41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference &Amp;amp; Exhibit 2005
DOI: 10.2514/6.2005-4411
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Manufacturing of 57cm Carbon-Carbon Composite Ion Optics for 20-kW-Class Ion Engine

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Cited by 7 publications
(3 citation statements)
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“…Then another densification by CVI is applied to fill in the undesired voids created during the aperture generation. Finally, a high-temperature low-pressure vacuum bake-out in autoclave takes place (Beatty et al , 2005).…”
Section: Methodsmentioning
confidence: 99%
“…Then another densification by CVI is applied to fill in the undesired voids created during the aperture generation. Finally, a high-temperature low-pressure vacuum bake-out in autoclave takes place (Beatty et al , 2005).…”
Section: Methodsmentioning
confidence: 99%
“…The weight loss is affected more by the curing and post-curing temperature than by the time period. During the curing stages, gas and volatiles must be continuously removed from the mould, otherwise they become trapped to form pores or voids, which could expand during further processing [135]. The process of curing (at 80 C-150 C) and post-curing (at 160 C-300 C) increases the carbon yield and density of the material and decreases its shrinkage, after carbonization [134].…”
Section: Curingmentioning
confidence: 99%
“…Typically, electric thrusters have incorporated innovations related to materials and fabrication processes to their components. For instance, the development of carbon-based composite materials [7] boosted intense research that led to the development of carbon-carbon ion optics [8][9][10], which nowadays are one of the options for the extraction systems of ion thrusters [11,12].However, very few works containing innovative fabrication approaches of electric propulsion components or focused on the application of new production technologies, such as additive manufacturing, have appeared recently.…”
Section: Introductionmentioning
confidence: 99%