Inert gas performance with three types of 12 cm diameter magnetoelectrostatic containment (MESC) ion thrusters was tested. The types tested included: (1) a hemispherical shaped discharge chamber with platinum cobalt magnets; (2) three different lengths of the hemispherical chambers with samarium cobalt magnets; and (3) three lengths of the conical shaped chambers with aluminum nickel cobalt magnets. The best argon performance was produced by a 8.0 cm long conical chamber with alnico magnets. The best xenon high mass utilization performance was obtained with the same 8.0 cm long conical thruster. The hemispherical thruster obtained 75 to 87% mass utilization at 185 to 205 eV/ion of singly charged ion equivalent beam
Some advances in component technology for inert gas thrusters are described. The maximum electron em...
Presented are performance data for laboratory and engineering model 30 cm-diameter ion thrusters ope...
Inert gases, particularly argon and xenon, are of interest as possible alternatives to the usual ele...
Two 12 cm magneto-electrostatic containment (MESC) ion thrusters were performance mapped with argon ...
Inert gases are of interest as possible alternatives to the usual electric thruster propellants of m...
Inert gas thrusters have continued to be of interest for space propulsion applications. Xenon is of ...
Design analyses showed that an ion thruster of approximately 50 cm in diameter will be required to p...
Space electric rocket test thruster performance with xenon, krypton, argon, neon, nitrogen, helium, ...
A 17 cm diameter line cusp ion thruster was evaluated with inert gases which are candidate propellan...
A 30-centimeter diameter ring-cusp ion thruster is described which operates at inert gas ion beam cu...
This study undertakes the analysis and conceptual design of a 0.5 Newton electrostatic ion thruster ...
Electron bombardment ion thrusters using inert gases are candidates for large space systems. The J-S...
The multipole thruster was used to investigate the use of argon and xenon propellants as possible al...
An electron-bombardment ion thruster of the SERT 2 type was operated with xenon, krypton, argon, neo...
The mercury bombardment electrostatic ion thruster is the most successful electric thruster availabl...
Some advances in component technology for inert gas thrusters are described. The maximum electron em...
Presented are performance data for laboratory and engineering model 30 cm-diameter ion thrusters ope...
Inert gases, particularly argon and xenon, are of interest as possible alternatives to the usual ele...
Two 12 cm magneto-electrostatic containment (MESC) ion thrusters were performance mapped with argon ...
Inert gases are of interest as possible alternatives to the usual electric thruster propellants of m...
Inert gas thrusters have continued to be of interest for space propulsion applications. Xenon is of ...
Design analyses showed that an ion thruster of approximately 50 cm in diameter will be required to p...
Space electric rocket test thruster performance with xenon, krypton, argon, neon, nitrogen, helium, ...
A 17 cm diameter line cusp ion thruster was evaluated with inert gases which are candidate propellan...
A 30-centimeter diameter ring-cusp ion thruster is described which operates at inert gas ion beam cu...
This study undertakes the analysis and conceptual design of a 0.5 Newton electrostatic ion thruster ...
Electron bombardment ion thrusters using inert gases are candidates for large space systems. The J-S...
The multipole thruster was used to investigate the use of argon and xenon propellants as possible al...
An electron-bombardment ion thruster of the SERT 2 type was operated with xenon, krypton, argon, neo...
The mercury bombardment electrostatic ion thruster is the most successful electric thruster availabl...
Some advances in component technology for inert gas thrusters are described. The maximum electron em...
Presented are performance data for laboratory and engineering model 30 cm-diameter ion thrusters ope...
Inert gases, particularly argon and xenon, are of interest as possible alternatives to the usual ele...