The service life assessment for NASA's Evolutionary Xenon Thruster is updated to incorporate the results from the successful and voluntarily early completion of the 51,184 hour long duration test which demonstrated 918 kg of total xenon throughput. The results of the numerous post-test investigations including destructive interrogations have been assessed against all of the critical known and suspected failure mechanisms to update the life and throughput expectations for each major component. Analysis results of two of the most acute failure mechanisms, namely pit-and-groove erosion and aperture enlargement of the accelerator grid, are not updated in this work but will be published at a future time after analysis completion
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 results of the NEXT wear test are presented. This test was conducted with a 36-cm ion engine (de...
The NEXT Long-Duration Test is part of a comprehensive thruster service life assessment intended to ...
The NASA's Evolutionary Xenon Thruster (NEXT) project is developing the next-generation solar electr...
This presentation describes results from the end-of-test performance characterization of NASA's Evol...
A Long Duration Test (LDT) was initiated in June 2005 as a part of NASA's Evolutionary Xenon Thruste...
The NASA's Evolutionary Xenon Thruster (NEXT) program is developing the next-generation solar electr...
The NEXT Long-Duration Test is part of a comprehensive thruster service life assessment intended to ...
A Long Duration Test (LDT) was initiated in June 2005 as a part of NASAs Evolutionary Xenon Thruster...
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 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...
Ion thrusters are low thrust, high specific impulse devices with required operational lifetimes on t...
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 results of the NEXT wear test are presented. This test was conducted with a 36-cm ion engine (de...
The NEXT Long-Duration Test is part of a comprehensive thruster service life assessment intended to ...
The NASA's Evolutionary Xenon Thruster (NEXT) project is developing the next-generation solar electr...
This presentation describes results from the end-of-test performance characterization of NASA's Evol...
A Long Duration Test (LDT) was initiated in June 2005 as a part of NASA's Evolutionary Xenon Thruste...
The NASA's Evolutionary Xenon Thruster (NEXT) program is developing the next-generation solar electr...
The NEXT Long-Duration Test is part of a comprehensive thruster service life assessment intended to ...
A Long Duration Test (LDT) was initiated in June 2005 as a part of NASAs Evolutionary Xenon Thruster...
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 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...
Ion thrusters are low thrust, high specific impulse devices with required operational lifetimes on t...
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 results of the NEXT wear test are presented. This test was conducted with a 36-cm ion engine (de...