Electric Propulsion Thrusters: Laboratory Investigation of Jets by Probe Methods
- Autores: Kozhevnikov V.V.1, Nadiradze A.B.1, Nazarenko I.P.1, Frolova Y.L.1, Khartov S.A.1
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Afiliações:
- Moscow Aviation Institute (National Research University)
- Edição: Volume 61, Nº 4 (2018)
- Páginas: 677-681
- Seção: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journals.rcsi.science/1068-7998/article/view/230778
- DOI: https://doi.org/10.3103/S106879981804027X
- ID: 230778
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Resumo
Features of probe measurements of plasma jet parameters of the electric propulsion thrusters under laboratory conditions are studied. Effect of the pressure of the residual gas in the vacuum chamber onto plasma jet formation and spread are investigated.
Sobre autores
V. Kozhevnikov
Moscow Aviation Institute (National Research University)
Email: nadiradze@mai.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
A. Nadiradze
Moscow Aviation Institute (National Research University)
Autor responsável pela correspondência
Email: nadiradze@mai.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
I. Nazarenko
Moscow Aviation Institute (National Research University)
Email: nadiradze@mai.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
Yu. Frolova
Moscow Aviation Institute (National Research University)
Email: nadiradze@mai.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
S. Khartov
Moscow Aviation Institute (National Research University)
Email: nadiradze@mai.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
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