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Experimental Investigation and Analysis of an Annular Pogo AccumulatorAn experimental investigation was conducted on a scaled annular pogo accumulator for the Ares I Upper Stage. The test article was representative of the LO2 feedline and preliminary accumulator design, and included multiple designs of a perforated ring connecting the accumulator to the core feedline flow. The system was pulse tested in water over a range of pulse frequency and flow rates. Time dependent measurements of pressure at various locations in the test article were used to extract system compliance, inertance, and resistance. Results indicate a significant deviation from standard orifice flow theory and suggest a strong dependence on feedline average velocity. In addition, several CFD analyses were conducted to investigate the details of the time variant flow field. Both two-dimensional and three-dimensional simulations were performed with time varying boundary conditions used to represent system pulsing. The CFD results compared well with the sub-scale results and demonstrated the influence of feedline average velocity on the flow into and out of the accumulator
Document ID
20100022138
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
Peugeot, John
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Zoladz, Tom
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Case, Nick
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Yang, H. Q.
(CFD Research Corp. Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
May 3, 2010
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M10-0305
Report Number: M10-0305
Meeting Information
Meeting: 57th JANNAF Joint Propulsion Meeting
Location: Colorado Springs, CO
Country: United States
Start Date: May 3, 2010
End Date: May 7, 2010
Sponsors: Department of the Air Force, NASA Headquarters, Department of the Navy, Department of the Army
Distribution Limits
Public
Copyright
Other

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