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Effects of segmented electrode in Hall current plasma thrusters
Y. Raitses
, M. Keidar
, D. Staack
,
N. J. Fisch
PPPL Discovery Plasma Science
Astrophysical Sciences
Mechanical & Aerospace Engineering
Research output
:
Contribution to journal
›
Article
›
peer-review
61
Scopus citations
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Dive into the research topics of 'Effects of segmented electrode in Hall current plasma thrusters'. Together they form a unique fingerprint.
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Engineering
Thruster
100%
Hall Thruster
50%
Plasma Plume
50%
Electron Emission
50%
Channel Wall
50%
Potential Distribution
50%
Secondary Electrons
50%
Keyphrases
Axial Acceleration
33%