NEXT (ion thruster)
NEXT affords larger delivered payloads, smaller launch vehicle size, and other mission enhancements compared to chemical and other electric propulsion technologies for Discovery, New Frontiers, Mars Exploration, and Flagship outer-planet exploration missions. Glenn Research Center manufactured the test engine's core ionization chamber, and Aerojet Rocketdyne designed and built the ion acceleration assembly.
The NEXT engine is a type of solar electric propulsion in which thruster systems use the electricity generated by the spacecraft's solar panel to accelerate the xenon propellant to speeds of up to 90,000 mph (145,000 km/h). NEXT can produce 6.9 kW thruster power and 236 mN thrust. It can be throttled down to 0.5 kW power, and has a specific impulse of 4190 seconds (compared to 3120 for NSTAR). The NEXT thruster has demonstrated a total impulse of 17 MN·s; which is the highest total impulse ever demonstrated by an ion thruster. A beam extraction area 1.6 times that of NSTAR allows higher thruster input power while maintaining low voltages and ion current densities, thus maintaining thruster longevity.
In November 2010, it was revealed that the prototype had completed a 48000 hours (5.5 years) test in December 2009. Thruster performance characteristics, measured over the entire throttle range of the thruster, were within predictions and the engine showed little signs of degradation and is ready for mission opportunities.
NASA is considering offering this ion thruster for the next Discovery Program mission. Proposed missions include placing an orbiter up to 4000 kg into Saturn orbit, or performing a sample return from Mars' moon Deimos.
- Electrically powered spacecraft propulsion
- Hall effect thruster
- Nuclear electric rocket
- Spacecraft propulsion
- George R Schmidt, Michael J Patterson, Scott W Benson. "The NASA Evolutionary Xenon Thruster (NEXT): the next step for US deep space propulsion".
- Herman, Daniel A. (May 3–7, 2010), "NASA’s Evolutionary Xenon Thruster (NEXT)Project Qualifi cation Propellant Throughput Milestone: Performance, Erosion, and Thruster Service Life Prediction After 450 kg", 57th Joint Army-Navy-NASA-Air Force (JANNAF) Propulsion Meeting, Colorado Springs, Colorado, USA: NASA - Glenn Research Center, retrieved 2014-03-08
- Dwayne Brown, Katherine K. Martin, Glenn Mahone. "NASA Thruster Achieves World-Record 5+ Years of Operation". Retrieved 2013-06-24.
- David Szondy. "NASA's NEXT ion thruster runs five and a half years nonstop to set new record". Retrieved 26 June 2013.
- Nancy Smith Kilkenny, SGT,Inc. "NEXT Provides Lasting Propulsion and High Speeds for Deep Space Missions". Retrieved 29 September 2013.
- Kane, Van (20 February 2014). "Boundaries for the Next Discovery Mission Selection". Future Planets. Archived from the original on 2014-03-07.
- Benson, Scott W.; John P. Riehl and Steven R. Oleson (2008), "NEXT Ion Propulsion System Configurations and", American Institute of Aeronautics and Astronautics, retrieved 9 March 2014
- "1633.PDF" (PDF). Lpi.usra.edu. Retrieved 28 February 2014.
- "Merlin : Mars-Moon Exploration" (PDF). Multimedia.seti.org. Retrieved 28 February 2014.