POLON is a satellite propulsion module, developed by Lukasiewicz Research Network - Institute of Aviation in cooperation with Creotech Instruments. The product is designed for small platforms operating at LEO. It is based on a monopropellant 98% hydrogen peroxide propulsion system, providing delta V and ACS. With nominal thrust at the level of 4 N, the system delivers minimum 8 kNs of the total impulse.
The project is funded by NCBiR.