Wear Test of a Hollow Cathode for 35-cm Xenon Ion Thrusters

2002 ◽  
Author(s):  
Yukio Hayakawa ◽  
Shoji Kitamura ◽  
Katsuhiro Miyazaki ◽  
Hideki Yoshida ◽  
Kouseki Akai ◽  
...  
Keyword(s):  
Hollow Cathode ◽  
Wear Test ◽  
Ion Thrusters

Evidence of fireball phenomena in hollow cathode of electron bombardment ion thrusters.

AIAA Journal ◽  
1973 ◽  
Vol 11 (3) ◽  
pp. 399-400
Author(s):  
R. A. JACOBSEN ◽  
H. P. EUBANK
Keyword(s):  
Hollow Cathode ◽  
Electron Bombardment ◽  
Ion Thrusters

Wear Test Demonstration of a Technique to Mitigate Keeper Erosion in a High-Current LaB 6 Hollow Cathode

2016 ◽  
Author(s):  
Amanda Ho ◽  
Benjamin Jorns ◽  
Ioannis G. Mikellides ◽  
Dan M. Goebel ◽  
Alejandro Lopez Ortega
Keyword(s):  
Hollow Cathode ◽  
Wear Test ◽  
High Current

scholarly journals Hollow Cathode and Low-Thrust Extraction Grid Analysis for a Miniature Ion Thruster

2008 ◽  
Vol 2008 ◽  
pp. 1-11 ◽  
Author(s):  
Richard Wirz ◽  
Regina Sullivan ◽  
JoHanna Przybylowski ◽  
Mike Silva
Keyword(s):  
Hollow Cathode ◽  
High Efficiency ◽  
Low Thrust ◽  
Discharge Performance ◽  
Ion Thruster ◽  
Ion Extraction ◽  
Ion Thrusters ◽  
Future Space ◽  
Thrust Characteristics ◽  
Computational Analyses

Miniature ion thrusters are well suited for future space missions that require high efficiency, precision thrust, and low contamination in the mN to sub-mN range. JPL's miniature xenon Ion (MiXI) thruster has demonstrated an efficient discharge and ion extraction grid assembly using filament cathodes and the internal conduction (IC) cathode. JPL is currently preparing to incorporate a miniature hollow cathode for the MiXI discharge. Computational analyses anticipate that an axially upstream hollow cathode location provides the most favorable performance and beam profile; however, the hot surfaces of the hollow cathode must be sufficiently downstream to avoid demagnetization of the cathode magnet at the back of the chamber, which can significantly reduce discharge performance. MiXI's ion extraction grids are designed to provide >3 mN of thrust; however, previous to this effort, the low-thrust characteristics had not been investigated. Experimental results obtained with the MiXI-II thruster (a near replica or the original MiXI thruster) show that sparse average discharge plasma densities of ∼5×1015–5×1016 m-3 allow the use of very low beamlet focusing extraction voltages of only ∼250–500 V, thus providing thrust levels as low as 0.03 mN for focused beamlet conditions. Consequently, the thrust range thus far demonstrated by MiXI in this and other tests is 0.03–1.54 mN.

TEMPERATURE OF HEAVY-CURRENT CYLINDRICAL HOLLOW CATHODE

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

TEMPORAL BEHAVIOUR OF THE OPTOGALVANIC SIGNAL IN A HOLLOW CATHODE LAMP

1983 ◽  
Vol 44 (C7) ◽  
pp. C7-479-C7-487 ◽  
Author(s):  
M. Broglia ◽  
F. Catoni ◽  
P. Zampetti
Keyword(s):  
Hollow Cathode ◽  
Temporal Behaviour ◽  
Hollow Cathode Lamp
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