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Liquid propellant densificationSuper cooling the cryogenic liquid propellant in a vehicle propellant tank densities the propellant allowing the vehicle propellant tank to carry more fuel in the same volume tank while lowering the vapor pressure and thus the tank operating pressure. Lowering the tank operating pressure reduces the stress and therefore allows the walls of the tank to be thinner. Both the smaller tank volume and thinner tank wall results in an overall smaller and lighter vehicle with increased payload capability. The cryogenic propellant can be supercooled well below the normal boiling point temperature level by transporting the liquid propellant from the vehicle tanks to a ground based cooling unit which utilizes a combination of heat exchanger and compressor. The compressor lowers the coolant fluid bath pressure resulting in a low temperature boiling liquid which is subsequently used to cool the recirculating liquid. The cooled propellant is then returned to the vehicle propellant tank. In addition to reducing the vehicle size and weight the invention also allows location of the vent valve on the ground, elimination of on-board recirculation pumps or bleed systems, smaller and lighter engine pumps and valves, lighter and more stable ullage gas, and significant reduction in tank fill operation. All of these mentioned attributes provide lower vehicle weight and cost.
Document ID
20080004638
Acquisition Source
Johnson Space Center
Document Type
Other - Patent
Authors
Lak, Tibor I.
Petrilla, Steve P.
Lozano, Martin E.
Date Acquired
August 24, 2013
Publication Date
July 8, 1997
Subject Category
Propellants And Fuels
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-533423
Patent Number: US-PATENT-5,644,920
Funding Number(s)
CONTRACT_GRANT: NAS9-18500
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,644,920
Patent Application
US-PATENT-APPL-SN-533423
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