A 5-cm diameter mercury ion thruster main cathode has completed over 20,000 hours of operation in an ongoing lifetime endurance test. The cathode operating parameters remained at acceptable performance levels throughout the test, the first 9175 hours of which were part of a thruster endurance test. After 20,000 hours, the cathode discharge was easily restarted, the tip orifice indicated negligible erosion and the tip heater showed no degradation. The cathode-isolator- vaporizer assembly, a major thruster subsystem, has thus successfully demonstrated an operational lifetime capability of 20,000 hours, which is the lifetime goal of the 8-cm diameter auxiliary propulsion ion thruster
Ion thrusters are high-efficiency, high-specific impulse space propulsion systems proposed for deep ...
An experimental investigation of hollow cathodes for 30-cm Hg bombardment thrusters was carried out....
The NEXT Long-Duration Test is part of a comprehensive thruster service life assessment intended to ...
Two main cathodes have successfully completed 2800 and 1980 cycles and three neutralizers, 3928, 305...
Electron bombardment thrusters, under development to provide both auxiliary and primary propulsion f...
A number of space missions were proposed which utilize 30-cm mercury bombardment ion thrusters and a...
A laboratory model 8 cm thruster with improvements to minimize ion chamber erosion and peeling of sp...
A 2000-hour durability test of a modified Hughes SIT-5 (Structurally Integrated Thruster, 5 cm) was ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76711/1/AIAA-21325-978.pd
A plasma contacting device using a hollow cathode for plasma production has been baselined for use o...
The environmental and instrumentation requirements for long term testing of electrical propulsion th...
Implementation of a hollow cathode plasma contactor for charge control on the Space Station has requ...
A modified Hughes SIT-5 system is being tested for durability at the Lewis Research Center. As of Oc...
Ion thrusters are high-efficiency, high-specific impulse space propulsion systems proposed for deep ...
This report describes the qualification test of an Engineering-Model 5-mN-thrust 8-cm-diameter mercu...
Ion thrusters are high-efficiency, high-specific impulse space propulsion systems proposed for deep ...
An experimental investigation of hollow cathodes for 30-cm Hg bombardment thrusters was carried out....
The NEXT Long-Duration Test is part of a comprehensive thruster service life assessment intended to ...
Two main cathodes have successfully completed 2800 and 1980 cycles and three neutralizers, 3928, 305...
Electron bombardment thrusters, under development to provide both auxiliary and primary propulsion f...
A number of space missions were proposed which utilize 30-cm mercury bombardment ion thrusters and a...
A laboratory model 8 cm thruster with improvements to minimize ion chamber erosion and peeling of sp...
A 2000-hour durability test of a modified Hughes SIT-5 (Structurally Integrated Thruster, 5 cm) was ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76711/1/AIAA-21325-978.pd
A plasma contacting device using a hollow cathode for plasma production has been baselined for use o...
The environmental and instrumentation requirements for long term testing of electrical propulsion th...
Implementation of a hollow cathode plasma contactor for charge control on the Space Station has requ...
A modified Hughes SIT-5 system is being tested for durability at the Lewis Research Center. As of Oc...
Ion thrusters are high-efficiency, high-specific impulse space propulsion systems proposed for deep ...
This report describes the qualification test of an Engineering-Model 5-mN-thrust 8-cm-diameter mercu...
Ion thrusters are high-efficiency, high-specific impulse space propulsion systems proposed for deep ...
An experimental investigation of hollow cathodes for 30-cm Hg bombardment thrusters was carried out....
The NEXT Long-Duration Test is part of a comprehensive thruster service life assessment intended to ...