РУС
ENG
News
About us
Order placement
Unified Product and Component Portal
for the rocket and space industry
Spacecraft
Launch Vehicles
Upper Stages
Human Space Flights
Ground Infrastructure
Other products
Home
→
Product guide
→
Spacecraft
→
Propulsion Systems
→
Thrusters
Thrusters
Ion Thruster for Geostationary Satellite Platforms Correction
Electric Thruster for Spacecraft with Mass up to 3000 kg 1
High-powered Electric Thruster for Spacecraft with Mass up to 3000 kg
Electrically Powered Cruise Engine
Multichannel Electric Thruster
Electric Thruster for Spacecraft with Mass up to 500 kg
Electric Thruster for Spacecraft with Mass up to 1500 kg
Electric Thruster for Spacecraft with Mass up to 2500-3000 kg
Electric Thruster for Spacecraft with Mass up to 3000 kg
Low Power Stationary Plasma Thruster
Stationary Plasma Thruster with a Nominal Discharge Power of 1350 W
Modified Stationary Plasma Thruster with a Nominal Discharge Power of 1350 W
Dual-mode Stationary Plasma Thruster with a Nominal Discharge Power of 2500/1350 W
Stationary Plasma Thruster with a Discharge Power of up to 5 kW
Modified Stationary Plasma Thruster with a Discharge Power of up to 5 kW
Stationary Plasma Thruster with a Discharge Power of up to 6 kW
Stationary Plasma Thruster with a Discharge Power of up to 25 kW
Low Power Stationary Plasma Thruster with 50 mm Diameter of the Accelerating Channel
Modified Low Power Stationary Plasma Thruster with 50 mm Diameter of the Accelerating Channel
Low Power Stationary Plasma Thruster with 70 mm Diameter of the Accelerating Channel
Modified Low Power Stationary Plasma Thruster with 70 mm Diameter of the Accelerating Channel
Thermocatalytic Thrusters
Modified Thermocatalytic Thrusters
Thermocatalytic Low Thruster
Modified Thermocatalytic Low Thruster
Xenon Cold Gas Thruster
Bipropellant Thruster 17d
Bipropellant Thruster 11d
Cool Gas Thruster
Adjustment and Braking Engine
Bipropellant Low Thrust Rocket Engine
Corrective Propulsion System
Corrective Propulsion System 95
Cold Ammonia Corrective Propulsion System
Propulsion System [PS] for Nanosatellite Platform
Integrated Thruster Unit
Integrated Thruster Unit 13
Pressure Stabilization Unit
Station Keeping Thruster Unit Based on Modified Thermocatalytic Thrusters
Station Keeping Thruster Unit Based on Thermocatalytic Thrusters
TU3 Truster Unit Based on Modified Thermocatalytic Low Thrusters
TU1 Thruster Unit Based on Modified Thermocatalytic Low Thruster
3TU Thruster Unit
Attitude Control Thruster Unit Based on Modified Thermocatalytic Low Thrusters
Attitude Control Thruster Unit Based on Thermocatalytic Low Thrusters
XFC unit
Xenon Flow Controller for Stationary Plasma Thruster with a Discharge Power of up to 5 kW
Xenon Flow Controller for Stationary Plasma Thruster with a Nominal Discharge Power of 1350 W
Xenon Flow Controller for Low Power Plasma Thruster with 70 mm Diameter of the Accelerating Channel
Xenon Flow Controller for Low Power Plasma Thruster with 50 mm Diameter of the Accelerating Channel
Propellant Management Assembly (PMA)
Correction Unit (CU) based on Stationary Plasma Thruster with a Nominal Discharge Power of 1350 W and XFC Unit
Thrust Module (TM) Based on Thruster with 70 mm Diameter of the Accelerating Channel with Xenon Flow Controller Unit (XFC Unit)