The NEXT propulsion system is an advanced ion propulsion system presently under development that is oriented towards robotic exploration of the solar system using solar electric power. The subsystem includes an ion engine, power processing unit, feed system components, and thruster gimbal. The Prototype Model engine PM1 was subjected to qualification-level environmental testing in 2006 to demonstrate compatibility with environments representative of anticipated mission requirements. Although the testing was largely successful, several issues were identified including the fragmentation of potting cement on the discharge and neutralizer cathode heater terminations during vibration which led to abbreviated thermal testing, and generation of pa...
Electron bombardment, mercury-fueled ion engine system - investigation, testing, and development pro...
A comparative review of the principles of ion thruster and chemical rocket operations is presented. ...
Several mission options are discussed for an electric propulsion space test which provides operation...
The NEXT propulsion system is an advanced ion propulsion system presently under development that is ...
The results of the NEXT wear test are presented. This test was conducted with a 36-cm ion engine (de...
NASA's New Millenium program will fly a xenon ion propulsion system on the Deep Space 1 Mission. Tes...
NASA's Evolutionary Xenon Thruster (NEXT) is a next-generation high-power ion thruster under develop...
NASA’s Evolutionary Xenon Thruster (NEXT) is a next-generation high-power ion propulsion system unde...
As a critical part of the NEXT test validation process, a multiple-string integration test was perfo...
The NASA's Evolutionary Xenon Thruster (NEXT) ion propulsion system has been in advanced technology ...
Xenon ion propulsion systems are being developed by NASA Lewis Research Center and the Jet Propulsio...
The NASA Solar Electric Propulsion Technology Applications Readiness Program (NSTAR) will provide a ...
The NASA Glenn Research Center ion-propulsion program addresses the need for high specific-impulse s...
The NASA's Evolutionary Xenon Thruster (NEXT) project is developing the next-generation solar electr...
NASA is continuing the development of a 12.5-kW Hall thruster system, which is baselined in a phased...
Electron bombardment, mercury-fueled ion engine system - investigation, testing, and development pro...
A comparative review of the principles of ion thruster and chemical rocket operations is presented. ...
Several mission options are discussed for an electric propulsion space test which provides operation...
The NEXT propulsion system is an advanced ion propulsion system presently under development that is ...
The results of the NEXT wear test are presented. This test was conducted with a 36-cm ion engine (de...
NASA's New Millenium program will fly a xenon ion propulsion system on the Deep Space 1 Mission. Tes...
NASA's Evolutionary Xenon Thruster (NEXT) is a next-generation high-power ion thruster under develop...
NASA’s Evolutionary Xenon Thruster (NEXT) is a next-generation high-power ion propulsion system unde...
As a critical part of the NEXT test validation process, a multiple-string integration test was perfo...
The NASA's Evolutionary Xenon Thruster (NEXT) ion propulsion system has been in advanced technology ...
Xenon ion propulsion systems are being developed by NASA Lewis Research Center and the Jet Propulsio...
The NASA Solar Electric Propulsion Technology Applications Readiness Program (NSTAR) will provide a ...
The NASA Glenn Research Center ion-propulsion program addresses the need for high specific-impulse s...
The NASA's Evolutionary Xenon Thruster (NEXT) project is developing the next-generation solar electr...
NASA is continuing the development of a 12.5-kW Hall thruster system, which is baselined in a phased...
Electron bombardment, mercury-fueled ion engine system - investigation, testing, and development pro...
A comparative review of the principles of ion thruster and chemical rocket operations is presented. ...
Several mission options are discussed for an electric propulsion space test which provides operation...