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BPT engine series
| BPT-600k Redmond electric/xenon rocket engine. In Development, 2005-2006. Began as 1995 contract for 600kWe Hall thruster electric propulsion system designed for future interplanetary manned spacecraft. |
 | BPT-2000 Redmond electric/xenon rocket engine. In Production. Hall effect thruster. Nominal power input 2200 W at 350 V. |
 | BPT-4000 Redmond electric/xenon rocket engine. In Production. Hall effect thruster. Nominal power input 4500 W at 350 V. |
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