| BPT-2000 | ||
Designer: Aerojet Redmond. Propellants: Electric/Xenon. Thrust(vac): 0.12 N (0.03 lbf). Isp: 1,765 sec. Burn time: 6,000 sec. Mass Engine: 5.20 kg (11.40 lb). Diameter: 0.20 m (0.65 ft). Length: 0.15 m (0.49 ft). Chambers: 1. Country: USA. Status: In Production. Hall effect thruster. Nominal power input 2200 W at 350 V.
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