Effect of Discharge Voltage on Plume Divergence of a High Specific Impulse Hall Thruster

Author(s):  
Yassir Azziz ◽  
Manuel Martinez-Sanchez ◽  
James Szabo
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.


2008 ◽  
Vol 36 (5) ◽  
pp. 2069-2081 ◽  
Author(s):  
A. Cohen-Zur ◽  
A. Fruchtman ◽  
A. Gany

2006 ◽  
Vol 89 (11) ◽  
pp. 111501 ◽  
Author(s):  
A. Fruchtman ◽  
A. Cohen-Zur

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

Measurement ◽  
2014 ◽  
Vol 50 ◽  
pp. 74-77 ◽  
Author(s):  
Yang Tianci ◽  
Wei Liqiu ◽  
Han Liang ◽  
Zhang Chaohai ◽  
Yu Daren

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

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