BPT-4000
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.

Credit: Aerojet Redmond
Redmond electric/xenon rocket engine. In Production. Hall effect thruster. Nominal power input 4500 W at 350 V.
Electrical Input Power: 4.50 kW. Engine: 7.50 kg (16.50 lb). Restarts: 6000.
Related
- Country
- USA
- Propellants
- Electric/Xenon
- Agency
- Redmond
