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RF gauging efforts with liquid hydrogen and liquid oxygen as applicable to subcritical space vehicle systemsThe RF gauging concept is based on the interaction between a fluid dielectric medium in an enclosed metallic cavity and electromagnetic fields set up within that cavity. In RF gauging systems, the fundamental measurement relies on the interpretation of changes in the resonant RF frequencies of an enclosed tank as the mass of the propellant contained in the tank is changed. In addition to a discussion of the basic principles of operation of these systems, the study presents a description of the current breadboard implementation with typical test arrangements, along with supporting test data. The experimental testing of the RF gauging technique for liquid cryogen mass gauging indicates that this technique is a feasible approach to liquid oxygen and liquid hydrogen gauging under all attitude or reduced gravity environments.
Document ID
19750059921
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Thompson, H. E.
(NASA Marshall Space Flight Center Huntsville, Ala., United States)
Ott, W.
Stanley, N.
(Bendix Corp. Davenport, Iowa, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1974
Subject Category
Propellants And Fuels
Meeting Information
Meeting: Cryogenic Engineering Conference
Location: Atlanta, GA
Start Date: August 8, 1973
End Date: August 10, 1973
Accession Number
75A43993
Distribution Limits
Public
Copyright
Other

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