Computer Science – Performance
Scientific paper
Feb 1988
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1988cryo...28...90i&link_type=abstract
(NASA, Space Cryogenics Workshop, Madison, WI, June 22, 23, 1987) Cryogenics (ISSN 0011-2275), vol. 28, Feb. 1988, p. 90-95.
Computer Science
Performance
Centrifugal Pumps, Cryopumping, Fluid Management, Liquid Helium 2, Bearings, Cavitation Flow, Space Infrared Telescope Facility
Scientific paper
Two alternate mechanical pump concepts have been identified for the transfer of superfluid helium in space. Both pumps provide flow at sufficient head and have operating characteristics suitable for the Space Infrared Telescope Facility (SIRTF) refill mission. One pump operates at a relatively low speed and utilizes mechanical roller bearings, while the other operates at a higher rotational speed using either electromagnetic or tilting pad gas-dynamic bearings. The use of gas bearings requires transfer of normal helium so that the gas pressure within the pump casing is high enough to operate the bearings. The operating characteristics of both pumps are predicted, the dimensions are estimated and major technology issues are identified. The major issues for each pump design are cavitation performance and bearing development. Roller bearings require quantified reliability for operation in space while electromagnetic bearings require basic development as well as a complex control system. The low speed pump has significantly poorer hydraulic efficiency than the high speed pump.
Izenson Michael G.
Swift Walter L.
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