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Modal Propellant Gauging: High-resolution and non-invasive gauging of both settled and unsettled liquids in reduced gravity.The modal response of a liquid-filled tank to external acoustic excitation can be used to infer with high resolutionthe mass of contained liquid, the mass flow rate of liquids into and out of the tank, and changes in tank pressure.Both contained liquid mass and internal ullage pressure affect the modal response of the tank walls through fluidmass-loading of the tank walls and pressure-induced wall stiffening, respectively. Modal Propellant Gauging refersto the technology that exploits these shifts in modal frequencies to infer the mass of propellant in a tank. MPG is anon-invasive gauging technology that has demonstrated gauging resolutions of 1% for settled propellants and 2-3%for unsettled, sloshing propellants. Extensive parabolic flight testing of the MPG system on model tanks has beenconducted to validate the technology in reduced gravity. MPG testing on a qualification tank for the Orion Program'sEuropean Service Module has also been conducted and is reported here. Finite element modeling of the OrionESM "upper" tank is discussed and compared with measurement data. Three computational approaches to massdetermination, Peak Tracking, Point Sensor, and Spectral Density methods, are described here. Use cases are definedand analyzed in the context of the Orion ESM Qualification tank data, and an implementation scheme for continuousmass gauging on the Orion ESM is discussed.Keywords: Propellant Mass Gauging, Modal Analysis, Orion ESM
Document ID
20200002896
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
External Source(s)
Authors
Kevin M Crosby
(Carthage College Kenosha, Wisconsin, United States)
Nehemiah J Williams
(Johnson Space Center Houston, Texas, United States)
Rudolph Werlink
(Kennedy Space Center Merritt Island, Florida, United States)
Eric A Hurlbert
(Johnson Space Center Houston, Texas, United States)
Date Acquired
April 22, 2020
Subject Category
Propellants And Fuels
Report/Patent Number
JSC-E-DAA-TN61248
IAC-18-C4.3.15 x42358
Report Number: JSC-E-DAA-TN61248
Meeting Information
Meeting: 69th International Astronautical Congress (IAC)
Location: Bremen
Country: DE
Start Date: October 2, 2018
End Date: October 5, 2018
Sponsors: International Astronautical Federation
Funding Number(s)
CONTRACT_GRANT: HQ-SG-FSP
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
Propellant Mass Gauging
Propellant Mass Gauging
Orion service module
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