Add to ORKGThe results of extensive testing of two 30-cm ion thrusters which are virtually identical to the 900...
Geometrically different sets of dished accelerator grids were tested on five 30-cm thrusters. The ge...
Engineering model designs and acceptance tests are described for the 800 and 900 series 30 cm electr...
The design of ion optics for bombardment thrusters strongly influences overall performance and lifet...
Performance of mercury electron bombardment thrustor at large acceleration potentia
The technology development of the 30 centimeter J series mercury ion thruster for prime propulsion a...
Results of the SERT II flight indicate that the hollow cathode neutralizer not only represents a pow...
The environmental and instrumentation requirements for long term testing of electrical propulsion th...
Thirteen sets of dished accelerator grids were treated on five different 30 cm diameter bombardment ...
A 2000-hour durability test of a modified Hughes SIT-5 (Structurally Integrated Thruster, 5 cm) was ...
Recent improvements in overall thruster performance have imposed new constraints on neutralizer perf...
Control logic functions were established for three automatic modes of operation of a 30-cm thruster ...
Electron bombardment thrusters, under development to provide both auxiliary and primary propulsion f...
Tests were performed to characterize the particles and fields associated with two 30 cm mercury ion ...
Some space flight missions require advanced ion thrusters which operate at conditions much different...
The results of extensive testing of two 30-cm ion thrusters which are virtually identical to the 900...
Geometrically different sets of dished accelerator grids were tested on five 30-cm thrusters. The ge...
Engineering model designs and acceptance tests are described for the 800 and 900 series 30 cm electr...
The design of ion optics for bombardment thrusters strongly influences overall performance and lifet...
Performance of mercury electron bombardment thrustor at large acceleration potentia
The technology development of the 30 centimeter J series mercury ion thruster for prime propulsion a...
Results of the SERT II flight indicate that the hollow cathode neutralizer not only represents a pow...
The environmental and instrumentation requirements for long term testing of electrical propulsion th...
Thirteen sets of dished accelerator grids were treated on five different 30 cm diameter bombardment ...
A 2000-hour durability test of a modified Hughes SIT-5 (Structurally Integrated Thruster, 5 cm) was ...
Recent improvements in overall thruster performance have imposed new constraints on neutralizer perf...
Control logic functions were established for three automatic modes of operation of a 30-cm thruster ...
Electron bombardment thrusters, under development to provide both auxiliary and primary propulsion f...
Tests were performed to characterize the particles and fields associated with two 30 cm mercury ion ...
Some space flight missions require advanced ion thrusters which operate at conditions much different...
The results of extensive testing of two 30-cm ion thrusters which are virtually identical to the 900...
Geometrically different sets of dished accelerator grids were tested on five 30-cm thrusters. The ge...
Engineering model designs and acceptance tests are described for the 800 and 900 series 30 cm electr...