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The ''delta p'' approach from Nike combustion instabilityApplicability of delta p approach to study of combustion instability in liquid and solid propellant rocket engines
Document ID
19660026016
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hisler, A. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 2, 2013
Publication Date
October 4, 1965
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-56943
Report Number: NASA-TM-X-56943
Accession Number
66N35306
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STAGNATION FLOW
SOLID PROPELLANT ROCKET ENGINE
LIQUID PROPELLANT ROCKET ENGINE
COMBUSTION INSTABILITY

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