPont rates continuous use to 107 degC and zero strength at 260 to 300 degC.
- Gaps in the record. No hazard sheet, PubChem record, melting point or radiation value was read in this run.
verdict: Clear Tedlar is a weatherable, flexible fluoropolymer film with good aging and chemical resistance, but on the MISSE 2 flight it eroded in low Earth orbit about as fast as Kapton H. Pigmented PVF is much more durable under atomic oxygen, so the pigment is the key choice for space use.
compare_rows:
- label: Atomic oxygen erosion yield (MISSE 2)
benchmark: atomic_oxygen_erosion_yield
scope: material
- label: Continuous use upper limit
benchmark: max_service_temp
scope: material
- label: Density
benchmark: density
scope: material
license: CC-BY-4.0
updated: 2026-10-20T00:00:00.000Z
review:
status: draft
method: assistant
checked_values: 13
unreachable: 1
caveats: 3
note: Written by an AI assistant on 2026-10-20. Values were read from NASA TM-2008-215490 (text extracted with pdftotext), the DuPont Tedlar general properties table and brochure, and NIST pages fetched in this run. PubChem was blocked by a captcha. Wikipedia was used for composition and history only.
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 |
|---|---|---|---|---|
| Atomic Oxygen Erosion Yield Predictive Tool for Spacecraft Polymers in Low Earth Orbit | report | 2008 | 8 values | |
| Mineral Commodity Summaries 2026: Fluorspar (USGS) | report | 2026 | 1 value | |
| DuPont Tedlar PVF Films: General Properties | datasheet | 2023 | 12 values | |
| DuPont Tedlar Polyvinyl Fluoride (PVF) Films brochure | datasheet | 2 values | ||
| Post-Flight Analysis of Selected Fluorocarbon and Other Thin Film Polymer Specimens flown on MISSE-S (De Groh et al.) | report | 2007 | 0 values | |
| Frontiers in Materials 2025 article on Tedlar PVF composite films (doi 10.3389/fmats.2025.1531950) | paper | 2025 | 0 values | |
| Atomic Weights and Isotopic Compositions (NIST) | database | 0 values | ||
| Polyvinyl fluoride (Wikipedia) | web | 1 value |