The NEXT Long-Duration Test is part of a comprehensive thruster service life assessment intended to demonstrate overall throughput capability, validate service life models, quantify wear rates as a function of time and operating condition, and identify any unknown life-limiting mechanisms. The test was voluntarily terminated in February 2014 after demonstrating 51,184 hours of high-voltage operation, 918 kg of propellant throughput, and 35.5 MN-s of total impulse. The post-test inspection of the thruster hardware began shortly afterwards with a combination of non-destructive and destructive analysis techniques, and is presently nearing completion. This paper presents relevant results of the post-test inspection for both discharge and neutra...
Hollow dispenser cathode inserts are a critical element of electric propulsion systems, and should t...
A 30-cm diameter xenon ion thruster is under development at NASA to provide an ion propulsion option...
The environmental and instrumentation requirements for long term testing of electrical propulsion th...
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 ...
The NASA's Evolutionary Xenon Thruster (NEXT) program is developing the next-generation solar electr...
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) project is developing the next-generation solar electr...
The service life assessment for NASA's Evolutionary Xenon Thruster is updated to incorporate the res...
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...
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 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...
Hollow dispenser cathode inserts are a critical element of electric propulsion systems, and should t...
A 30-cm diameter xenon ion thruster is under development at NASA to provide an ion propulsion option...
The environmental and instrumentation requirements for long term testing of electrical propulsion th...
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 ...
The NASA's Evolutionary Xenon Thruster (NEXT) program is developing the next-generation solar electr...
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) project is developing the next-generation solar electr...
The service life assessment for NASA's Evolutionary Xenon Thruster is updated to incorporate the res...
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...
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 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...
Hollow dispenser cathode inserts are a critical element of electric propulsion systems, and should t...
A 30-cm diameter xenon ion thruster is under development at NASA to provide an ion propulsion option...
The environmental and instrumentation requirements for long term testing of electrical propulsion th...