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Design Analysis of the Ares 1 Pogo AccumulatorSeveral accumulator designs and gas charge systems are considered in order to suppress POGO within the Ares I vehicle Upper Stage Liquid Ox ygen System. The thermodynamic and flow analysis completed to evaluat e candidate designs are presented and the results are used to evaluat e the ability of each concept to meet the levied suppression requirements. One annular accumulator design meets all suppression requirement s while also providing manufacturability and operability advantages. Of the two proposed charge systems to provide and maintain gas within the accumulator, a passive level control design meets the charge req uirements and maximizes reliability.
Document ID
20090034946
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Swanson, Luke A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Giel, Thomas V.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
August 2, 2009
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
M09-0237
M09-0548
Report Number: M09-0237
Report Number: M09-0548
Meeting Information
Meeting: 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Location: Denver, CO
Country: United States
Start Date: August 2, 2009
End Date: August 5, 2009
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNM-05ABSC
Distribution Limits
Public
Copyright
Public Use Permitted.
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