Add to ORKGThe objective was to study the effect of the arcjet thruster plume on the performance of an onboard satellite reflector antenna. A project summary is presented along with sections on plasma and electromagnetic modeling. The plasma modeling section includes the following topics: wave propagation; plasma analysis; plume electron density model; and the proposed experimental program. The section on electromagnetic modeling includes new developments in ray modeling and the validation of three dimensional ray results
An ion thruster for satellites on the order of 10-50 kg in mass is currently under development. The ...
An ion thruster for satellites on the order of 10-50 kg in mass is currently under development. The ...
Four basic areas were covered: development of analysis techniques and software and numerical simulat...
The final report includes an analysis of various plasma effects on the electromagnetic environment o...
An experiment was designed and conducted in the Electric Propulsion Laboratory of NASA Lewis Researc...
The interaction of a 1 kW arcjet thruster plume with a communications signal is evaluated. A two-par...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76213/1/AIAA-1996-2706-928.pd
During the course of this grant, work was performed on a variety of topics and there were a number o...
Electric thrusters are being considered for a variety of space missions because of the significant p...
Spacecraft entering a planetary atmosphere are surrounded by a plasma layer containing high levels o...
Plasma effects in antenna near zone field - admittance and ionization rise time measurements on Tefl...
Active research is reported in the following areas: (1) whistler propagation; (2) whistler triggered...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77043/1/AIAA-2001-3638-544.pd
Application of electrothermal arcjets on communications satellites requires assessment of integratio...
An ion thruster for satellites on the order of 10-50 kg in mass is currently under development. The ...
An ion thruster for satellites on the order of 10-50 kg in mass is currently under development. The ...
An ion thruster for satellites on the order of 10-50 kg in mass is currently under development. The ...
Four basic areas were covered: development of analysis techniques and software and numerical simulat...
The final report includes an analysis of various plasma effects on the electromagnetic environment o...
An experiment was designed and conducted in the Electric Propulsion Laboratory of NASA Lewis Researc...
The interaction of a 1 kW arcjet thruster plume with a communications signal is evaluated. A two-par...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76213/1/AIAA-1996-2706-928.pd
During the course of this grant, work was performed on a variety of topics and there were a number o...
Electric thrusters are being considered for a variety of space missions because of the significant p...
Spacecraft entering a planetary atmosphere are surrounded by a plasma layer containing high levels o...
Plasma effects in antenna near zone field - admittance and ionization rise time measurements on Tefl...
Active research is reported in the following areas: (1) whistler propagation; (2) whistler triggered...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77043/1/AIAA-2001-3638-544.pd
Application of electrothermal arcjets on communications satellites requires assessment of integratio...
An ion thruster for satellites on the order of 10-50 kg in mass is currently under development. The ...
An ion thruster for satellites on the order of 10-50 kg in mass is currently under development. The ...
An ion thruster for satellites on the order of 10-50 kg in mass is currently under development. The ...
Four basic areas were covered: development of analysis techniques and software and numerical simulat...