System and method for combined liquefaction and densification of oxygen
OwnerBrian R. Kromer, Sean M. Kelly +1inventors
InventorsBrian R. Kromer, Sean M. Kelly, Seth A. Potratz
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OwnerBrian R. Kromer, Sean M. Kelly +1inventors
InventorsBrian R. Kromer, Sean M. Kelly, Seth A. Potratz
Estimating the term…
A system and method for the production and supply of a densified, liquid oxidant to a space vehicle launch facility with one or more launch platforms is provided. A low pressure gaseous oxygen stream is piped from a nearby air separation unit and is then liquefied and densified in a two-stage, integrated liquefaction/densification system. The first refrigeration stage is a nitrogen based reverse Brayton cycle refrigeration cycle, that liquefies the gaseous oxygen and subcools the resulting liquid oxygen to a temperature of about 81 Kelvin. The second refrigeration stage is a mixed refrigerant loop containing some combination of helium and/or neon refrigerants that densifies the liquid oxygen to a temperature of about 57 Kelvin. The integrated liquefaction and densification system may also be configured to densify liquid methane or other propellants used in space vehicle launches.
A system for production of a densified, liquid oxygen stream from a low pressure gaseous oxygen stream, the system comprises:
A system for production of a densified, liquid oxygen stream from a gaseous oxygen stream, the system comprises:
Dependencies are inferred from the claim text.