NASA applications for the technology developed under this SBIR include low heat leak cryogenic circulators and transfer pumps for propellant depot, upper stage engine recirculation pumps, and cryogenic stage boost pumps, including the NTP application. Additional applications for this technology include small, light-weight, cryogenic; Hydrogen, Methane, Oxygen propellant boost pumps for chemical rocket engine applications as well as propellant loading ground support equipment.
Potential Non-NASA commercial applications of the technology developed under this SBIR include any boost pump application for cryogenic upper stages to increase main pump NPSP margins and/or reduce tank pressurization requirements to reduce system weight. Ground based refueling station applications to transfer liquid natural gas from the storage tank to the vehicle tank.
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