Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76213/1/AIAA-1996-2706-928.pd
An advanced microwave interferometric system operating in the Ku (12–18 GHz) band has been implement...
Spacecraft entering a planetary atmosphere are surrounded by a plasma layer containing high levels o...
An ion thruster for satellites on the order of 10-50 kg in mass is currently under development. The ...
An experiment was designed and conducted in the Electric Propulsion Laboratory of NASA Lewis Researc...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76372/1/AIAA-1997-3067-147.pd
Electric thrusters are being considered for a variety of space missions because of the significant p...
The objective was to study the effect of the arcjet thruster plume on the performance of an onboard ...
The interaction of a 1 kW arcjet thruster plume with a communications signal is evaluated. A two-par...
Electric propulsion is ideal for some space missions due to its high exhaust velocities and efficien...
Electric propulsion is ideal for some space missions due to its high exhaust velocities and efficien...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76740/1/AIAA-1998-3642-699.pd
Microwave interferometry was used to investigate the impact of the plume of a D-55 anode layer thrus...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77043/1/AIAA-2001-3638-544.pd
Stationary Plasma Thrusters (SPT's) are being investigated for application to a variety of near-term...
The transmission and degradation of RF signals through the plasma sheath surrounding hypersonic vehi...
An advanced microwave interferometric system operating in the Ku (12–18 GHz) band has been implement...
Spacecraft entering a planetary atmosphere are surrounded by a plasma layer containing high levels o...
An ion thruster for satellites on the order of 10-50 kg in mass is currently under development. The ...
An experiment was designed and conducted in the Electric Propulsion Laboratory of NASA Lewis Researc...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76372/1/AIAA-1997-3067-147.pd
Electric thrusters are being considered for a variety of space missions because of the significant p...
The objective was to study the effect of the arcjet thruster plume on the performance of an onboard ...
The interaction of a 1 kW arcjet thruster plume with a communications signal is evaluated. A two-par...
Electric propulsion is ideal for some space missions due to its high exhaust velocities and efficien...
Electric propulsion is ideal for some space missions due to its high exhaust velocities and efficien...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76740/1/AIAA-1998-3642-699.pd
Microwave interferometry was used to investigate the impact of the plume of a D-55 anode layer thrus...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77043/1/AIAA-2001-3638-544.pd
Stationary Plasma Thrusters (SPT's) are being investigated for application to a variety of near-term...
The transmission and degradation of RF signals through the plasma sheath surrounding hypersonic vehi...
An advanced microwave interferometric system operating in the Ku (12–18 GHz) band has been implement...
Spacecraft entering a planetary atmosphere are surrounded by a plasma layer containing high levels o...
An ion thruster for satellites on the order of 10-50 kg in mass is currently under development. The ...
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