D-20
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
TsNIIMash electric/xenon rocket engine. Development. Hall effect thruster with anode layer, designed for satellite station-keeping and attitude control. Taken to engineering model stage.
Thrust 0.5 to 1.5 mN, power requirement 0.2 to 0.4 kW, specific impulse 1400-2500 seconds, efficiency 40%.
Electrical Input Power: 0.40 kW.
Related
- Country
- Russia
- Propellants
- Electric/Xenon
- Agency
- TsNIIMash