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Flowmeter evaluation for on-orbit operationsVarious flowmetering concepts were flow tested to characterize the relative capabilities and limitations for on-orbit fluid-transfer operations. Performance results and basic operating principles of each flowmetering concept tested are summarized, and basic considerations required to select the best flowmeter(s) for fluid system application are discussed. Concepts tested were clamp-on ultrasonic, area averaging ultrasonic, offset ultrasonic, coriolis mass, vortex shedding, universal venturi tube, turbine, bearingless turbine, turbine/turbine differential-pressure hybrid, dragbody, and dragbody/turbine hybrid flowmeters. Fluid system flowmeter selection considerations discussed are flowmeter performance, fluid operating conditions, systems operating environments, flowmeter packaging, flowmeter maintenance, and flowmeter technology. No one flowmetering concept tested was shown to be best for all on-orbit fluid systems.
Document ID
19890004389
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Baird, R. S.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1988
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
S-578
NAS 1.15:100465
NASA-TM-100465
Report Number: S-578
Report Number: NAS 1.15:100465
Report Number: NASA-TM-100465
Accession Number
89N13760
Funding Number(s)
PROJECT: RTOP 906-63-06-33
PROJECT: RTOP 992-15-00-00-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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