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Liquid propellant rocket combustion instabilityThe solution of problems of combustion instability for more effective communication between the various workers in this field is considered. The extent of combustion instability problems in liquid propellant rocket engines and recommendations for their solution are discussed. The most significant developments, both theoretical and experimental, are presented, with emphasis on fundamental principles and relationships between alternative approaches.
Document ID
19720026079
Document Type
Special Publication (SP)
Authors
Harrje, D. T. (NASA Headquarters Washington, DC United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
PROPELLANTS
Report/Patent Number
NASA-SP-194
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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