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Data Oscillation Resolution of Propellant Flowmeter Used in FASTRAC Engine TestingThe Stennis Space Centers' horizontal test facility, Marshall Space Flight Centers' propulsion test article and the X-34 flight vehicle are designed with V-cone flowmeters for measurement of both RP-1 and LOX flow-rates for Fastrac engine testing. Delta pressure transducer data from these flowmeters are used to calibrate the RP-1 and LOX mixture ratio in the Fastrac engine. Data from the V-Cone flowmeter delta pressure transducers have excessive oscillation. The delta pressure oscillations have caused flowrate data fluctuations that interfered with making the accurate readings necessary to calibrate the RP-1 and LOX mixture ratio required for Fastrac engine operation. The objective of this report is to document the flowmeter data oscillation problem and the method used to obtain more reliable flowmeter data.
Document ID
20000093951
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Heflin, J.
(Sverdrup Technology, Inc. Huntsville, AL United States)
Koelbl, M.
(Sverdrup Technology, Inc. Huntsville, AL United States)
Martin, M. A.
(Sverdrup Technology, Inc. Huntsville, AL United States)
Nesman, T.
(Sverdrup Technology, Inc. Huntsville, AL United States)
Hicks, G. D.
(Sverdrup Technology, Inc. Huntsville, AL United States)
Kennedy, Jim W.
Date Acquired
September 7, 2013
Publication Date
February 1, 2000
Subject Category
Instrumentation And Photography
Meeting Information
Meeting: 36th Joint Propulsion Conference
Location: Huntsville, AL
Country: United States
Start Date: July 17, 2000
End Date: July 19, 2000
Sponsors: American Society for Electrical Engineers, American Society of Mechanical Engineers, Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NAS8-40836
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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