Modeling the Effects of Discharge Voltage on Hall Thruster Performance

Author(s):  
Aysegul Yilmaz
2011 ◽  
Vol 18 (6) ◽  
pp. 064501 ◽  
Author(s):  
S. Mazouffre ◽  
K. Dannenmayer ◽  
C. Blank

Author(s):  
И.А. Хмелевской ◽  
Д.А. Томилин

Two stable operating modes, which were called “jet” and “bell” mode, were investigated for Hall thruster with power 1.5 kW. Performances (thrust, thrust specific impulse) in two modes were investigated. The study were conducted for discharge voltage 300-800 V and gas flow rate from 1.5 to 3.0 mg/s. This result is compared with the previous study, which carried out on geometrically similar but bigger Hall thruster model.


AIP Advances ◽  
2019 ◽  
Vol 9 (2) ◽  
pp. 025320
Author(s):  
Lubos Brieda ◽  
Justin Koo ◽  
Michelle Scharfe

2010 ◽  
Vol 26 (6) ◽  
pp. 1312-1317 ◽  
Author(s):  
Jerry L. Ross ◽  
Jason D. Sommerville ◽  
Lyon B. King

Author(s):  
Yevgeny Raitses ◽  
Artem Smirnov ◽  
David Staack ◽  
Michael Keidar ◽  
Nathaniel Fisch

2016 ◽  
Vol 18 (4) ◽  
pp. 382-387 ◽  
Author(s):  
Ping Duan ◽  
Guangrui Liu ◽  
Xingyu Bian ◽  
Long Chen ◽  
Yan Yin ◽  
...  

2009 ◽  
Vol 49 (6) ◽  
pp. 413-421 ◽  
Author(s):  
D. R. Yu ◽  
J. Li ◽  
H. Liu ◽  
Z. X. Ning ◽  
Y. Li

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