This paper describes measurements of Hall thruster plumes that characterize ion energy distributions and charge state fractions using remotely located plasma diagnostics. Plume measurements were performed using electrostatic analyzers (ESAs) and ExB probes from Plasma Controls, LLC on ion and plasma sources at Colorado State University (CSU) and Hall thrusters operated at the Air Force Institute of Technology (AFIT) and the Air Force Research Laboratory (AFRL). Data are presented from ion source testing at CSU that demonstrated the performance of ESA and ExB probes to characterize energy and charge state. Next, energy and charge state measurements are described from testing of a 200 W Hall thruster at AFIT. Measurements showed variation in ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76401/1/AIAA-2008-5287-309.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77342/1/AIAA-11953-462.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76547/1/AIAA-20514-735.pd
For the purpose of understanding and characterizing the behavior of multiply charged propellant ions...
Electric propulsion offers new capabilities for ambitious space missions of the future. However, coa...
Electric propulsion offers new capabilities for ambitious space missions of the future. However, coa...
This thesis represents an effort to design, build, and characterize a 5 kW class Hall thruster for l...
This thesis represents a broad study to characterize the heavy-particle structure of the exhaust plu...
This thesis represents a broad study to characterize the heavy-particle structure of the exhaust plu...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77389/1/AIAA-1998-3641-696.pd
An E×B probe was used to characterize the angular distribution of multiply-charged ions in the plume...
The effects of facility backpressure and localized electric fields on the measured ion current densi...
Of primary concern with the integration of Hall thrusters on conventional satellite designs is the p...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76139/1/AIAA-2008-4647-932.pd
This dissertation represents a design and experimental effort of developing a two-stage hybrid Hall/...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76401/1/AIAA-2008-5287-309.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77342/1/AIAA-11953-462.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76547/1/AIAA-20514-735.pd
For the purpose of understanding and characterizing the behavior of multiply charged propellant ions...
Electric propulsion offers new capabilities for ambitious space missions of the future. However, coa...
Electric propulsion offers new capabilities for ambitious space missions of the future. However, coa...
This thesis represents an effort to design, build, and characterize a 5 kW class Hall thruster for l...
This thesis represents a broad study to characterize the heavy-particle structure of the exhaust plu...
This thesis represents a broad study to characterize the heavy-particle structure of the exhaust plu...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77389/1/AIAA-1998-3641-696.pd
An E×B probe was used to characterize the angular distribution of multiply-charged ions in the plume...
The effects of facility backpressure and localized electric fields on the measured ion current densi...
Of primary concern with the integration of Hall thrusters on conventional satellite designs is the p...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76139/1/AIAA-2008-4647-932.pd
This dissertation represents a design and experimental effort of developing a two-stage hybrid Hall/...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76401/1/AIAA-2008-5287-309.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77342/1/AIAA-11953-462.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76547/1/AIAA-20514-735.pd