BPT-2000

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BPT-2000

Part of BPT engine series

BPT-2000
Credit: Aerojet Redmond

Redmond electric/xenon rocket engine. In Production. Hall effect thruster. Nominal power input 2200 W at 350 V.

Status: In Production. Thrust: 0.12 N (0.03 lbf). Unfuelled mass: 5.20 kg (11.40 lb). Specific impulse: 1,765 s. Burn time: 6,000 s. Height: 0.15 m (0.49 ft). Diameter: 0.20 m (0.65 ft).

Electrical Input Power: 2.20 kW. Engine: 5.20 kg (11.40 lb). Restarts: 6000.

Country: USA. Propellants: Electric/Xenon. Agency: Redmond.

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