NEXT (ion thruster)

Type: Ion Engine
Country of Origin: United States
Manufacturer: NASA, Aerojet Rocketdyne

First Flight:
Status: In development
Propellant: Xenon
Chambers: 1

Thrust (vac.): 0.236 N (6.9 kW)
Throttle: 7.2% to 100% (0.5 kW to 6.9 kW)
ISP (vac.): 4190 s
Burn time: 5.5 years +
Ignitions: unlimited