Near exit plane velocity field of a 200-watt Hall thruster

Journal of Propulsion and Power

Volumn 24, Issue 1, 2008, Pages 127-133

  Hargus Jr , William A ^a,b,c   Charles, Christopher S ^a,b,c  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b Spacecraft Propulsion Branch ^*

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

HALL EFFECT; IONIZATION; PROPELLANTS; VELOCITY MEASUREMENT; XENON;

ANODE POTENTIAL; HALL THRUSTERS; IONIZED PROPELLANT VELOCITIES; NEAR EXIT PLANE VELOCITY FIELD;

ROCKET ENGINES;

EID: 43649091590     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/1.29949     Document Type: Article

References (16)