Add to ORKGA Long Duration Test (LDT) was initiated in June 2005 as a part of NASAs Evolutionary Xenon Thruster (NEXT) service life validation approach. Testing was voluntarily terminated in February 2014, with the thruster accumulating 51,184 hours of operation, processing 918 kg of xenon propellant, and delivering 35.5 MN-s of total impulse. This presentation will present the post-test inspection results to date for the thrusters ion optics
A 30-cm diameter xenon ion thruster is under development at NASA to provide an ion propulsion option...
A long duration test of the DSl flight spare ion thruster (FT2) is presently being conducted at the ...
The NASA Hall Effect Rocket with Magnetic Shielding (HERMeS) 12.5-kW Hall thruster has been the subj...
A Long Duration Test (LDT) was initiated in June 2005 as a part of NASA's Evolutionary Xenon Thruste...
The NEXT Long-Duration Test is part of a comprehensive thruster service life assessment intended to ...
The NEXT Long-Duration Test is part of a comprehensive thruster service life assessment intended to ...
This presentation describes results from the end-of-test performance characterization of NASA's Evol...
The NASA's Evolutionary Xenon Thruster (NEXT) program is developing the next-generation solar electr...
The service life assessment for NASA's Evolutionary Xenon Thruster is updated to incorporate the res...
The NASA's Evolutionary Xenon Thruster (NEXT) project is developing the next-generation solar electr...
The NASA s Evolutionary Xenon Thruster (NEXT) program is developing the next-generation ion propulsi...
The NASA's Evolutionary Xenon Thruster (NEXT) program is developing the next-generation ion propulsi...
The NASA s Evolutionary Xenon Thruster (NEXT) program is developing the next-generation ion propulsi...
The NASA s Evolutionary Xenon Thruster (NEXT) program is tasked with significantly improving and ext...
The results of the NEXT wear test are presented. This test was conducted with a 36-cm ion engine (de...
A 30-cm diameter xenon ion thruster is under development at NASA to provide an ion propulsion option...
A long duration test of the DSl flight spare ion thruster (FT2) is presently being conducted at the ...
The NASA Hall Effect Rocket with Magnetic Shielding (HERMeS) 12.5-kW Hall thruster has been the subj...
A Long Duration Test (LDT) was initiated in June 2005 as a part of NASA's Evolutionary Xenon Thruste...
The NEXT Long-Duration Test is part of a comprehensive thruster service life assessment intended to ...
The NEXT Long-Duration Test is part of a comprehensive thruster service life assessment intended to ...
This presentation describes results from the end-of-test performance characterization of NASA's Evol...
The NASA's Evolutionary Xenon Thruster (NEXT) program is developing the next-generation solar electr...
The service life assessment for NASA's Evolutionary Xenon Thruster is updated to incorporate the res...
The NASA's Evolutionary Xenon Thruster (NEXT) project is developing the next-generation solar electr...
The NASA s Evolutionary Xenon Thruster (NEXT) program is developing the next-generation ion propulsi...
The NASA's Evolutionary Xenon Thruster (NEXT) program is developing the next-generation ion propulsi...
The NASA s Evolutionary Xenon Thruster (NEXT) program is developing the next-generation ion propulsi...
The NASA s Evolutionary Xenon Thruster (NEXT) program is tasked with significantly improving and ext...
The results of the NEXT wear test are presented. This test was conducted with a 36-cm ion engine (de...
A 30-cm diameter xenon ion thruster is under development at NASA to provide an ion propulsion option...
A long duration test of the DSl flight spare ion thruster (FT2) is presently being conducted at the ...
The NASA Hall Effect Rocket with Magnetic Shielding (HERMeS) 12.5-kW Hall thruster has been the subj...