Электронный архив

THRUST AND THRUST-TO-POWER RATIO IN ELECTROHYDRODYNAMIC PROPULSION ELECTRODE SYSTEMS

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dc.contributor Казанский (Приволжский) федеральный университет
dc.contributor.author Dremin D.V. ru_RU
dc.contributor.author Khomich Yu.V. ru_RU
dc.contributor.author Rebrov I.E. ru_RU
dc.date.accessioned 2018-01-10T12:32:13Z
dc.date.available 2018-01-10T12:32:13Z
dc.date.issued 2017
dc.identifier.uri http://dspace.kpfu.ru/xmlui/handle/net/117412
dc.description.abstract Abstract: Dependences for the efficiency of ionocraft electrode system and the magnitude of the thrust were obtained for different polarity of the corona. The most effective mode of work lifters of the considered structures is achieved at low current. The increase of distance between the corona electrode and the collector gives the growth of thrust and thrust-to-power ratio up to some distance. In the subsequent distancing statistically significant increase of characteristics is not observed. It is advisable to use emitters with smaller diameter to reduce losses to the formation of the corona. ru_RU
dc.relation.ispartofseries "ФИЗИКА НИЗКОТЕМПЕРАТУРНОЙ ПЛАЗМЫ" ФНТП-2017 ru_RU
dc.subject - ru_RU
dc.title THRUST AND THRUST-TO-POWER RATIO IN ELECTROHYDRODYNAMIC PROPULSION ELECTRODE SYSTEMS ru_RU
dc.type article
dc.identifier.udk -
dc.description.pages 241-241


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