Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
BPT-2000
Part of BPT engine series Family
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.

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.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2017 Mark Wade - Contact
© / Conditions for Use