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Nonlinear Combustion Instability PredictionThe liquid rocket engine stability prediction software (LCI) predicts combustion stability of systems using LOX-LH2 propellants. Both longitudinal and transverse mode stability characteristics are calculated. This software has the unique feature of being able to predict system limit amplitude.
Document ID
20100033605
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
External Source(s)
http://www.techbriefs.com/component/content/article/8432
Authors
Flandro, Gary (Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Date Acquired
August 25, 2013
Publication Date
September 1, 2010
Publication Information
Publication: NASA Tech Briefs, September 2010
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
MFS-32549-1
Report Number: MFS-32549-1
Distribution Limits
Public
Copyright
Public Use Permitted.

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