The NASA s Evolutionary Xenon Thruster (NEXT) program is developing the next-generation ion propulsion system with significant enhancements beyond the state-of-the-art in ion propulsion to provide future NASA science missions with enhanced mission capabilities at a low total development cost. As part of a comprehensive thruster service life assessment utilizing both testing and analyses, a Long-Duration Test (LDT) was initiated to verify the NEXT propellant throughput capability to a qualification-level of 450 kg, 1.5 times the anticipated throughput requirement of 300 kg from mission analyses conducted utilizing the NEXT propulsion system. The LDT is being conducted with a modified, flight-representative NEXT engineering model ion thruster...
Direct thrust measurements have been made on the NASA Evolutionary Xenon Thruster (NEXT) ion engine ...
A 30 cm diameter xenon ion thruster is under development at NASA to provide an ion propulsion option...
The NEXT ion thruster is a low specific mass, high performance thruster with a nominal throttling ra...
The NASA s Evolutionary Xenon Thruster (NEXT) program is developing the next-generation ion propulsi...
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 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 tasked with significantly improving and ext...
This presentation describes results from the end-of-test performance characterization of NASA's Evol...
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 NASA's Evolutionary Xenon Thruste...
The NEXT Long-Duration Test is part of a comprehensive thruster service life assessment intended to ...
The results of the NEXT wear test are presented. This test was conducted with a 36-cm ion engine (de...
A Long Duration Test (LDT) was initiated in June 2005 as a part of NASAs Evolutionary Xenon Thruster...
The NEXT Long-Duration Test is part of a comprehensive thruster service life assessment intended to ...
Direct thrust measurements have been made on the NASA Evolutionary Xenon Thruster (NEXT) ion engine ...
A 30 cm diameter xenon ion thruster is under development at NASA to provide an ion propulsion option...
The NEXT ion thruster is a low specific mass, high performance thruster with a nominal throttling ra...
The NASA s Evolutionary Xenon Thruster (NEXT) program is developing the next-generation ion propulsi...
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 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 tasked with significantly improving and ext...
This presentation describes results from the end-of-test performance characterization of NASA's Evol...
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 NASA's Evolutionary Xenon Thruste...
The NEXT Long-Duration Test is part of a comprehensive thruster service life assessment intended to ...
The results of the NEXT wear test are presented. This test was conducted with a 36-cm ion engine (de...
A Long Duration Test (LDT) was initiated in June 2005 as a part of NASAs Evolutionary Xenon Thruster...
The NEXT Long-Duration Test is part of a comprehensive thruster service life assessment intended to ...
Direct thrust measurements have been made on the NASA Evolutionary Xenon Thruster (NEXT) ion engine ...
A 30 cm diameter xenon ion thruster is under development at NASA to provide an ion propulsion option...
The NEXT ion thruster is a low specific mass, high performance thruster with a nominal throttling ra...