Electric Propulsion Thrusters: Laboratory Investigation of Jets by Probe Methods
- Авторы: Kozhevnikov V.1, Nadiradze A.1, Nazarenko I.1, Frolova Y.1, Khartov S.1
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Учреждения:
- Moscow Aviation Institute (National Research University)
- Выпуск: Том 61, № 4 (2018)
- Страницы: 677-681
- Раздел: 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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Аннотация
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.
Об авторах
V. Kozhevnikov
Moscow Aviation Institute (National Research University)
Email: nadiradze@mai.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
A. Nadiradze
Moscow Aviation Institute (National Research University)
Автор, ответственный за переписку.
Email: nadiradze@mai.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
I. Nazarenko
Moscow Aviation Institute (National Research University)
Email: nadiradze@mai.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
Yu. Frolova
Moscow Aviation Institute (National Research University)
Email: nadiradze@mai.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
S. Khartov
Moscow Aviation Institute (National Research University)
Email: nadiradze@mai.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993