Hall effect
thrusters

We design stationary Hall effect thrusters that allow manufacturers to reduce the launch mass of satellites, along with increasing its payload to reduce overall cost of production. Our team has developed three models of engines with various capacity: SPT20, SAL37 and SAL40.

THRUSTER WITH ANODE LAYER SAL37

The magnetic system of the thruster is significantly different from the classical scheme. In the central magnetic core a permanent magnet is used instead of an electromagnet. This reduces the power consumption while increasing efficiency. At the exit of the accelerating channel, a pyro graphite ring is used to reduce the erosion of the channel material.

Download our Product Sheet to learn more detailed information on specifications.

THRUSTER WITH ANODE LAYER SAL40

Thruster with anode layer-SAL40 is designed for use as part of the propulsion system for satellites mass up to 1T. It is aimed at solving the tasks of orientation and stabilization of the spacecraft in different orbits. The propulsion system provides a thrust of up to 40mN at a maximum electric power consumption equal to 600W. The propulsion system that contains SAL40 can be used on satellites of various purposes.

Download our Product Sheet to learn more detailed information on specifications.

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