The goal of this development was to produce a simple, reliable, and inexpensive power and control system for an electric propulsion system. The system should also provide the collection of telemetry and control for the propellant feeding unit. Using an FPGA as a central control element made it possible to make a flexible system that can be easily adapted to any TC/TM interface and propulsion system control algorithm. The widespread use of COTS components made it possible to short and simplify the development process and reduce the final cost of the product. This system is ideally suited for use on LEO satellites. The system was launched to the space in 2015