Electric Propulsion Thrusters: Laboratory Investigation of Jets by Probe Methods

V. V. Kozhevnikov; A. B. Nadiradze; I. P. Nazarenko; Yu. L. Frolova; S. A. Khartov

doi:10.3103/S106879981804027X

Electric Propulsion Thrusters: Laboratory Investigation of Jets by Probe Methods

Authors: Kozhevnikov V.V.¹, Nadiradze A.B.¹, Nazarenko I.P.¹, Frolova Y.L.¹, Khartov S.A.¹
Affiliations:
1. Moscow Aviation Institute (National Research University)
Issue: Vol 61, No 4 (2018)
Pages: 677-681
Section: 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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Abstract

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.