Electrically powered ion acceleratot with contact ionixation for perspertive electrically powered thrusters

Electrically powered ion acceleratot with contact ionixation for perspertive electrically powered thrusters

A number of characteristics of ionic and ion-plasma accelerators laboratory samples designed for electrically powered spacecraft propulsion were investigated in the experimental research. In a large-sized vacuum chamber (2.4 m^3, 10^-3 Pa) in the MCA named after A.F. Mozhaysky provided the necessary...

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Bibliographic Details
Main Authors: Tsybin Oleg, Makarov Sergey, Dyubo Dmitry, Kuleshov Yuri, Goncharov Pavel, Martynov Viktor, Shunevich Nikolay
Format: Article
Language:English
Published: Peter the Great St.Petersburg Polytechnic University 2020-06-01
Series:St. Petersburg Polytechnical University Journal: Physics and Mathematics
Subjects:
vacuum chamber
experimental studies
computer simulation
ionization
ion beam
ion accelerator
electrically powered spacecraft propulsion
Online Access:https://physmath.spbstu.ru/article/2020.48.08/

Internet

https://physmath.spbstu.ru/article/2020.48.08/

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