Publication: Electrodynamic Plasma Thruster with Capillary-Porous Electrode
Дата
2021
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© 2021, Pleiades Publishing, Ltd.Abstract: A scheme of a spacecraft thruster based on a stationary electrodynamic plasma accelerator with capillary-porous electrodes is proposed. Such electrodes are renewable and nondegradable, and the service life is limited by the supply of filler metal. High-efficiency regimes of the capillary-porous electrodes are determined. In such regimes, the accelerator can give a thrust of greater than 10 N and a specific impulse of several tens of kilometers per second. Li, Sn, and Ga with porous molybdenum or tungsten mats can be used as filler metal for capillary-porous electrodes.
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Nagel', M. Y. Electrodynamic Plasma Thruster with Capillary-Porous Electrode / Nagel', M.Y., Martynenko, Y.V. // Technical Physics. - 2021. - 10.1134/S1063784221090115
URI
https://www.doi.org/10.1134/S1063784221090115
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https://openrepository.mephi.ru/handle/123456789/25257
https://www.scopus.com/record/display.uri?eid=2-s2.0-85124771225&origin=resultslist
http://gateway.webofknowledge.com/gateway/Gateway.cgi?GWVersion=2&SrcAuth=Alerting&SrcApp=Alerting&DestApp=WOS_CPL&DestLinkType=FullRecord&UT=WOS:000754145000031
https://openrepository.mephi.ru/handle/123456789/25257