Plasma plume measurements are reported for a hollow cathode assembly (HCA) oper-ated at discharge currents of 50, 70, and 100 A at xenon ow rates between 19 - 46 sccm.The HCA was centrally mounted in the annulus of the NASA-300MS Hall Thruster andwas operated in the spot and plume modes with additional data taken with an appliedmagnetic eld. Langmuir probes, retarding potential analyzers, and optical emission spec-troscopy were employed to measure plasma properties near the orice of the HCA and toassess the charge state of the near-eld plasma. Electron temperatures (2-6 eV) and plasmapotentials are consistent with probe-measured values in previous investigations. Operationwith an applied-eld yields higher discharge voltages, increased Xe II...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77184/1/AIAA-2001-3795-876.pd
The applications of electric propulsion are widely increasing in commercial and scientific missions ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76514/1/AIAA-1998-3658-652.pd
Plasma plume measurements are reported for a hollow cathode assembly (HCA) operated at discharge cur...
Electric propulsion for spacecraft has become increasingly commonplace in recent decades as designer...
Lanthanum hexaboride hollow cathodes represent a viable option for high power Hall effect thruster a...
Lanthanum hexaboride hollow cathodes represent a viable option for high power Hall effect thruster a...
Lanthanum hexaboride hollow cathodes represent a viable option for high power Hall effect thruster a...
Lanthanum hexaboride hollow cathodes represent a viable option for high power Hall effect thruster a...
NASA's Office of the Chief Technologist In-Space Propulsion project is sponsoring the testing and de...
High-power Hall Effect thrusters (HETs) represent an attractive propulsion option for the next-gener...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76762/1/AIAA-2003-4171-765.pd
High-power Hall Effect thrusters (HETs) represent an attractive propulsion option for the next-gener...
High-power Hall Effect thrusters (HETs) represent an attractive propulsion option for the next-gener...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77317/1/AIAA-2004-3795-393.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77184/1/AIAA-2001-3795-876.pd
The applications of electric propulsion are widely increasing in commercial and scientific missions ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76514/1/AIAA-1998-3658-652.pd
Plasma plume measurements are reported for a hollow cathode assembly (HCA) operated at discharge cur...
Electric propulsion for spacecraft has become increasingly commonplace in recent decades as designer...
Lanthanum hexaboride hollow cathodes represent a viable option for high power Hall effect thruster a...
Lanthanum hexaboride hollow cathodes represent a viable option for high power Hall effect thruster a...
Lanthanum hexaboride hollow cathodes represent a viable option for high power Hall effect thruster a...
Lanthanum hexaboride hollow cathodes represent a viable option for high power Hall effect thruster a...
NASA's Office of the Chief Technologist In-Space Propulsion project is sponsoring the testing and de...
High-power Hall Effect thrusters (HETs) represent an attractive propulsion option for the next-gener...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76762/1/AIAA-2003-4171-765.pd
High-power Hall Effect thrusters (HETs) represent an attractive propulsion option for the next-gener...
High-power Hall Effect thrusters (HETs) represent an attractive propulsion option for the next-gener...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77317/1/AIAA-2004-3795-393.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77184/1/AIAA-2001-3795-876.pd
The applications of electric propulsion are widely increasing in commercial and scientific missions ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76514/1/AIAA-1998-3658-652.pd