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A High Repetition Rate, Scalable, Pulsed PPU for Electric Propulsion Applications

Completed TRL 3 (started at 3, targeting 4)

Description

Develop a scalable power processing unit (PPU) for pulsed, high power in-space solar and nuclear electric propulsion systems operating at high repetition rates. Specific goals are to design and construct a PPU for pulsed electric propulsion systems which demonstrate scalable, high power (1–10 kW, with scaling to at least 100 kW) operation at high pulse rates (1–10 kHz) while simultaneously achieving high electrical efficiency (at least 80%), low specific mass (no more than 3 kg/kW), and compatibility with standard large spacecraft bus voltages (120–200 V).

Benefits

Potential applications at these power levels include reduced orbit raising times for communications satellites, orbit transfers for the NASA Lunar Orbital Platform-Gateway, deep space science missions, and cargo missions to Mars. Scaling the technology to higher average power levels (100’s of kW) could ultimately support manned missions to the Moon and Mars.

Details

Technology areaPropulsion Systems > Electric Space Propulsion > Electromagnetic Propulsion
ProgramCenter Independent Research & Development: MSFC IRAD (MSFC IRAD)
Lead organizationMarshall Space Flight Center, Huntsville, AL
Start date2019-04-01
End date2021-10-31

Project contacts

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How to get involved

This is early/mid-stage (TRL 3) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.

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