Power supply for aerospace applications PPU

for satellite platformDC/DC

This technology demonstrator of a Propulsion Power Unit was used to prove the ASP technology concept by coupling tests with a RIT thruster. The digital control is based on a FPGA to convert all required signals into a digital value, calculate the control algorithm and generate the PWM pattern to drive the power stage. Details: Power: 300 W Outputs: RFG Neutralizer Heater Neutralizer Keeper Neutralizer Ignition Valve control