Review of hall thruster plume modeling

Journal of Spacecraft and Rockets

Volumn 38, Issue 3, 2001, Pages 381-387

  Boyd, I D ^a  

^a UNIVERSITY OF MICHIGAN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; COMMUNICATION SATELLITES; COMPUTER SIMULATION; ELECTRIC FIELDS; ELECTRIC PROPULSION; MATHEMATICAL MODELS; PROPELLANTS; SPACECRAFT;

HALL THRUSTER PLUMES;

SPACECRAFT PROPULSION;

EID: 0035331503     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3695     Document Type: Article

References (31)

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4. Hall thruster ion beam characterization
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20. The mobilities of ions in unlike gases
21. Charge exchange between gaseous ions and atoms
22. + + Xe symmetric charge transfer
23. Origins of accelerator grid current: Analysis of T5 grid test results
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27. Analysis of collision phenomena in hall thruster plumes
28. Computational modeling of plasma plumes in a vacuum tank