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: SPT 20, SPT 40 and SPT 100.

SPT 20

Xenon plasma thruster SPT 20 is designed for use in the propulsion system for satellites mass up to 150kg to work in Low-Earth Orbit (LEO). At the maximum electric power consumption equal to 150W, Xenon plasma thruster provides a thrust up to 7mN. The propulsion system on basis of SPT 20 can be used in Earth’s remote sensing satellites, weather prediction, communication, and others.

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

SPT 40

Xenon plasma thruster SPT 40 is designed for use as a 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 15 mN at a maximum electric power consumption of 380W. The propulsion system that contains SPD 40 can be used on satellites of various purposes.

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

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