D-100-II
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 orbital raising. Taken to engineering model stage.
Thrust 8 to 65 mN, power requirement 1.3 to 15 kW, specific impulse 1600-4250 seconds, efficiency 65%.
Electrical Input Power: 15.00 kW.
Related
- Country
- Russia
- Propellants
- Electric/Xenon
- Agency
- TsNIIMash