Materials/Polymers/Engineering polymers
Polyimides
polyimidesAbout polyimides
Polyimides (Kapton, Upilex, PMR-15, CP1): temperature range, radiation tolerance and electrical data with sources.
Polyimides are among the most heat-resistant polymers and are used as flexible circuit film, wire insulation and spacecraft thermal blankets. Film, resin and composite forms behave differently, so each value names its form.
At a glance
- Highest density: Upilex-S polyimide film (BPDA) reaches 1.47 g/cm³. Lowest: High temperature polyimide resin (PMR-15) starts at 1.29 g/cm³. (5 of 5 grades have a sourced value.)
Ranges run across the conditions each source reports (temper, heat treatment, form), measured at room temperature where the source says so.
How they compare
The same measurements for every material in the collection. A range means the grade has values under several conditions; "at least" means the source gives a specified minimum. "no data" means no sourced value yet. For ranked tables, open a benchmark.
| Material | Density | Tensile strength | Young's modulus | Glass transition | Heat deflection temperature | Maximum service temperature |
|---|---|---|---|---|---|---|
| Colorless polyimide CP1 filmflexible, optically clear polyimide film for thin-film space structures | 1.42 g/cm³ | no data | no data | no data | no data | no data |
| Kapton H polyimide filmflexible insulating film, the original general-purpose grade | 1.43 g/cm³ | no data | no data | no data | no data | 400 °C |
| Kapton HN polyimide filmflexible insulating film | 1.42 to 1.43 g/cm³ | no data | no data | no data | no data | 400 °C |
| High temperature polyimide resin (PMR-15)high-temperature structural matrix resin for composites | 1.29 to 1.32 g/cm³ | no data | no data | 332 to 362 °C | no data | 316 °C |
| Upilex-S polyimide film (BPDA)flexible insulating film | 1.39 to 1.47 g/cm³ | 520 MPa | 9.1 GPa | no data | no data | no data |
What these materials are made of
Composition by weight, as printed in the sources for each grade (the first constituents listed).
| Material | Main constituents |
|---|---|
| Upilex-S polyimide film (BPDA) | C 72.1% · H 2.8% · O 17.5% · N 7.6% |
Where they are used
| Use | Grades |
|---|---|
| Solar sail made of 2 micrometre CP1 film with vapour-deposited aluminum | Colorless polyimide CP1 film |
| Thin-film sunshade for a deployable space telescope | Colorless polyimide CP1 film |
| Multilayer insulation blankets on a spacecraft | Kapton H polyimide film |
| Flexible printed circuits and flexible electronics | Kapton H polyimide film |
| Aluminized Kapton multilayer insulation (MLI) blankets | Kapton HN polyimide film |
| Double-aluminized Kapton sunshield sheets | Kapton HN polyimide film |
| General-purpose film for electrical insulation and electronic parts | Kapton HN polyimide film |
| QCSEE inner cowl for an experimental turbofan engine | High temperature polyimide resin (PMR-15) |
| Oil tank bracket and augmentor duct for F100 engines | High temperature polyimide resin (PMR-15) |
| Shuttle orbiter aft body flap | High temperature polyimide resin (PMR-15) |
| Flexible printed circuit and TAB-tape substrates | Upilex-S polyimide film (BPDA) |
| Carrier base and release film for high-temperature processing | Upilex-S polyimide film (BPDA) |
| Electrical insulation in high-temperature circuits | Upilex-S polyimide film (BPDA) |
When each grade fits
| Material | Best for | Weakest at |
|---|---|---|
| Colorless polyimide CP1 film | Thin, clear, flexible film for solar sails and sunshades where the film stays uncoated in orbit only for short times | Optical darkening under UV and particle radiation (solar absorptance rose more than 0.3 in simulation), and atomic-oxygen erosion of exposed film |
| Kapton H polyimide film | A thin, flexible polyimide film for insulation and multilayer blankets where the film is covered or coated against atomic oxygen | Atomic-oxygen erosion in low Earth orbit. The MISSE 2 flight value is 3.00e-24 cm3/atom, so bare outer film is eaten away. |
| Kapton HN polyimide film | A thin, flexible, electrically insulating film that works from cryogenic to about 400 degC and passes the usual outgassing screen | Atomic-oxygen erosion in low Earth orbit (the outer film is eaten away unless it is covered or coated), and slow darkening under space radiation |
| High temperature polyimide resin (PMR-15) | Structural composite parts that must hold strength at about 290 to 316 degC, such as engine ducts, cowls and fan blades | Atomic-oxygen erosion in low Earth orbit (the MISSE 2 sample eroded through), and weight loss from thermo-oxidation at 316 degC; the MDA monomer is a carcinogen concern during manufacture |
| Upilex-S polyimide film (BPDA) | A thin, flexible, electrically insulating film with a very low coefficient of thermal expansion and no melting point, where dimensional stability over temperature matters more than atomic-oxygen resistance | Atomic-oxygen erosion in low Earth orbit (MISSE 2 erosion yield 9.22e-24 cm3/atom, the highest of the polyimides in the NASA table), so exposed film must be covered or coated |