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Advanced Booster Liquid Engine Combustion StabilityCombustion instability is a phenomenon in liquid rocket engines caused by complex coupling between the time-varying combustion processes and the fluid dynamics in the combustor. Consequences of the large pressure oscillations associated with combustion instability often cause significant hardware damage and can be catastrophic. The current combustion stability assessment tools are limited by the level of empiricism in many inputs and embedded models. This limited predictive capability creates significant uncertainty in stability assessments. This large uncertainty then increases hardware development costs due to heavy reliance on expensive and time-consuming testing.
Document ID
20160008013
Acquisition Source
Marshall Space Flight Center
Document Type
Other
Authors
Tucker, Kevin
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Gentz, Steve
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Nettles, Mindy
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
June 29, 2016
Publication Date
January 1, 2015
Publication Information
Publication: George C. Marshall Space Flight Center Research and Technology Report 2014
Subject Category
Spacecraft Propulsion And Power
Fluid Mechanics And Thermodynamics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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