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Fluid quantity gagingA system for measuring the mass of liquid in a tank on orbit with 1 percent accuracy was developed and demonstrated. An extensive tradeoff identified adiabatic compression as the only gaging technique that is independent of gravity or its orientation, and of the size and distribution of bubbles in the tank. This technique is applicable to all Earth-storable and cryogenic liquids of interest for Space Station use, except superfluid helium, and can be applied to tanks of any size, shape, or internal structure. Accuracy of 0.2 percent was demonstrated in the laboratory, and a detailed analytical model was developed and verified by testing. A flight system architecture is presented that allows meeting the needs of a broad range of space fluid systems without custom development for each user.
Document ID
19910015252
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mord, Allan J.
(Ball Aerospace Systems Div. Muncie, IN, United States)
Snyder, Howard A.
(Ball Aerospace Systems Div. Muncie, IN, United States)
Kilpatrick, Kathleen A.
(Ball Aerospace Systems Div. Muncie, IN, United States)
Hermanson, Lynn A.
(Ball Aerospace Systems Div. Muncie, IN, United States)
Hopkins, Richard A.
(Ball Aerospace Systems Div. Muncie, IN, United States)
Vangundy, Donald A.
(Ball Aerospace Systems Div. Muncie, IN, United States)
Date Acquired
September 6, 2013
Publication Date
December 5, 1988
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-185516
NAS 1.26:185516
F88-06-102A
Report Number: NASA-CR-185516
Report Number: NAS 1.26:185516
Report Number: F88-06-102A
Accession Number
91N24566
Funding Number(s)
CONTRACT_GRANT: NAS9-17616
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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