The CSSP delivers improved flow, pressure and two-phase flow capability of cryogenic pumping to achieve NASA�s goal of methane in space propulsion for scalably sized spacecraft. A single or linked CSSP could be integrated into satellites or a spacecraft�s reaction control system to increase fuel flow rates and pressure providing better flexibility and dexterity during docking and landing. RES systems allow for altitude, translation, and rotational control and the CSSP would allow such systems to be integrated on to potentially larger or smaller modules. The CSSP minimizes space and weight needs while significantly improving fuel flow rate and pressure, allowing better engineering optimization for NASA modular spacecraft. The CSSP enables efficient, low or zero boil-off cryogenic systems by circulating cryogenic helium gas from a cryocooler to broad area thermal shields surrounding the tanks. This would eliminate the need for high-efficiency heat exchangers that are required with ambient temperature circulator pumps. The pump would also enable thermodynamic vent systems in which cryo propellants are dropped in pressure and temperature and heat exchanged with liquid pumped in a circulation loop within the tank. The development of a long life, variable speed, and low leakage pump would add flexibility to NASA satellite and surface to space spacecraft.
Hydrogen has been identified as a potentially game-changing fuel by the aerospace industry, however, the necessary heavy cryogenic fuel tanks and low-pressure pumps have handicapped successful research and development. Integration of CSSP in hydrogen aircraft and unmanned aerial vehicles would improve fuel delivery, reduce fuel tank size, and become a critical component of lightweight aircraft. The estimated weight savings of the proposed pump is over 400 pounds per aircraft. The scroll pump would be a significant contributor to increased aircraft endurance and payload. Several aerospace leaders, including Boeing and AeroViromnet, already partner with Air Squared and demonstrate a niche market for the CSSP for next-generation aircraft with both the Department of Defense and commercial research and development. Another commercial application would be a liquid natural gas pump, for LNG rail transport. SOA offers only limited options for positive displacement LNG pumps of which the CSSP two-phase fuel delivery and variable pressure operations could be disruptive. Progress Rail has already contacted Air Squared about using a positive displacement LNG scroll pump for locomotive transportation and has invested in an Air Squared�s orbiting scroll type LNG pump prototype. The greater reliability and flexible scaling of the CSSP holds vast potential in the next generation cryogenic fuel economy.
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