TAL-100
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
TAL-200 HAL effect thruster
Credit: TsNIIMASH
TsNIIMash electric/xenon rocket engine. Development. Hall effect thruster with anode layer. Export version of D-100-I thruster developed under NASA/BMDO contract. Taken to engineering model stage.
Used for satellite orbital altitude maintenance and raising. Thrust 8 to 34 mN, power requirement 1.3 to 7.5 kW, specific impulse 1450-2800 seconds, efficiency 60%.
Electrical Input Power: 7.50 kW.
Related
- Country
- Russia
- Propellants
- Electric/Xenon
- Agency
- TsNIIMash