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Experimental Waterflow Determination of the Dynamic Hydraulic Transfer Function for the J-2X Oxidizer Turbopump: Results and Interpretation - Part TwoExperimental results describing the hydraulic dynamic pump transfer matrix (Yp) for a cavitating J-2X oxidizer turbopump inducer+impeller tested in subscale waterflow are presented. The transfer function is required for integrated vehicle pogo stability analysis as well as optimization of local inducer pumping stability. Dynamic transfer functions across widely varying pump hydrodynamic inlet conditions are extracted from measured data in conjunction with 1D-model based corrections. Derived Dynamic transfer functions are initially interpreted relative to traditional Pogo pump equations. Water-to-liquid oxygen scaling of measured cavitation characteristics are discussed. Comparison of key dynamic transfer matrix terms derived from waterflow testing are made with those implemented in preliminary Ares Upper Stage Pogo stability modeling. Alternate cavitating pump hydraulic dynamic equations are suggested which better reflect frequency dependencies of measured transfer matrices.
Document ID
20120002802
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
Zoladz, Tom
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Patel, Sandeep
(Optical Sciences Corp. Huntsville, AL, United States)
Lee, Erik
(Jacobs Engineering Group, Inc. Huntsville, AL, United States)
Karon, Dave
(Concepts NREC White River Jct., VT, United States)
Date Acquired
August 25, 2013
Publication Date
December 5, 2011
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M11-0640
Report Number: M11-0640
Meeting Information
Meeting: JANNAF 5th Spacecraft Propulsion Subcommittee Meeting
Location: Hunstville, AL
Country: United States
Start Date: December 5, 2011
End Date: December 9, 2011
Sponsors: Department of the Air Force, Department of the Navy, NASA Headquarters, Department of the Army
Distribution Limits
Public
Copyright
Public Use Permitted.
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