A modified Hughes SIT-5 system is being tested for durability at the Lewis Research Center. As of October 1, 1972, the thruster subsystem has logged over 8000 hours of operation. The initial 2023 hours were run with a translating screen thrust vector grid. The thruster is currently operating with an electrostatic type vector grid. Profiles and maps taken at widely separated intervals show that performance and operating characteristics have remained essentially constant. Overall efficiency is about 32 percent and power to thrust ratio is 170 watts per millipound at a specific impulse of 2500 seconds. Telescopic examination of the vector grid shows some sputtering erosion due to charge exchange and direct impingement ions
This report describes the qualification test of an Engineering-Model 5-mN-thrust 8-cm-diameter mercu...
A single-axis electrostatic beam deflection system has been tested on a 5-cm diameter mercury ion th...
The technology development of the 30 centimeter J series mercury ion thruster for prime propulsion a...
A 2000-hour durability test of a modified Hughes SIT-5 (Structurally Integrated Thruster, 5 cm) was ...
A grid-translation type beam deflection system was tested on a 5-cm diameter mercury ion thruster fo...
A 5-cm diameter mercury ion thruster main cathode has completed over 20,000 hours of operation in an...
The environmental and instrumentation requirements for long term testing of electrical propulsion th...
A laboratory model 8 cm thruster with improvements to minimize ion chamber erosion and peeling of sp...
Prototype auxiliary propulsion subsystem with isolated single tank propellant feed system and 5-cm-d...
Two thruster sizes are studied. One, a small 5-cm or 8-cm size is for spacecraft station keeping. Th...
A 5-cm structurally integrated ion thruster has been developed for attitude control and stationkeepi...
Electron bombardment thrusters, under development to provide both auxiliary and primary propulsion f...
Some space flight missions require advanced ion thrusters which operate at conditions much different...
A 30-cm diameter xenon ion thruster is under development at NASA to provide an ion propulsion option...
Engineering model designs and acceptance tests are described for the 800 and 900 series 30 cm electr...
This report describes the qualification test of an Engineering-Model 5-mN-thrust 8-cm-diameter mercu...
A single-axis electrostatic beam deflection system has been tested on a 5-cm diameter mercury ion th...
The technology development of the 30 centimeter J series mercury ion thruster for prime propulsion a...
A 2000-hour durability test of a modified Hughes SIT-5 (Structurally Integrated Thruster, 5 cm) was ...
A grid-translation type beam deflection system was tested on a 5-cm diameter mercury ion thruster fo...
A 5-cm diameter mercury ion thruster main cathode has completed over 20,000 hours of operation in an...
The environmental and instrumentation requirements for long term testing of electrical propulsion th...
A laboratory model 8 cm thruster with improvements to minimize ion chamber erosion and peeling of sp...
Prototype auxiliary propulsion subsystem with isolated single tank propellant feed system and 5-cm-d...
Two thruster sizes are studied. One, a small 5-cm or 8-cm size is for spacecraft station keeping. Th...
A 5-cm structurally integrated ion thruster has been developed for attitude control and stationkeepi...
Electron bombardment thrusters, under development to provide both auxiliary and primary propulsion f...
Some space flight missions require advanced ion thrusters which operate at conditions much different...
A 30-cm diameter xenon ion thruster is under development at NASA to provide an ion propulsion option...
Engineering model designs and acceptance tests are described for the 800 and 900 series 30 cm electr...
This report describes the qualification test of an Engineering-Model 5-mN-thrust 8-cm-diameter mercu...
A single-axis electrostatic beam deflection system has been tested on a 5-cm diameter mercury ion th...
The technology development of the 30 centimeter J series mercury ion thruster for prime propulsion a...