2016
DOI: 10.1016/j.actaastro.2015.11.031
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The effects of low earth orbit atomic oxygen on the properties of Polytetrafluoroethylene

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Cited by 22 publications
(7 citation statements)
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“…Diamond-like carbon (DLC) thin films have been extensively studied for this purpose, due to their appropriate tribological characteristics, such as a stable and low wear rate 8 . However, the use of DLC films for these aerospace applications faces a technical barrier, since they are severely etched by atomic oxygen present in the low orbit atmosphere (200 to 700 km), resulting in a significant lifetime reduction [9][10][11] . Methods to increase the lifetime of the DLC film include incorporation of dielectric and metallic nanoparticles 12,13 .…”
Section: Introductionmentioning
confidence: 99%
“…Diamond-like carbon (DLC) thin films have been extensively studied for this purpose, due to their appropriate tribological characteristics, such as a stable and low wear rate 8 . However, the use of DLC films for these aerospace applications faces a technical barrier, since they are severely etched by atomic oxygen present in the low orbit atmosphere (200 to 700 km), resulting in a significant lifetime reduction [9][10][11] . Methods to increase the lifetime of the DLC film include incorporation of dielectric and metallic nanoparticles 12,13 .…”
Section: Introductionmentioning
confidence: 99%
“…[5][6][7] Although the AO density is very low in LEO, high incident fluxes of 5-eV oxygen atoms can be generated due to the orbital velocity 8 km/s. The attack of AO on spacecraft surfaces with such high kinetic energies can initiate numerous chemical and physical events, [8][9][10] which is one of the most critical factors that cause space materials degradation. Therefore, it is of paramount importance to evaluate AO effects on space materials.…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, it is crucial to investigate the LEO environmental AO effects of materials to find the proper materials for long lifetime spacecrafts. Many related researches had been carried out, and some experiments have been conducted using ground-based AO simulation equipment or in-flight tests (Banks et al, 2004; Hooshangi et al, 2016; Lv et al, 2015; Minton et al, 2012; Srinivasan and Banks, 1990; Zhao et al, 2015). Banks et al (2004) investigated some samples exposed in LEO environment, and the results indicated that the polymers commonly used in spacecraft usually exhibit a serious AO oxidization.…”
Section: Introductionmentioning
confidence: 99%
“…Minton et al incorporated polyhedral oligomeric silsesquioxane (POSS) into the polyimide matrix to prevent the AO erosion, they did laboratory and space-flight experiments, and the results showed that the POSS polyimides are highly resistant to AO attack, with erosion yields that may be as little as 1% those of Kapton directly exposed to AO (Minton et al, 2012). Additionally, Hooshangi et al studied the effects of AO on the properties of polytetrafluoroethylene films; they characterized the appearance, mass, thermal, and mechanical properties of the films (Hooshangi et al, 2016).…”
Section: Introductionmentioning
confidence: 99%