Add to ORKGDevelopment and tests of flight prototype power conditioner for 20 cm mercury bombardment electric thruster syste
A planned flight test of an 8 cm diameter, electron-bombardment mercury ion thruster system is descr...
The mechanical design of the mercury bombardment thruster that was tested on SERT is described. The ...
Xenon ion propulsion systems are being developed by NASA Lewis Research Center and the Jet Propulsio...
A prototype electric power management and thruster control system for a 30 cm ion thruster is descri...
Control logic functions were established for three automatic modes of operation of a 30-cm thruster ...
The design and development of power conditioning equipment for the thermoelectric outer planet space...
A feasibility study was made of the application of silicon-controlled, rectifier series, resonant in...
An electrical prototype power processor unit was designed, fabricated and tested with a 30 cm mercur...
A thrust stand for use with high power electric propulsion devices was designed and tested. The thru...
The technology development of the 30 centimeter J series mercury ion thruster for prime propulsion a...
A comparative review of the principles of ion thruster and chemical rocket operations is presented. ...
The development of electric propulsion systems is discussed and the benefits of these systems to var...
NASA GRC successfully designed, built and tested four different power processor concepts for high po...
Equipment was designed to receive power from a radioisotope thermoelectric generator source, conditi...
Analysis of electric propulsion electric power conditioning component technology - data revie
A planned flight test of an 8 cm diameter, electron-bombardment mercury ion thruster system is descr...
The mechanical design of the mercury bombardment thruster that was tested on SERT is described. The ...
Xenon ion propulsion systems are being developed by NASA Lewis Research Center and the Jet Propulsio...
A prototype electric power management and thruster control system for a 30 cm ion thruster is descri...
Control logic functions were established for three automatic modes of operation of a 30-cm thruster ...
The design and development of power conditioning equipment for the thermoelectric outer planet space...
A feasibility study was made of the application of silicon-controlled, rectifier series, resonant in...
An electrical prototype power processor unit was designed, fabricated and tested with a 30 cm mercur...
A thrust stand for use with high power electric propulsion devices was designed and tested. The thru...
The technology development of the 30 centimeter J series mercury ion thruster for prime propulsion a...
A comparative review of the principles of ion thruster and chemical rocket operations is presented. ...
The development of electric propulsion systems is discussed and the benefits of these systems to var...
NASA GRC successfully designed, built and tested four different power processor concepts for high po...
Equipment was designed to receive power from a radioisotope thermoelectric generator source, conditi...
Analysis of electric propulsion electric power conditioning component technology - data revie
A planned flight test of an 8 cm diameter, electron-bombardment mercury ion thruster system is descr...
The mechanical design of the mercury bombardment thruster that was tested on SERT is described. The ...
Xenon ion propulsion systems are being developed by NASA Lewis Research Center and the Jet Propulsio...