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BPT-2000

Engine · USA

Original archive entry. The text, images and links below are kept as they were written.

BPT-2000
BPT-2000
Credit: Aerojet Redmond

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

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

Country
USA
Propellants
Electric/Xenon
Agency
Redmond