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Propellant Delivery Via VDC Driven Pump, Year 2

Completed TRL 5 (started at 4, targeting 5)

Description

Current cryogenic propellant delivery systems typically rely on some combination of high volume/pressure/mass/cost run tanks and gaseous driven turbomachinery for supply to a rocket engine. Reducing the physical size of the propellant delivery system enables mobility and shifts the volume handling requirement from expensive pressure rated vessels to far cheaper storage vessels. Further it could yield valuable data in terms of cryogenic handling and transfer for potential application outside of main propulsion systems.

Benefits

More efficient, reliable, quick turnaround testing

Details

Technology areaGround, Test, and Surface Systems > Infrastructure Optimization > Propellant Production, Storage, and Transfer
ProgramCenter Innovation Fund: SSC CIF (SSC CIF)
Lead organizationStennis Space Center, Stennis Space Center, MS
Start date2020-10-01
End date2021-09-30

Project contacts

Listed on TechPort itself — the most direct way to ask about this specific project.

How to get involved

This is early/mid-stage (TRL 5) — 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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