Overview

A centrifugal pump was developed for the efficient and reliable transfer of liquid helium in space. The pump can be used to refill cryostats on orbiting satellites which use liquid helium for refrigeration at extremely low temperatures. The pump meets the head and flow requirements of on-orbit helium transfer: a flow rate of 800 L/hr at a head of 128 J/kg. The overall pump efficiency at the design point is 0.45. The design head and flow requirements are met with zero net positive suction head, which is the condition in an orbiting helium supply Dewar. The mass transfer efficiency calculated for a space transfer operation is 0.99. Steel ball bearings are used with gas fiber-reinforced teflon retainers to provide solid lubrication. These bearings have demonstrated the longest life in liquid helium endurance tests under simulated pumping conditions. Technology developed in the project also has application for liquid helium circulation in terrestrial facilities and for transfer of cryogenic rocket propellants in space. Hasenbein, Robert and Izenson, Michael G. and Swift, Walter L. and Sixsmith, Herbert Unspecified Center CENTRIFUGAL PUMPS; CRYOGENIC ROCKET PROPELLANTS; CRYOPUMPING; CRYOSTATS; LIQUID HELIUM; ORBITAL SERVICING; PROPELLANT TRANSFER; REFRIGERANTS; BALL BEARINGS; CRYOGENIC EQUIPMENT; FLOW VELOCITY; HEAD FLOW; LOW TEMPERATURE; MASS TRANSFER; SOLID LUBRICANTS; SUCTION; TEFLON (TRADEMARK)...

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9781723143328

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