US 6,131,395 AGranted

Propellant densification apparatus and method

AssigneeLockheed Martin Corporation

InventorsWilliam Duncan Greene, Miranda Leigh Anthony

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Abstract

A method for densifying the LO2 propellant of a vehicle (10) includes providing a heat exchanger (16) including a chamber (22), and an isolated heater (24) and cooler (26) located within the chamber (22). The method further includes the step of pumping propellant (LO2) (with pump 14) from the vehicle (10) to the first port (24i) of the path of the heater (24), to thereby create a flow of propellant (LO2) through the heater (24) path, and from the second port (24o) of the path of the heater (24). In conjunction with the pumping, propellant (LO2) is coupled from the second port (24o) of the heater (24) back to the vehicle (10), to thereby establish a recirculating flow of propellant (LO2). The chamber (22) of the heat exchanger (16) is filled with at least sufficient cryogenic liquid (LN2) to cover at least a portion of the path of the cooler (26), and preferably the entirety of the path of the cooler (26). A cryogenic fluid (LH2) is boiled, to thereby cool the cryogenic fluid, and the resulting cooled cryogenic fluid is flowed through the path of the cooler (26). As a result, or whereby, the flow of the cooled cryogenic fluid through the cooler (26) cools the cryogenic liquid, and the cryogenic liquid cools the heater (24) by convection (60). When the cryogenic liquid cools the heater (24), the cryogenic propellant (LO2) flowing through the heater (24) gives up heat to the cryogenic liquid and becomes cooler (26), thereby densifying the cryogenic propellant (LO2).

Claims4

Dependent claims

A method for densifying the propellant of a vehicle, said method comprising the steps of:

providing a heat exchanger including a chamber, a heater located within said chamber, and a cooler also located within said chamber, at a position higher than said heater, said heater comprising a path through said chamber for the flow of fluid, said path of said heater being isolated from said chamber so that fluid in said path of said heater cannot co-mingle with fluid in said chamber as said fluid in said path of said heater moves from a first port to a second port of said path of said heater, said cooler also comprising a path through said chamber for the flow of fluid, said path of said cooler being isolated from said chamber so that fluid in said path of said cooler cannot co-mingle with fluid in said chamber as said fluid in said path of said cooler moves from a first port to a second port of said path of said cooler;
pumping propellant from said vehicle to said first port of said path of said heater, to thereby create a flow of propellant from said second port of said path of said heater;
coupling propellant from said second port of said heater back to said vehicle, to thereby establish a recirculating flow of propellant;
filling said chamber of said heat exchanger with at least sufficient cryogenic liquid to cover at least a portion of said path of said cooler;
boiling a cryogenic fluid to thereby cool said cryogenic fluid, and flowing cooled cryogenic fluid through said path of said cooler, whereby said flow of said cooled cryogenic fluid through said cooler cools said cryogenic liquids, and said cryogenic liquid cools said heater by convection, whereby said cryogenic propellant flowing through said heater gives up heat to said cryogenic liquid and becomes cooler, thereby densifying said cryogenic propellant.

2 more elements

Dependencies are inferred from the claim text.