ST40 hall-effect thruster
The ST40 Hall-Effect Thruster with an anode layer is designed for use as part of the propulsion system for satellites mass up to 1 T. It is used to orient and stabilize of the spacecraft in various orbits. The propulsion system provides a thrust of up to 35 mN at a maximum electric power consumption of 500 W. The propulsion system that contains ST40 can be used on satellites for various purposes.
Input power, W
up to 500
Specific Impulse, s
1500
Thrust, mN
35
Efficiency, %
45
ST40
hall-effect thruster
/
Other systems
The SPS40 Propulsion System was designed for medium and large satellites and able to adjust the orbit parameters and insure the maneuverability of satellites in space.
The SPS37 Propulsion System was designed for mini satellites mass up to 500 kg.
The ST37 Hall-Effect Thruster is a modification of a Thruster with an Anode Layer.
SETS is developing a modular Xenon Feed System (XFS) with significant reductions in mass and cost while increasing system reliability.
