Electric Propulsion Thrusters: Laboratory Investigation of Jets by Probe Methods
- 作者: Kozhevnikov V.1, Nadiradze A.1, Nazarenko I.1, Frolova Y.1, Khartov S.1
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隶属关系:
- Moscow Aviation Institute (National Research University)
- 期: 卷 61, 编号 4 (2018)
- 页面: 677-681
- 栏目: 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
如何引用文章
详细
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.
作者简介
V. Kozhevnikov
Moscow Aviation Institute (National Research University)
Email: nadiradze@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
A. Nadiradze
Moscow Aviation Institute (National Research University)
编辑信件的主要联系方式.
Email: nadiradze@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
I. Nazarenko
Moscow Aviation Institute (National Research University)
Email: nadiradze@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
Yu. Frolova
Moscow Aviation Institute (National Research University)
Email: nadiradze@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
S. Khartov
Moscow Aviation Institute (National Research University)
Email: nadiradze@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993