Electric Propulsion Thrusters: Laboratory Investigation of Jets by Probe Methods


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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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