| BPT-4000 |
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Engine Model: BPT-4000. Designer: Aerojet Redmond. Propellants: Electric/Xenon. Thrust(vac): 0.27 N (0.06 lbf). Isp: 1,950 sec. Burn time: 6,000 sec. Mass Engine: 7.50 kg (16.50 lb). Diameter: 0.25 m (0.82 ft). Length: 0.16 m (0.52 ft). Chambers: 1. Country: USA. Status: In Production. Hall effect thruster. Nominal power input 4500 W at 350 V. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |
