Thrust and thrust-to-power ratio in electrohydrodynamic propulsion electrode systems

The influence on thrust parameter and efficiency from geometric parameters and design features of the ionocraft electrode is considered, dependences were obtained. The most effective mode of work lifters of the considered structures is achieved at low current. The increase of distance between the co...

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Published inJournal of physics. Conference series Vol. 927; no. 1; pp. 12015 - 12019
Main Authors Dremin, D V, Khomich, V Yu, Rebrov, I E
Format Journal Article
LanguageEnglish
Published Bristol IOP Publishing 01.11.2017
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Abstract The influence on thrust parameter and efficiency from geometric parameters and design features of the ionocraft electrode is considered, dependences were obtained. 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. It is advisable to use emitters with smaller diameter to reduce losses to the formation of the corona.
AbstractList The influence on thrust parameter and efficiency from geometric parameters and design features of the ionocraft electrode is considered, dependences were obtained. 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. It is advisable to use emitters with smaller diameter to reduce losses to the formation of the corona.
Author Dremin, D V
Rebrov, I E
Khomich, V Yu
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  givenname: V Yu
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  fullname: Khomich, V Yu
  organization: Institute for Electrophysics and Electric Power RAS , Russia
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  givenname: I E
  surname: Rebrov
  fullname: Rebrov, I E
  email: rbrv.igor@gmail.com
  organization: Institute for Electrophysics and Electric Power RAS , Russia
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Cites_doi 10.1023/A:1022470901385
10.1070/QE2011v041n12ABEH014686
10.1002/9781118547519
10.1615/TsAGISciJ.v42.i2.70
10.5772/1990
10.1080/09398368.2013.11463867
10.1063/1.2776164
ContentType Journal Article
Copyright Published under licence by IOP Publishing Ltd
2017. This work is published under http://creativecommons.org/licenses/by/3.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.
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StartPage 12015
SubjectTerms Design parameters
Electrodes
Electrohydrodynamics
Emitters
Low currents
Physics
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Title Thrust and thrust-to-power ratio in electrohydrodynamic propulsion electrode systems
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