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Propellant Mass Gauging in Microgravity with Electrical Capacitance TomographyAdvancements in microgravity propellant mass gauging will result in improvements to many areas of propellant management, which influences space vehicle performance and mission assurance. Propellant mass gauging technologies designed to work in an accelerated environment, where the propellant remains settled at one end of the propellant tank, do not always work well in a microgravity environment because the propellant is not necessarily settled. While some microgravity mass gauging technologies exist at various stages of development, most of them have major disadvantages. Electrical Capacitance Tomography (ECT) is a sensing technology that is able to reconstruct the liquid distribution inside of a tank, which can then be integrated to obtain mass. While ECT mass gauging will theoretically work during all phases of flight, it had not yet been tested in microgravity. The NASA Kennedy Space Center Launch Services Program, with support from the Flight Opportunities Program, successfully tested an ECT liquid mass gauging system experiment on a parabolic flight aircraft in May 2022. Basics of ECT measurement theory, details of the experiment setup, data processing, ground test results, and the flight test result will be discussed. The results suggest that ECT sensor systems will be useful as a propellant mass gauging technology in both accelerated and microgravity environments.
Document ID
20230012805
Acquisition Source
Kennedy Space Center
Document Type
Technical Publication (TP)
Authors
Jedediah M Storey
(Kennedy Space Center Merritt Island, Florida, United States)
Brandon S Marsell
(Kennedy Space Center Merritt Island, Florida, United States)
Michael T Elmore
(AI Solutions Lanham, Maryland, United States)
Scott Clark
(AI Solutions Lanham, Maryland, United States)
Date Acquired
August 31, 2023
Publication Date
September 1, 2023
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Spacecraft Instrumentation and Astrionics
Spacecraft Propulsion and Power
Funding Number(s)
WBS: 725932.08.03.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
electrical capacitance tomography
propellant tank
slosh
mass gauging
microgravity
zero-g
parabolic
fluid mechanics
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