A low-current LaB6 open-end knife-edge emitter hollow cathode for Hall thrusters

Author(s):  
George-Cristian Potrivitu ◽  
Luxiang Xu ◽  
Shuyan Xu
2008 ◽  
Vol 24 (1) ◽  
pp. 142-146 ◽  
Author(s):  
Jason M. Makela ◽  
Dean R. Massey ◽  
Lyon B. King

Aerospace ◽  
2020 ◽  
Vol 7 (7) ◽  
pp. 96
Author(s):  
Daniela Pedrini ◽  
Cosimo Ducci ◽  
Ugo Cesari ◽  
Tommaso Misuri ◽  
Mariano Andrenucci

SITAEL is active in the field of electric propulsion and is involved in the development of different thruster technologies—mainly Hall thrusters (HTs)—of power levels ranging from 100 W up to 20 kW. Low-power HTs are the most effective choice to perform orbit transfer, drag compensation, and de-orbiting maneuvers for small satellites. This paper is dedicated to the activities regarding HC1, the hollow cathode conceived for the 100-W-class Hall thruster under development at SITAEL. Successful test campaigns were performed and are described, with emphasis on the improvements in the cathode design after an extensive research and development phase. The results are presented and discussed, along with future developments of the ongoing activities.


2016 ◽  
Vol 32 (6) ◽  
pp. 1557-1561 ◽  
Author(s):  
Daniela Pedrini ◽  
Riccardo Albertoni ◽  
Fabrizio Paganucci ◽  
Mariano Andrenucci

1979 ◽  
Vol 40 (C7) ◽  
pp. C7-229-C7-230
Author(s):  
N. N. Rykalin ◽  
A. V. Nikolaev ◽  
A. P. Borzhov

1983 ◽  
Vol 44 (C7) ◽  
pp. C7-479-C7-487 ◽  
Author(s):  
M. Broglia ◽  
F. Catoni ◽  
P. Zampetti

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