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Inlet Cover Treatment to Enhance Zero NPSH Inducer Operation
Completed
TRL 3 (started at 2, targeting 3)
Description
Zero net positive suction head (NPSH)-capable hydrogen pump inducers are a critical component needed to lower the cost and increase the effectiveness of Nuclear Thermal Propulsion (NTP) engines. Zero NPSH pumps need to be able to pump up to 55% vapor fraction by volume without significant head fall-off. Current technology inducers can pump liquid hydrogen up to a limit of about 25% vapor fraction by volume because of choking of the vapor in either the inlet pipe or the inducer blade passage. It is proposed that the Concepts NREC (CN) inlet cover treatment cavitation and stability control device (SCD) will be able to increase the hydrogen vapor volume pumping fraction to the required 55%. The device allows the inducer to operate stably at high blade angles and low flow coefficients which increases the blade passage and the inlet pipe area to delay choking of the pumped fluid.
Benefits
Nuclear Thermal Propulsion (NTP) hydrogen two-phase pump and chemical rocket pumps for any fluid that exhibits some level of thermal suppression head benefit like hydrogen or oxygen.
High power density electronic cooling that requires two-phase pumping and Oil/gas mixture seabed pumps
Details
| Technology area | Thermal Management Systems > Cryogenic Systems > In-Space Propellant Storage and Use |
| Program | Small Business Innovation Research/Small Business Tech Transfer (SBIR/STTR) |
| Lead organization | Concepts NREC, LLC, White River JCT, VT |
| Start date | 2014-06-20 |
| End date | 2014-12-19 |
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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