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Strain Gage Measurement System to Determine Cryogenic Propellant Tank LevelMeasurement of tank level, particularly for cryogenic propellants, has proven to be a difficult proposition. Current methods based on differential pressure, capacitance sensors, temperature sensors, etc.; do not provide sufficiently accurate or robust measurements, especially at run time. This paper describes a simple, but effective method to determine propellant volume by measuring very small deformations of the structure supporting the tank. Results of a laboratory study to validate the method, and experimental data from a deployed system are presented. A comparison with an existing differential pressure sensor shows that the strain gage system provides a very good quality signal even during pressurization.
Document ID
20040008399
Acquisition Source
Stennis Space Center
Document Type
Conference Paper
Authors
Figueroa, Fernando
(NASA Stennis Space Center Stennis Space Center, MS, United States)
St.Cyr, William W.
(NASA Stennis Space Center Stennis Space Center, MS, United States)
VanDyke, David
(Lockheed Martin Space Operations Bay Saint Louis, MS, United States)
McVay, Greg
(Lockheed Martin Space Operations Bay Saint Louis, MS, United States)
Mitchell, Mark
(Lockheed Martin Space Operations Bay Saint Louis, MS, United States)
Langford, Lester
(Lockheed Martin Space Operations Bay Saint Louis, MS, United States)
Date Acquired
August 21, 2013
Publication Date
July 20, 2003
Subject Category
Instrumentation And Photography
Report/Patent Number
SE-2002-11-00075-SSC
Meeting Information
Meeting: 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Location: Huntsville, AL
Country: United States
Start Date: July 20, 2003
End Date: July 23, 2003
Sponsors: American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers, American Society of Mechanical Engineers, Society of Automotive Engineers, Inc.
Funding Number(s)
CONTRACT_GRANT: NAS13-650
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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