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Power supply for aerospace applications PPU
for satellite platformDC/DC

power supply for aerospace applications
power supply for aerospace applications
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for aerospace applications, for satellite platform
Input voltage

28 V

Output voltage

Max.: 900 V

Min.: -250 V


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
*Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.