2006
DOI: 10.2514/1.16402
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Erosion of Kapton H® by Hyperthermal Atomic Oxygen

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Cited by 67 publications
(93 citation statements)
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“…A detailed description of the sample mount can be found in an earlier paper (26). Nine samples can be exposed simultaneously.…”
Section: Articlementioning
confidence: 99%
See 1 more Smart Citation
“…A detailed description of the sample mount can be found in an earlier paper (26). Nine samples can be exposed simultaneously.…”
Section: Articlementioning
confidence: 99%
“…The exposure experiment was conducted in the source region of a molecular beam apparatus (26)(27)(28)(29)(30) (32), and that the O 2 molecules in the beam are in their O 2 ( 3 Σ g -) ground state (33). These results establish that the exposure environment used in our laboratory subjects materials to groundstate O and O 2 .…”
Section: Exposures and Erosion-depth Measurementsmentioning
confidence: 99%
“…The difference in etch depth between the eroded and stainless steel screen-protected areas of the samples, made it possible to calculate an AO reaction efficiency (R e ) or erosion yield of the material for a given AO flux. [29] The AO reaction efficiency of the Kapton H ® reference sample was used to calculate the Kapton ® equivalent fluence and erosion yields of each sample exposure. [29] For various exposures, the step heights (or etch depths) of POSS-PI films were plotted as a function of the step height of the Kapton H ® film.…”
Section: Resultsmentioning
confidence: 99%
“…[29] The AO reaction efficiency of the Kapton H ® reference sample was used to calculate the Kapton ® equivalent fluence and erosion yields of each sample exposure. [29] For various exposures, the step heights (or etch depths) of POSS-PI films were plotted as a function of the step height of the Kapton H ® film. [23] The derivative functions indicated that the 3.5 and 7.0 wt % Si 8 This paper is declared a work of the U.S. Government and is not subject to copyright protection in the United States and increased in depth to 1.4 µm after the second exposure.…”
Section: Resultsmentioning
confidence: 99%
“…In this respect, satellites operating in low earth orbits are most vulnerable to optical degradation effects [4]. Efforts can be taken to mitigate degradation effects for commonly used spacecraft materials such as Kapton or MLI, which show severe degradation for long-time space exposure [5][6][7]. However, different materials are affected in different ways by exposure to the space environment and the magnitude of the effect depends on mission and spacecraft specific parameters.…”
Section: Introductionmentioning
confidence: 99%